NX Nastran 8 DMAP Programmer's Guide

NX Nastran 8 DMAP Programmer’s Guide

Proprietary & Restricted Rights Notice

© 2011 Siemens Product Lifecycle Management Software Inc. All Rights Reserved. This software and related documentation are proprietary to Siemens Product Lifecycle Management Software Inc. NASTRAN is a registered trademark of the National Aeronautics and Space Administration. NX Nastran is an enhanced proprietary version developed and maintained by Siemens Product Lifecycle Management Software Inc. MSC is a registered trademark of MSC.Software Corporation. MSC.Nastran and MSC.Patran are trademarks of MSC.Software Corporation. All other trademarks are the property of their respective owners.

TAUCS Copyright and License TAUCS Version 2.0, November 29, 2001. Copyright (c) 2001, 2002, 2003 by Sivan Toledo, Tel-Aviv University, [email protected]. All Rights Reserved. TAUCS License: Your use or distribution of TAUCS or any derivative code implies that you agree to this License. THIS MATERIAL IS PROVIDED AS IS, WITH ABSOLUTELY NO WARRANTY EXPRESSED OR IMPLIED. ANY USE IS AT YOUR OWN RISK. Permission is hereby granted to use or copy this program, provided that the Copyright, this License, and the Availability of the original version is retained on all copies. User documentation of any code that uses this code or any derivative code must cite the Copyright, this License, the Availability note, and "Used by permission." If this code or any derivative code is accessible from within MATLAB, then typing "help taucs" must cite the Copyright, and "type taucs" must also cite this License and the Availability note. Permission to modify the code and to distribute modified code is granted, provided the Copyright, this License, and the Availability note are retained, and a notice that the code was modified is included. This software is provided to you free of charge. Availability (TAUCS) As of version 2.1, we distribute the code in 4 formats: zip and tarred-gzipped (tgz), with or without binaries for external libraries. The bundled external libraries should allow you to build the test programs on Linux, Windows, and MacOS X without installing additional software. We recommend that you download the full distributions, and then perhaps replace the bundled libraries by higher performance ones (e.g., with a BLAS library that is specifically optimized for your machine). If you want to conserve bandwidth and you want to install the required libraries yourself, download the lean distributions. The zip and tgz files are identical, except that on Linux, Unix, and MacOS, unpacking the tgz file ensures that the configure script is marked as executable (unpack with tar zxvpf), otherwise you will have to change its permissions manually.

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DMAP Programmer’s Guide

Contents

Proprietary & Restricted Rights Notice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Direct Matrix Abstraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 Introduction to DMAP . . . . . . . . . . . . . . . . . . . . The NX Nastran DMAP Language . . . . . . . . . . . Parameters . . . . . . . . . . . . . . . . . . . . . . . . . . . Data Blocks . . . . . . . . . . . . . . . . . . . . . . . . . . . Instructions . . . . . . . . . . . . . . . . . . . . . . . . . . . Output from a Previous Module Rule . . . . . . . . . Automatic Deletion of Scratch Data Blocks . . . . . Preface Modules and SOLution 100 . . . . . . . . . . Processing User Errors . . . . . . . . . . . . . . . . . . . SubDMAPs DBMGR, DBSTORE, and DBFETCH WHERE and CONVERT Clauses . . . . . . . . . . . .

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. 1-2 . 1-2 . 1-3 1-10 1-12 1-30 1-30 1-31 1-32 1-32 1-34

Overview of Data Blocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 Matrix Data Blocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 Table Data Blocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2 Data Block Descriptions A-E . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 AXIC . . . . AXIC68 . . BGPDT . . BGPDT68 . CASECC . CDDATA . CLAMA . . CONTAB . CONTACT CSTM . . . CSTM68 . . DBCOPT . DESCYC . DESTAB . DISTL . . . DIT . . . . . DSCMCOL DVPTAB . DYNAMIC EDOM . . . EDT . . . . . EGPSF . . . EGPSTR .

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. 3-2 3-14 3-26 3-28 3-29 3-49 3-53 3-54 3-55 3-60 3-62 3-69 3-71 3-72 3-73 3-74 3-78 3-90 3-92 3-106 3-133 3-161 3-166

DMAP Programmer’s Guide

3

Contents

ELDCT EPT . . . EPT705 EQEXIN ERROR EST . . .

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3-169 3-171 3-207 3-242 3-244 3-245

Data Block Descriptions F-M . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 FOL . . . . . GEOM1 . . GEOM2 . . GEOM3 . . GEOM4 . . GEOM168 GEOM4705 GPDT . . . GPDT68 . . GPL . . . . . HIS . . . . . KDICT . . . LAMA . . . MPT . . . .

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. 4-1 . 4-2 4-15 4-64 4-80 4-106 4-119 4-144 4-145 4-146 4-147 4-148 4-150 4-152

Data Block Descriptions O-V . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-1 OBC . . . OBG . . . OBJTAB OCCORF OCPSDF OEE . . . OEF . . . . OEFMC . OES . . . . OESMC . OGF . . . OGK . . . OGS . . . OMECON OMEOSC OMKEC OMKEO OMSEC . OMSEO OPG . . . OPTPRM OQG . . . OQGMC . OSDISP2 OSHT . . OSPDS . . OSTRMC OUG . . . OUGGC .

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DMAP Programmer’s Guide

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5-1 5-3 5-7 5-8 5-9 5-10 5-16 5-84 5-87 5-279 5-281 5-286 5-288 5-295 5-297 5-299 5-302 5-304 5-306 5-308 5-313 5-314 5-320 5-322 5-323 5-325 5-327 5-330 5-342

Contents

OUGMC . OUGPC . OUGRC . R1MAP . R1TAB . RESP3 . RESP12 SEMAP . SET . . . SETMC . SIL . . . . TOL . . . VIEWTB

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5-344 5-349 5-351 5-354 5-355 5-363 5-366 5-369 5-373 5-374 5-375 5-376 5-376

Glossaries . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1 Data Block Glossary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1 Parameter Glossary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-55 NASTRAN Data Definition Language (NDDL)

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NDDL Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-1 Detailed Description of NDDL Statements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-2 Overview of DMAP Modules and Statements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-1 DMAP Module and Statement List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-1 DMAP Module and Statement Description Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-5 Descriptions of DMAP Modules and Statements . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-1 ACMG . . . . ADAPT . . . ADD . . . . . ADD5 . . . . . ADDVM . . ADG . . . . . ADR . . . . . AELOOP . . AEMODEL AMG . . . . . AMP . . . . . APD . . . . . APPEND . . ASDR . . . . ASG . . . . . AXMDRV . AXMPR1 . . AXMPR2 . . BCDR . . . . BDRYINFO BGCASO . . BGP . . . . . BMG . . . . . BNDSPC . . BOLTFOR .

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9-2 9-3 9-6 9-8 9-10 9-10 9-12 9-13 9-15 9-15 9-17 9-18 9-20 9-23 9-25 9-26 9-27 9-28 9-29 9-30 9-32 9-33 9-34 9-35 9-36

DMAP Programmer’s Guide

5

Contents

BOLTSF . . . . . . . . . . CASE . . . . . . . . . . . CEAD . . . . . . . . . . . CHKCOME . . . . . . . CHKCOMG . . . . . . . CHKCVG . . . . . . . . . CMPZPR . . . . . . . . . CNTGLUE . . . . . . . . CNTITER . . . . . . . . . COMBOUT . . . . . . . COPY . . . . . . . . . . . CURV . . . . . . . . . . . CURVPLOT . . . . . . . CYCLIC1 . . . . . . . . CYCLIC2 . . . . . . . . CYCLIC3 . . . . . . . . CYCLIC4 . . . . . . . . DBC . . . . . . . . . . . . DBDELETE . . . . . . DBDICT . . . . . . . . . DBEQUIV . . . . . . . . SubDMAP DBFETCH SubDMAP DBMGR . DBSTATUS . . . . . . . SubDMAP DBSTORE DBVIEW . . . . . . . . . DCMP . . . . . . . . . . . DDR2 . . . . . . . . . . . DDR2N . . . . . . . . . . DDRMM . . . . . . . . . DECOMP . . . . . . . . DELETE . . . . . . . . . DIAGONAL . . . . . . . DISDCMP . . . . . . . . DISFBS . . . . . . . . . . DISOFPM . . . . . . . . DISOFPS . . . . . . . . . DISOPT . . . . . . . . . . DISUTIL . . . . . . . . . DIVERG . . . . . . . . . DMIIN . . . . . . . . . . . DOM6 . . . . . . . . . . . DOM9 . . . . . . . . . . . DOM10 . . . . . . . . . . DOM11 . . . . . . . . . . DOM12 . . . . . . . . . . DOPFS . . . . . . . . . . DOPR1 . . . . . . . . . . DOPR2 . . . . . . . . . . DOPR3 . . . . . . . . . . DOPR4 . . . . . . . . . . DOPR5 . . . . . . . . . . DOPR6 . . . . . . . . . . DOPRAN . . . . . . . . .

6

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DMAP Programmer’s Guide

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9-37 9-38 9-43 9-45 9-46 9-47 9-48 9-49 9-49 9-52 9-52 9-53 9-55 9-56 9-58 9-59 9-61 9-63 9-70 9-71 9-83 9-85 9-86 9-89 9-90 9-92 9-93 9-96 9-99 9-102 9-104 9-108 9-109 9-111 9-112 9-113 9-114 9-115 9-117 9-120 9-121 9-122 9-124 9-126 9-129 9-131 9-135 9-137 9-139 9-141 9-144 9-145 9-146 9-148

Contents

DPD . . . . . DRMH1 . . . DRMH2 . . . DRMH3 . . . DRMS1 . . . DSABO . . . DSAD . . . . DSADJ . . . . DSAE . . . . DSAF . . . . DSAH . . . . DSAJ . . . . DSAL . . . . DSAM . . . . DSAN . . . . DSAP . . . . DSAPRT . . DSAR . . . . DSARLP . . DSARME . DSARMG . . DSARSN . . DSAW . . . . DSDVRG . . DSFLTE . . DSFLTF . . DSMA . . . . DSPRM . . . DSTA . . . . . DSTAP2 . . DSVG1 . . . . DSVG1P . . DSVG2 . . . DSVG3 . . . DSVGP4 . . DSVGP5 . . DTIIN . . . . DUMMOD1 DUMMOD2 DUMMOD3 DUMMOD4 DVIEWP . . DYNREDU EFFMAS . . ELFDR . . . ELTPRT . . . EMA . . . . . EMAKFR . EMC . . . . . EMG . . . . . EMR . . . . . EQUIVX . . ESTINDX . EXTSEIDS

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9-148 9-151 9-152 9-153 9-154 9-156 9-158 9-163 9-165 9-166 9-168 9-170 9-171 9-173 9-174 9-175 9-176 9-177 9-179 9-180 9-181 9-181 9-183 9-183 9-184 9-185 9-186 9-187 9-189 9-191 9-192 9-193 9-195 9-196 9-197 9-198 9-199 9-200 9-200 9-201 9-202 9-203 9-204 9-205 9-206 9-207 9-210 9-211 9-212 9-213 9-218 9-219 9-220 9-221

DMAP Programmer’s Guide

7

Contents

FA1 . . . . . . FA2 . . . . . . FBS . . . . . FILE . . . . . FOCOASET FOCODS . . FOCOEL . . FOCOST . . FOELCF . . FOELCS . . FOELCCS . FONOTR . . FORTIO . . FRLG . . . . FRLGEN . . FRQDRV . . FRRD1 . . . FRRD2 . . . FRRDRU . . GENTRAN GETCOL . . GETMKL . GI . . . . . . . GKAM . . . GKAMW . . GLFONOTR GMERGE . GNFM . . . . GP0 . . . . . GP1 . . . . . . GP1EX . . . . GP1LM . . . GP2 . . . . . GP3 . . . . . GP4 . . . . . GP5 . . . . . . GP6 . . . . . . GPARTN . . GPFDR . . . GPFTOTL . GPFXPND . GPJAC . . . GPSP . . . . GPSTR1 . . GPSTR2 . . GPWG . . . . GUST . . . . IFP . . . . . . IFP1 . . . . . IFP3 . . . . . IFP4 . . . . . IFP5 . . . . . IFP6 . . . . . IFP7 . . . . .

8

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DMAP Programmer’s Guide

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9-221 9-223 9-224 9-226 9-227 9-228 9-228 9-230 9-231 9-232 9-233 9-234 9-235 9-236 9-238 9-239 9-239 9-242 9-243 9-245 9-246 9-247 9-247 9-248 9-250 9-253 9-253 9-254 9-255 9-257 9-259 9-259 9-260 9-261 9-262 9-265 9-266 9-267 9-268 9-271 9-272 9-272 9-273 9-275 9-276 9-277 9-278 9-280 9-283 9-284 9-286 9-288 9-289 9-290

Contents

IFP8 . . . . . . IFP9 . . . . . . IFPINDX . . . IFT . . . . . . . INPUTT2 . . INPUTT4 . . INTERR . . . ISHELL . . . LAMX . . . . . LANCZOS . . LCGEN . . . . LMATPRT . . LRFORCE . . MACOFP . . MAKAEFA . MAKAEFS . MAKAEMON MAKCOMP . MAKENEW . MAKEOLD . . MAKETR . . MAKMON . . MATGEN . . . MATGPR . . . MATINIT . . MATMOD . . MATPCH . . MATPRN . . MATPRT . . . MATREDU . MCE1 . . . . . MCE2 . . . . . MDATA . . . . MDCASE . . MERGE . . . MERGEOFP MESSAGE . MGEN . . . . MKCNTRL . . MKCSTMA . . MKSPLINE . MODACC . . . MODEPF . . . MODEPOUT MODEPT . . MODGDN . . MODGM2 . . MODGM4 . . MODTRK . . MODTRL . . MODUSET . MONVEC . . MPP . . . . . . MPYAD . . . .

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9-291 9-292 9-293 9-294 9-294 9-296 9-298 9-299 9-301 9-305 9-307 9-308 9-309 9-310 9-311 9-312 9-313 9-314 9-314 9-316 9-318 9-319 9-320 9-332 9-336 9-337 9-385 9-387 9-388 9-388 9-390 9-390 9-391 9-392 9-395 9-399 9-400 9-400 9-401 9-402 9-403 9-403 9-405 9-408 9-410 9-410 9-411 9-412 9-414 9-415 9-417 9-419 9-419 9-421

DMAP Programmer’s Guide

9

Contents

MRGCOMP . MRGMON . . MSGHAN . . MSGSTRES . MTRXIN . . . NASSETS . . NLCOMB . . NLITER . . . NLTRD . . . . NLTRD2 . . . NORM . . . . NXNADAMS NXNMATLB . NXNRFI . . . OFP . . . . . . OPTGP0 . . . ORTHOG . . OUTPRT . . . OUTPUT2 . . OUTPUT4 . . PARAM . . . . PARAML . . . PARTN . . . . PCOMB . . . . PCOPY . . . . PLOT . . . . . PLTHBDY . . PLTSET . . . PRESOL . . . PROJVER . . PRTMSG . . . PRTPARM . . PURGEX . . . PVT . . . . . . RANDOM . . RBMG3 . . . . RBMG4 . . . . READ . . . . . RESTART . . RMAXMIN . . RMG2 . . . . . ROTCDA . . . ROTCZG . . . ROTUTL . . . RSPEC . . . . SCALAR . . . SDP . . . . . . SDR1 . . . . . . SDR2 . . . . . . SDR3 . . . . . SDRCOMP . SDREE . . . . SDRHT . . . . SDRNL . . . .

10

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DMAP Programmer’s Guide

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9-426 9-427 9-427 9-428 9-428 9-433 9-434 9-435 9-441 9-444 9-448 9-450 9-451 9-452 9-454 9-456 9-457 9-458 9-462 9-470 9-476 9-478 9-496 9-500 9-501 9-502 9-504 9-504 9-506 9-507 9-508 9-508 9-510 9-510 9-511 9-515 9-516 9-517 9-524 9-525 9-527 9-528 9-530 9-531 9-532 9-533 9-534 9-536 9-538 9-543 9-544 9-545 9-546 9-547

Contents

SDRP . . . . SDRX . . . . SDRXD . . . SDSA . . . . SDSB . . . . SDSC . . . . SECONVRT SEDR . . . . SEDRDR . . SELA . . . . SEMA . . . . SEP1 . . . . SEP1X . . . SEP2 . . . . SEP2CT . . SEP2DR . . SEP2X . . . SEP3 . . . . SEP4 . . . . SEPDIS . . . SEPLOT . . SEPR1 . . . SEQP . . . . SETMON . . SHPCAS . . SMA3 . . . . SMPYAD . . SOLVE . . . SOLVIT . . . SSG1 . . . . . SSG2 . . . . . SSG3 . . . . SSG4 . . . . STATICS . . STDCON . . STRSORT . TA1 . . . . . . TABEDIT . TABPRT . . TABPT . . . TAFF . . . . TAHT . . . . TASNP1 . . TASNP2 . . TIMETEST TOLAPP . . TRD1 . . . . TRD2 . . . . TRLG . . . . TRNSP . . . TYPE . . . . UEIGL . . . UGVADD . UMERGE .

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DMAP Programmer’s Guide

9-549 9-551 9-553 9-554 9-555 9-556 9-557 9-558 9-560 9-562 9-563 9-565 9-566 9-568 9-570 9-570 9-574 9-575 9-576 9-578 9-578 9-580 9-581 9-586 9-586 9-587 9-588 9-589 9-591 9-597 9-599 9-600 9-602 9-603 9-605 9-606 9-607 9-610 9-614 9-622 9-623 9-624 9-625 9-625 9-627 9-631 9-633 9-635 9-637 9-640 9-640 9-643 9-645 9-646

11

Contents

UMERGE1 UPARTN . . UREDUC . VDR . . . . . VDRE . . . . VDRMC . . . VDRPC . . . VEC . . . . . VECPLOT . VIEW . . . . VIEWP . . . WEIGHT . . XSELOADS XSORT . . . XYPLOT . . XYTRAN . .

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DMAP Programmer’s Guide

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•

Introduction to DMAP

•

The NX Nastran DMAP Language

•

Parameters

•

Data Blocks

•

Instructions

•

“Output from a Previous Module” Rule

•

Automatic Deletion of Scratch Data Blocks

•

Preface Modules and SOLution 100

•

Processing of User Errors

•

SubDMAPs DBMGR, DBSTORE, and DBFETCH

•

WHERE and CONVERT Clauses

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1.1 Introduction to DMAP NX Nastran Direct Matrix Abstraction Program (DMAP) is a high-level language with its own compiler and grammatical rules. This section provides a summary description of the NX Nastran DMAP language, rules, and syntax. A DMAP program consists of a series of functional blocks called “modules,” each of which has a unique name and a specific function. Modules are executed sequentially; branching and looping operations are performed by DMAP control statements. Modules communicate through the NX Nastran Executive System (NES) via logical collections of data called “data blocks” and “parameters.” Data blocks come in two distinct forms: “matrices” that obey the rules of matrix algebra, and “tables” that represent a convenient collection of data items. Data blocks are given arbitrary names (Siemens PLM Software recommends mnemonic names) and have header and trailer information defining their characteristics. Parameters are scalar items used for specifying control, operation, or system characteristics. Modules can use “input parameters,” “output parameters,” or both. Input parameters affect the internal operation of the modules. Output parameters are used to control DMAP logic and/or to pass scalar information to subsequent modules. Data blocks and parameters can be written onto either scratch or permanent physical files. When the normal NX Nastran execution completes, data blocks and parameters written to scratch files are erased, and those written to the permanent physical file are available for future use. The NX Nastran Data Definition Language (NDDL) designates whether a data block is scratch or permanent. A detailed description of the NDDL statements can be found in “NASTRAN Data Definition Language (NDDL)” . NX Nastran provides a variety of prewritten solution sequences. These solution sequences consist of a series of DMAP statements. You can use DMAP to modify these prewritten solution sequences or to write your own solution sequences. The compilation, linkage, and execution of a DMAP program is specified by executive control statements in the input file. The creation of and access to databases is specified by file management statements also contained in the input file. File management statements are described in the “File Management Statements” in the NX Nastran Quick Reference Guide .

1.2 The NX Nastran DMAP Language The basic components, or objects, of the DMAP language are: Parameters

Scalar quantities used to control the flow of DMAP execution and to communicate options and/or values to modules or functions.

Data Blocks

Tables or matrices represented by a symbolic name.

Instructions

Statements or modules that process parameters and/or data blocks as input and/or output.

The basic syntax of the DMAP language is: •

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The DMAP language uses free-field input format and is case insensitive.

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•

A physical entry consists of information in columns 1 through 72. Columns 73 through 80 can be used for comments, but these columns do not appear in the printed listing and are not stored on the database.

•

For the specification of modules or statements, a parent entry continues to a subsequent entry if it terminates in a comma [ , ] or a slash [ / ], or if it is missing a right parenthesis [ ) ].

•

The dollar sign [ $ ] ends any DMAP instruction and causes all subsequent data to be treated as commentary. Siemens PLM Software recommends following the convention of terminating all DMAP instructions with a dollar sign.

•

DMAP symbolic names are used to identify variable parameters, data blocks, DBVIEW view-names, subDMAPs, or LABEL statements. A symbolic name is composed of alphanumeric characters and is 1 to 8 characters in length. The following characters are allowed: A through Z, and 0 through 9. The first character must be a character from A through Z.

1.3 Parameters Parameters can be either constants, variables, or expressions and can represent one of several types: Type

Description

Example(s)

Integer

Whole number

10 or -4

Real

Decimal number that is a whole number and a decimal point, with an optional decimal fraction.

27000. or 2.7E5 or 2.7D5

Complex

A pair of real numbers representing the real and imaginary parts of a complex quantity

(1.1,2.3) or (1.D0,3.5D1)

Logical

Represents either TRUE or FALSE

TRUE or FALSE

Character

A string of 1 to 80 characters

’GEORGE’

Also, the real and complex types are either single or double precision. The following table indicates the storage units required as a function of data type. One storage unit is the basic word size on a computer. Typically, a word is 32 bits long on a short-word computer and 64 bits on a long-word computer. Type

Number of words

Integer

1

Real single precision

1

Real double precision

2

Complex single precision

2

Complex double precision

4

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Type

Number of words

Logical

1

Character

1 to 20

The type of a parameter must be declared in at least one of three ways: Constant

Inherent in its specification or construction

Explicit

On a TYPE statement for variable parameters

Implicit

In a module’s parameter list for variable parameters

Constant Parameters A constant represents a fixed value and is a number (integer, real, or complex), logical, or character string. Integer Constants An integer constant is a whole number with no decimal point. Its form is: snn

where: s

=

a sign, plus (+) or minus (-)

nn

=

a string of digits (0 through 9)

s is optional if the sign is positive (+). A minus sign must be used to indicate a negative integer constant. The absolute value of an integer constant cannot be greater than 231 − 1 = 214748367. Real Constants A real constant is a whole number with a decimal point that can be followed by a decimal fraction and/or a decimal exponent. The complete form is: snn.ddEsee

For single precision

snn.ddDsee

For double precision

where: s

=

A sign, plus (+) or minus (-)

nn, dd, ee

=

Strings of digits (0 through 9)

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E or D

=

That snn.dd is multiplied by ee raised to the power of 10. E indicates single precision, and D indicates double precision.

s is optional if the sign is positive (+). A minus sign (-) indicates a negative real constant or negative exponent. D is required to specify double precision. E is optional if no exponent is required and the constant is single precision. However, if either E or D is specified, an integer must follow, even if the exponent is 0. Only the leftmost 14 digits in nn.dd are used by NX Nastran. Leading zeros are ignored in counting the leftmost 14 digits. Complex Constants A complex constant is a pair of real constants separated by a comma and enclosed in parentheses. The first real constant represents the real part of the complex number, and the second real constant represents the imaginary part. Logical Constants A logical constant is specified as TRUE or FALSE. Character Constants A character constant is a string of 1 through 80 characters that can have embedded blanks. A character constant must also be enclosed by right hand single quotation marks.

Variable Parameters A variable parameter is represented by a symbolic name, and its value can change during the DMAP execution. The name of a variable parameter does not have to be unique with respect to symbolic names for modules, data blocks, subDMAPs, or LABELs. The name of a variable parameter cannot be NOT, AND, XOR, OR, or EQV. Variable parameters can have their attributes (type, authorization, and default) set explicitly with a TYPE DMAP statement or implicitly by a module. (Variable parameters that are saved on the database must also be designated as NDDL parameters in the TYPE DMAP statement.) Variable parameters that are not specified with a TYPE DMAP statement use the attributes from the DMAP instruction where the parameter first appears. Value of a Variable Parameter During a DMAP execution or when restarting a DMAP from the database, the value of a variable parameter is determined by the first applicable value on the following sequential list: 1. Value from the most recently executed assignment DMAP statement or the most recently executed save function (S,N prefix. See “DMAP Modules and Statements”). 2. Value from the PARAM Bulk Data entry, if the parameter NAME has the Y authorization. 3. Value saved on the database, if the parameter NAME is listed with an NDDL TYPE DMAP statement and the run is a restart.

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4. Value from the NAME=v, if present in a non-NDDL parameter TYPE instruction. This value is determined at DMAP compile time from the TYPE instruction (regardless of its location in DMAP) that contains the statement. 5. Default value from the NDDL, if the NDDL keyword is specified on the TYPE DMAP statement. Parameters listed in the NDDL always have a default value of zero, blank, or FALSE, unless a value is explicitly given in the PARAM NDDL statement. 6. Default value from the first occurrence of either a non-NDDL TYPE DMAP statement or a module with a MPL default value. Non-NDDL TYPE DMAP statements have a default value of zero, blank, or FALSE for real or integer, character, or logical parameters. 7. Default value is zero, blank, or FALSE for real or integer, character, or logical parameters. Determining the current value of a variable parameter is summarized in the following table. NDDL

TYPEd

Not TYPEd

Last executed assignment statement or module save (S,N,). The qualifier values for NDDL parameters cannot change. Bulk Data PARAM entry override, if the parameter is type Y and has not been previously reassigned in an assignment (=) statement (unless the PVT module has been executed to reset the Bulk Data and Case Control PARAM entries). Value on the data base

name=vfrom its first occurrence in a TYPE statement

NDDL default value

TYPE statement default

MPL default of parameter first occurrence

Predefined Variable Parameters The program predefines the value of some variable parameters. It is not necessary to type these parameters with a TYPE DMAP statement, nor is it possible to change their type. Siemens PLM Software does not recommend changing these parameter values. The predefined variable parameters are: NAME

TYPE

VALUE

ALWAYS

-1

Integer

NEVER

+1

Integer

TRUE

TRUE

Logical

FALSE

FALSE

Logical

NOGO

0

Integer

Initial values for variable parameters can be specified using the PARAM Bulk Data entry or the PARAM Case Control command.

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Parameter values from the Bulk Data Section are brought into the DMAP sequence via the IFP module. Parameter values from case control are brought into the DMAP sequence via the PVT module. The PVT module reads the case control PARAM commands and resolves parameter values specified in both the Case Control and Bulk Data Sections. Recommended Parameter Type Specification Follow these recommendations to produce a more readable DMAP sequence where all Y parameters and parameters with non-MPL defaults are specified on TYPE statements. •

If the parameter’s value is to be specified in the Case Control or Bulk Data Section, type the parameter near the top of the DMAP sequence, as shown below. TYPE PARM,,type,Y,param_name $

•

If the parameter’s default value is defined on the NDDL PARAM statement and you want to use the NDDL default value, type the parameter near the top of the DMAP sequence, as shown below. TYPE PARM,NDDL,type,Y,param_name $

•

If the desired default value differs from the MPL default, specify the parameter and the default value on a TYPE statement, as shown below. TYPE PARM,,type,Y,param_name=default_value $

•

Specify in module instructions, as needed, "/param_name/" or "/S,N,param_name/”.

•

Do not use the following obsolete parameter prefix specifications in module instructions: /V,Y,param_name/ /S,Y,param_name/ /V,N,param_name/ /C,Y,param_name/ /C,N,param_name/

For example, Siemens PLM Software recommends the following sequence for setting the TYPE of ALPHA: TYPE PARM,,CS,Y,ALPHA=(1.,1.) $ TYPE PARM,,CS,N,ALPHAX $ . . . ALPHAX=ALPHA $ IF( FLAG ) ALPHAX=CMPLX(BETA,GAMMA) $ . . . ADD

A,B/C/ALPHAX $

Siemens PLM Software does not recommend the following: IF( FLAG ) PARAMR

//’COMPLEX’//BETA/GAMMA/S,Y,ALPHA $

. . .

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ADD

A,B/C/V,Y,ALPHA=(1.,1.) $

Expressions and Operators An expression represents a single value and consists of one or more constant and/or variable parameters separated by operators. Expressions are classified as arithmetic, relational, logical, or character. Arithmetic expressions produce numerical values; relational and logical expressions produce logical values. An expression can contain intrinsic functions. An expression is specified: •

In the right-hand side of an assignment (=) statement

•

As arguments for intrinsic functions

•

As logical expressions in control statements: DO WHILE, IF, IF-THEN, ELSE IF-THEN

•

As logical expressions in the WHERE clause of DBVIEW, DBEQUIV, and DBDELETE statements

Arithmetic Operators The allowable arithmetic operations are shown in the table below in the order of execution precedence. Parentheses are used to change the order of precedence. Operations within parentheses are performed first, with the usual order of precedence being maintained within the parentheses. Operator

Operation

Sample expressions

Interpreted as

–,+

Negative or Positive immediately preceded by exponentiation

X–Y

X(–Y)

**

Exponentiation

–X**Y

–(X**Y)

–,+

Negative or Positive

–X – Y

(–X) – Y

*, /

Multiplication or Division

X*Y+Z

(X*Y)+Z

+,–

Addition or Subtraction

X+Y

X+Y

In general, mixed mode expressions are not supported. For example, to compute A = B*C, where A and B are complex, but C is real, it is necessary to convert C to a complex number: A = B*CMPLX (C), where CMPLX is described under “Intrinsic Functions” in this section. Character Operator The only character operation is concatenation. Its form is shown below. Operator &

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Operation Concatenation

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Sample expressions ‘ABC’ & ‘DE’ = ‘ABCDE’

Direct Matrix Abstraction

Relational Operators Relational operators are used to compare two expressions. The result of the comparison is a logical TRUE or FALSE. When arithmetic and relational operators are combined in one expression, the arithmetic operations are performed first. The table below shows the allowable relational operators. Operator

Relation tested

Expression

=

Equality

X=Y

,><

Inequality

XY, X>Y

≤

Less than or equal

X≤Y

≥

Greater than or equal

X≥Y

Logical Operators Logical operators perform tests on multiple relations or Boolean operations. A logical operator returns a result that is either TRUE or FALSE. The outcome of a logical operation is determined as shown in the table below. These outcomes are listed in order of precedence. Parentheses are used to change the order of precedence. Operations within parentheses are performed first, with the usual order of precedence being maintained within the parentheses. X

Operator NOT

X AND Y

X OR Y

Y

Output

TRUE

n/a

FALSE

FALSE

n/a

TRUE

TRUE

TRUE

TRUE

TRUE

FALSE

FALSE

FALSE

TRUE

FALSE

FALSE

FALSE

FALSE

TRUE

TRUE

TRUE

TRUE

FALSE

TRUE

FALSE

TRUE

TRUE

FALSE

FALSE

FALSE

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X

Operator X XOR Y

X EQV Y

Y

Output

TRUE

TRUE

FALSE

TRUE

FALSE

TRUE

FALSE

TRUE

TRUE

FALSE

FALSE

FALSE

TRUE

TRUE

TRUE

TRUE

FALSE

FALSE

FALSE

TRUE

FALSE

FALSE

FALSE

TRUE

1.4 Data Blocks A data block is a table or matrix represented by a symbolic name. All data blocks are comprised of records. Each record can contain a variable number of words. The first record ("Record 0") is called the header record, of which the first two words (when concatenated) form the name of the data block. The third and subsequent words are not usually used. The subsequent records are sometimes called "data records." For tables, the data record can contain a mixture of any type of data; for example, real, integer, complex, character, and so on. For matrices, the data record corresponds to the nonzero values in the column of the matrix; for example, record 3 corresponds to the nonzero values in column 3. The last record is called the trailer record and contains summary information about the table or matrix.

Table trailers In tables, the trailer record contains six words. The contents vary among the tables and are described in “Data Blocks” at the end of the table’s description. Table trailers are printed when DIAG 15 is specified in the Executive Control or DIAGON(15) is specified in the DMAP sequence.

Matrix trailers In matrices, the characteristics of a matrix are described in a twelve-word matrix trailer. Matrix trailers are printed when DIAG 8 is present in the Executive Control Section DIAGON(8) or is specified in the DMAP sequence. The contents of a matrix trailer are as follows: Word

Contents

1

Number of columns in matrix

2

Number of rows in matrix

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Word

Contents

3

Form of the matrix

4

Type of matrix

5

Largest number of nonzero words among all columns

6

Density of the matrix multiplied by 10000

7

Size in blocks

8

Maximum string length over all strings

9

Number of strings

10

Average bandwidth

11

Maximum bandwidth

12

Number of null columns

Form is defined as one of the following: Form

Meaning

1

Square

2

Rectangular

3

Diagonal

4

Lower triangular factor

5

Upper triangular factor

6

Symmetric

8

Identity

9

Pseudo identity

10

Cholesky factor

11

Trapezoidal factor

13

Sparse lower triangular factor

15

Sparse upper triangular factor

Type is defined as one of the following:

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Type

Meaning

1

Real, single precision

2

Real, double precision

3

Complex, single precision

4

Complex, double precision

Data Block Type and Status The data block type depends on whether the data block is stored on a permanent or scratch DBset and whether its name appears on a TYPE DB statement. A DBset is a physical file that is a subdivision of the database (see the NX Nastran User’s Guide). There are three types of DMAP data blocks: Permanent NDDL

Referenced on a TYPE DB statement and assigned to a permanent DBset through the NDDL

Scratch NDDL

Referenced on a TYPE DB statement and assigned to the SCRATCH DBset through the NDDL

Local

Not referenced on a TYPE DB statement and automatically assigned to the SCRATCH DBset.

At any point during a DMAP execution a data block is in one of the three following states: Generated

The data block has been created

Not generated

The data block has been deleted or is not yet created

Empty

The data block has been created but has no data (or purged). In other words, the name of the data block is stored on a permanent DBset without any associated data.

Permanent blocks can have all states: generated, not generated, and empty. Empty data blocks are created when a module is executed, but no data is actually generated for the data block. For example, the ADD module has two inputs; if both inputs do not exist (not generated), the output is empty or purged. Empty data blocks are required to support automatic restarts. A permanent data block can be explicitly purged with the PURGEX statement. Permanent data blocks can be deleted from the database with the DELETE statement. Scratch data blocks can have only two states: generated and not generated. These data blocks can be deleted with the DELETE or PURGEX statements.

1.5 Instructions A DMAP instruction can be classified as either a module or a statement. A module is similar to a "macro" function and, in general, processes data blocks as input and/or output. A module

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can also have parameters as input and/or output. A statement is any instruction that is not a module and that does not operate on data blocks.

Modules A module instruction has the following form: the name of the module followed by a comma [,] and a list of input data block names separated by commas, a slash [/], a list of output data block names separated by commas, a slash, and a list of parameter (variable names or constants) separated by slashes: module_name ,

input_data_block_list / output_data_block_list / parameter_list $

The dollar sign [$] is required to terminate the module instruction. The modules are described in “Descriptions of DMAP Modules and Statements”. Most modules have a prescribed number of inputs, outputs, and parameters, which are defined in the Module Property List (MPL). The MPL is an internal NX Nastran table that prescribes the exact format of all modules; the number of input and output data block lists and the number, type, and default of the parameters in the parameter list. The MPL can be listed by specifying DIAG 31 in the Executive Control Section. The position of the data block and parameter names is critical to the proper execution of the module. Below is an example using the MPYAD module, which performs the following matrix operation: [D] = SIGNAB*[A][B] + SIGNC*[C] or [D] = SIGNAB*[A] T [B] + SIGNC*[C] where [A], [B], [C] and [D] represent matrices, and SIGNAB and SIGNC represent the sign to be applied to the product and additive matrices, respectively. The format of the MPYAD module is: MPYAD ,

A , B , C / D / T / SIGNAB / SIGNC / PREC / FORM $

where A, B, and C, represent the input data block names, D represents the output data block name, and T, SIGNAB, SIGNC, PREC, and FORM represent the parameter names. The MPL listing for the MPYAD and PARAML modules appears below:

Listing 1-1. Module Properties List.

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The MPL listing contains useful information under the following column headers: Header

Description

MOD-NAME

Module name

IN

Number of input data blocks

OUT

Number of output data blocks

ID

Parameter position

TYP

type of parameter: INT - integer RSP - real single precision RDP - real double precision CSP - complex single precision CDP - complex double precision BCD - character LOG - logical

DEFAULT

Default value of parameter

The other column headers are less important to the DMAP programmer. Some or all data blocks and parameters can be left unspecified (or purged), according to the module description in “Descriptions of DMAP Modules and Statements”. If a parameter is unspecified, the default value is assumed and obtained from the MPL. For example, MPYAD

A , B , / D $

According to the MPYAD module description, if C is unspecified, only the matrix multiplication of A and B is performed. Also, by default, T=0 and therefore A is not transposed. SIGNAB and SIGNC parameters are defaulted to 1 resulting in: [D] = [A][B]

However, if no default is defined in the MPL, a constant or variable parameter must be specified for the first parameter. For example, -- NO DEFAULT --

on the PARAML module indicates that there is no default value for the first parameter. The first comma after the module name can be omitted as long as the first input data block name is specified. For example, the ELTPRT module has the following format: ELTPRT

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ECT,GPECT,BGPDT,UNUSED4,EST,CSTM,MPT,DIT,CASECC/ VELEM/PROUT/S,N,ERROR $

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To obtain a printout of the elements connected to each grid point, only GPECT and BGPDTS need to be specified. However, a comma must also be specified after the module name: ELTPRT ,

,GPECT,BGPDTS,,,,,,/ $

In addition, trailing commas can be left unspecified: ELTPRT ,

,GPECT,BGPDTS,,,,,,/ $

Parameters can be specified on a module as: •

Input only

•

Input and output

•

Output only

Each module has its own rules for parameter specification, as described in “Descriptions of DMAP Modules and Statements”. If a parameter is specified as input, either a constant or variable can be specified. Note that character strings or variables specified for parameters are limited to eight characters in length. For example, the first parameter of the ADD module specifies a scalar multiplier of 1+2i on the first input matrix: ADD

A , B / C / (1.,2.) $

or ALPHA: ADD

A , B / C / ALPHA $

If a parameter is to be used as both input and output, or output only, a variable name must be specified and preceded by S, N. For example, on the PARAML module, the fourth parameter, TERM, is an output parameter: PARAML

A // ’DMI’ / 4 / 7 / S, N, TERM $

TERM is the value of matrix A at column 4 and row 7, which is returned by the PARAM module for later use in the DMAP program. If the S,N prefix is omitted, TERM is assumed to be input only, no fatal message is issued, and the TERM value is incorrect.

Statements A statement is any instruction that is not a module and that typically does not produce output data blocks from input data blocks or parameters. Another distinction is that a statement has no definition in the MPL (Module Property List). The different types of statements are: •

Assignment (=)

•

Function

•

Control

•

Declarative

•

Database Function

Assignment Statement The assignment statement evaluates an expression and assigns the resulting value to a variable parameter. This statement has the following form:

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v = e $

where v is a variable parameter name, and e is an expression. The dollar sign [$] is required to terminate the statement. Assignment statements are arithmetic, logical, or character, depending on the type of the variable parameter. The type of the variable and the expression must be the same. In other words, no mixed mode specification is allowed. Type conversions can be performed with the INT, REAL, CMPLX, ITOL, and LTOI DMAP functions. For character assignment statements, if the length of the expression does not match the size of the variable, the expression is adjusted as follows: •

If the expression is shorter than the variable, the expression is padded with enough blanks on the right before the assignment takes place to make the sizes equal.

•

If the expression is longer than the variable, characters on the right are truncated to make the sizes the same.

Function Statement Functions can appear only within an arithmetic or logical expression; they cannot be referenced within module or CALL statements. Execution of the function causes the evaluation of the function and returns a value to the referencing expression. Some functions, however, can appear as a DMAP statement without appearing in an arithmetic or logical expression. These functions are DIAGON, DIAGOFF, NOOP, PUTSYS, PUTDIAG, RDIAGOFF, and RDIAGON. The type of the value returned from a function is dependent on the type of the argument(s) supplied, in addition to the functional operation. In general, the precision (single, double) and form (integer, real, complex) of the result returned by the function carries at least as much information as the arguments supplied. For example, ACOS(X) is typed as follows: X

ACOS(X)

I

RS

RS

RS

RD

RD

CS

CS

CD

CD

Returned values for character functions can be processor dependent. The following table shows the complete function library. The abbreviations in the far right column signify types: Type

Abbreviation I

Integer

R, RS, or RD

Real

C, CS, or CD

Complex

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Type

Abbreviation A

Character

L

Logical Format

ABS(x)

Definition absolute value

Result

Argument type to result type I to IR and C to R

|x| if x is I or R if x = a + ib

ACOS(x)

arccosine

,

cos−1(x) where −1 ≤ x ≤ 1, if x is I or R

I and R to CC to C

The result is computed in radians. ACOSH(x)

hyperbolic arccosine

cosh−1(x)x ≥ 1

I and R to RC to C

For real and integer arguments, values less than 1 result in errors. ANDL(x, y)

numeric AND

TRUE if x< 0 and y< 0

I, R, and C to L

FALSE otherwise ASIN(x)

arcsin

sin−1(x) where−1 ≤ x ≤ 1, if x is I or R

I and R to RC to C

The result is computed in radians. ASINH(x)

hyperbolic sine

sinh−1(x)

I and R to RC to C

ATAN(x)

arctangent

tan−1(x)

I and R to RC to C

The result is computed in radians. ATAN2(x1, x2)

arctangent of quotient

tan−1(x1/x2)

I and R to RC to C

If both arguments are zero, the result is zero. If x1 and x2 are real and: x1 = 0 and x2 > 0, the result is 0.x1 = 0 and x2 < 0, the result is π.x1 > 0 and x2 = 0, the result is π/2.x1 < 0 and x2 = 0, the result is −π/2. If x1 and x2 are complex (x1 = a + bi and x2 = b + di) and: a = b = 0 and (sign of c) = (sign of d), the result is 0.a = b = 0 and (sign of c) ≠ (sign of d), the result is π. (sign of a) = (sign of b) and c = d = 0, the result is π/2. (sign of a) ≠ (sign of b) and c = d = 0, the result is −π/2. ATANH(x)

hyperbolic arctangent

tan−1(x) where −1 ≤ x≤ 1, if x is I or R

I and R to RC to C

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Format ATANH2(x1, x2)

Definition hyperbolic arctangent of quotient

Result tan−1(x1, x2)

Argument type to result type I and R to RC to C

For real arguments, the following must be true: |x1| > |x2| and x2 ≠ 0. If x1 and x2 are complex (x1 = a + bi and x2 = b + di) and: a = b = 0 and (sign of c) = (sign of d), the result is 0.a = b = 0 and (sign of c) ≠ (sign of d), the result is π. (sign of a) = (sign of b) and c = d = 0, the result is π/2. (sign of a) ≠ (sign of b) and c = d = 0, the result is −π/2. CHAR(x)

character value

See note below.

I to A

The function takes the processor collating sequence equivalent (for example, ASCII or EBCDIC) of a character and converts it to the character value. The integer value must be within the range 1 to n − 1, where n = 2(number of bits per character). CLEN(c)

character length

CLOCK( )

CPU time in sec. since job started

CMPLX(a, b) CMPLX(x)

convert to complex

Character string length in multiples of 4.

A to I

I

a + ib

See below

x, if complex x+i 0, otherwise For real arguments, if one value is specified, the result is (value, 0). The precision of the complex number is dependent on the precision of the argument; for example, integer and real single values create complex single results, and real double values create complex double results. For complex arguments only one value can be specified. The result is the value and type of the argument. Integer, real single, and real double values are allowed with two arguments only. The results are complex double if either or both arguments are real double. The results are complex single if neither argument is real double. CONCAT1(a1, a2)

full word concatenation

a1 & a2

A to A

CONCAT2(a1, a2)

concatenation

a1 & a2

A to A

Any trailing blanks of a1 are compressed to a single blank before a2 is concatenated. CONCAT3(a1, a2)

concatenation

a1 & a2

A to A

The result is argument 1, with trailing blanks removed and argument 2 concatenated together. CONJG (x)

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complexconjugate

DMAP Programmer’s Guide

a − ib is conjugate to a + ib

C to C

Direct Matrix Abstraction

Format COS(x)

Definition cosine

Result cos(x)

Argument type to result type I,R to R, C to C

The angle must be in radians. COSH(x)

hyperbolic cosine

cosh(x)

I,R to R, C to C

The angle must be in radians. DBLE(x)

convert to double precision

I to RD, R to RDC to CD

Integer and real single values are converted to real double values. Real double values are not changed. Complex single values are converted to complex double values Complex double values are not changed. DIAGOFF(x1, ..)

turn off DIAG

TRUE if 0 < x1...xn x2

Argument type to result type I,R,C to L

FALSE, if x1 ≤ x2 NUMLE(x1,x2)

less than or equal to

TRUE if x1 ≤ x2

I,R,C to L

FALSE otherwise NUMLT(x1,x2)

less than

TRUE, if x1 < x2

I,R,C to L

FALSE otherwise NUMNE(x1,x2)

not equal to

TRUE, if x1 ≠ x2

I,R,C to L

FALSE otherwise ORL(x1,x2)

numeric or

TRUE, if x1 0. Use last RAND(x) as seed if x=0. If x0, and y 0−|x1|, if x2 < 0

I to I, R to R

Resultant type determined by first argument. sine

SIN(x)

sin(x)

I,R to R, C to C

The angles are given in radians. SINH(x)

hyperbolic sine

sinh(x)

I,R to R, C to C

The angles are given in radians. SNGL(x)

convert to single

SPROD(x1,x2)

single prec product

I,R to RS, C to CS x1 * x2

RD to RS, CD to CS

The results are real single if both arguments are real double and complex single if at least one of the arguments is complex double. SQRT(x)

square root

I,R to R, C to C

If the value of integer or real arguments is less than 0, an error results. For complex arguments the principal square root is returned. That is, the first component is always greater than or equal to 0. SUBSTRIN(A,x1,x2)

substring

SUBSTRIN (¢ABC¢, 2, 3) ® ¢BC¢

x1,x2 can be I, R or C

Return substring of first argument with length of ABS(x2-x1)+1. Arguments 2 and 3 must be numeric values. Prior to use as substring subscripts, both arguments are converted to integers and checked for range of 1 to 80. If the lower string subscript is less than 1, it is changed to 1. If the upper string subscript is greater than 80, it is changed to 80. The larger string subscript value becomes the upper substring subscript.

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Format

Definition

Result

Argument type to result type

TAN(x)

tangent

tan(x)

I,R to R, C to C

TANH(x)

hyperbolic tangent

tanh(x)

I,R to R, C to C

TIMETOGO()

remaining CPU Time

returns I

Returns the remaining CPU time in integer seconds. Time remaining is found by subtracting the current CPU time from the value on the TIME executive control statement. WLEN(x)

VPS word length

Returns VPS word length of argument

A,I,R,C,L to I

Returns VPS word length of argument. Constant for all types, except character data that ranges from 1-20. XORL(x1,x2)

numeric exclusive OR

TRUE, if x1 or x2 < 0

I,R,C to L

FALSE otherwise

PUTDIAG, GETDIAG In the PUTDIAG and GETDIAG examples below, DVALUE is an integer whose 32 bits from left to right represent 32 DIAG values. DVALUE=GETDIAG(DWORD) $ PUTDIAG(DVALUE,DWORD) $

DWORD=1 represents the 1st through 32nd DIAG settings and DWORD=2, the 33rd through 64th DIAG settings. GETDIAG and PUTDIAG are best used in pairs. For example, to turn on DIAG 8 temporarily and restore the original DIAG 8 setting, the following sequence can be used: TYPE PARM,,I,,DIAG32 $ DIAG32=GETDIAG(1) $ DIAGON(8) $ DIAG 8 WILL BE ON HERE REGARDLESS OF SETTING IN $ EXEC. CONTROL . . . PUTDIAG(DIAG32,1) $ RESTORE DIAGs TO THEIR ORIGINAL VALUE

PUTSYS, GETSYS System cell values can be set and recovered via the PUTSYS and GETSYS DMAP functions. See “nastran Command and NASTRAN Statement” in the NX Nastran Quick Reference Guide for a description of various system cells. System cells 253 through 262 are reserved for the DMAP writer. This permits the DMAP writer to pass parameter values in via the NASTRAN statement or between subDMAPs. For example, NASTRAN SYSTEM(253)=4 SOL MYDMAP COMPILE MYDMAP SUBDMAP MYDMAP $ TYPE PARM,,I,N,NP $ . . .

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IF ( GETSYS(NP,253)4 ) THEN $ . . . ENDIF $

Control Statement The NX Nastran DMAP language contains control statements that perform conditional branching and looping similar to those found in the FORTRAN programming language. The control statements are: Conditional Execution

IF

Unconditional Branching

JUMP and LABEL

Conditional Branching

IF()THEN, ELSE IF()THEN, ELSE, and ENDIF

Looping

DO WHILE and ENDDO

Calling SubDMAP Operations

SUBDMAP, CALL, and RETURN

Termination

EXIT and END

Conditional Execution—IF Statement The IF statement conditionally executes a single DMAP instruction: IF ( logical expression ) instruction $

In other words, if the logical expression is true, the instruction is executed. Instruction is any DMAP module or statement, except a control statement or the FILE, DBVIEW, TYPE and SUBDMAP statements. Examples include: IF ( NOGOA=-1 ) ADD GOAT,GOAQ/GOA $ IF ( ERRFLAG 2 AND SElD > 0) selects all items under version 4 for all values of SEID greater than 0 except 2. A simple where-expr is a comparison using the following relational operators = , > ‘ < ‘ ≤, ≥, or utortu. For example, SElD > 0 means if SEID is greater than zero, the logical expression is true. Several simple where expressions can be joined into one where expression by the following logical operators: AND, OR, XOR, and EQV. The NOT operator can be used to negate a where expression. For example, NOT(SEID>0) is the same as SEID≥0. Arithmetic operations and DMAP functions can also be specified in the where expression (see “Expressions and Operators”). If a qualifier in a where-expr is not a qualifier in the path of a specified item, the where-expr is set to FALSE. If the where-expr does not contain a specification for all qualifiers in the path of an item, the unspecified qualifiers are wildcarded. (For example, in the statement quali= * , all values are selected.) The default values of qualifiers, PROJECT, VERSION, and DBSET are described under the statement in which the WHERE clause is specified. Examples of the WHERE clause are: 1. Select all items in the database for all superelements except 10 and 30 from Version 1. WHERE (VERSION=1 AND SEID≥0 AND NOT(SEID=10 OR SEID=30)) 2. Select all entries in database on DBSET=DBALL from all projects and versions.

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WHERE(PROJECT=PROJECT AND VERSlON>0 AND DBSET=’DBALL’) The CONVERT clause modifies project- and version-ID, DBset-name (see “INIT” in the NX Nastran Quick Reference Guide), and qualifier values of items selected by the WHERE clause on the DBLOCATE and DBLOAD statements. The CONVERT clause contains one or more assignment statements separated by semicolons. The format of the CONVERT clause is: CONVERT(PROJECT=project-expr; VERSION=version-expr; , DBSET=DBset-expr;quali=qual-expri[;...]) The PROJECT and VERSION statements modify the project-ID (see “PROJ” in the NX Nastran Quick Reference Guide) and version-ID. The DBSET statement modifies the DBset-name. The value of quali is replaced by qual-expri for selected items that have quali in their path. qual-expri is any valid expression (see “Expressions and Operators” containing constants or any qualifier name defined in the path of the item. If qual-expri contains names of qualifiers not in the path of the selected item, a fatal message is issued. If project-expr and/or version-expr produces a project- or version-ID which does not exist, one is created. Also, all version-lDs less than version-expr that do not exist are created; but they are “empty.” Examples of the CONVERT clause are: •

Set qualifiers SEID, PEID, and SPC to constants 10, 20, 102 respectively.

•

CONVERT(SEID=10;PEID=20;SPC=102)

If more than one value of a qualifier is found for an item by the WHERE clause, each value is processed in qual-expri to define the new qualifier value for each of the selected items. In the example below, if the original values of PEID were 1, 2, and 3; the new values for the SElD qualifier are 2, 4, and 6: •

Set all values of qualifier SElD to be twice the value of the PEID qualifier.

•

CONVERT(SElD=2*PElD)

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Chapter

2

Overview of Data Blocks

•

Introduction

•

Matrix Data Blocks

•

Table Data Blocks

2.1 Introduction Data block descriptions are provided for all matrices and tables that are currently processed by the OUTPUT2 and DBC modules in the NX Nastran solution sequences with PARAM,POST. Data block descriptions are arranged alphabetically by the generic name of the data block. A data block description can encompass descriptions of several data blocks from different modules. For example, the OES data block description describes data blocks OES1, OES2, OESNL, OSTR1, and OES1C which are output by the SDR2, SDR3, SDRNL, and SDRCOMP modules. The generic name of a data block also appears in the “Glossaries” .

2.2 Matrix Data Blocks The rows and columns of most matrices correspond to degree-of-freedom sets which are defined in the USET table. Matrices are usually named according to __rc where r and c are the names of the degree-of-freedom sets for the row and column, respectively. For example, the rows and columns of KFS correspond to the f-set and the s-set. The rows and columns corresponding to degree-of-freedom sets are ordered according to an ascending internal point identification number sequence. This is the same as the external (user-assigned) grid point identification number sequence unless resequencing is requested (PARAM,OLDSEQ,>-1). Some matrices are also named with pseudo-degree-of-freedom set names. W – The set omitted after auto-omit (a-set combines x-set and w-set) X – The set retained after auto-omit (complement of w-set) J – Superelement interior degrees-of-freedom; for example, KJJ and PJ H – Modal degrees-of-freedom; for example, PHDH, MHH, PHF and UHF In some matrices the columns correspond to subcases, normal modes, time steps, or forcing frequencies. These matrices are usually related to loads and solutions and named __r__ where r is the name of the degree-of-freedom set. For example, PG is static loads applied to the g-set and PHA is the a-set eigenvector matrix. In frequency and transient response, an "F" or "T" can also be added to the name. For example, UDF and UDT, are the solution matrices at the d-set for frequency and transient response.

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Overview of Data Blocks

Chapter 2

Analysis type

Columns correspond to ascending

Linear statics

Subcase identification number

Nonlinear statics

Loop identification number

Normal or complex eigenvalues

Mode number

Frequency response

Subcase ID and Forcing frequency value

Transient response

Time step value

In transient response analysis, the columns of the solution matrix U_T correspond to "time step triplets." The first column in the triplet represents displacement, then velocity and acceleration. The triplet is then repeated for each time step. For example, if there are 10 time steps, U_T has 30 columns. If multiple TSTEP command subcases are requested, there is a separate solution matrix for each subcase. The columns of the dynamic load, MPCForce, and SPCForce matrices; P_T, QM_T, and Q_T, correspond to time step and, using the example above, they each have 10 columns. In frequency response analysis, the columns of the dynamic load, MPCForce, SPCForce and solution matrices; P_F, QM_F, Q_F, and U_F, correspond to forcing frequency. If multiple dynamic load (DLOAD) subcases are requested with NFREQ number of forcing frequencies, the first NFREQ columns represent the first DLOAD subcase and NFREQ frequencies, the second NFREQ columns represent the second subcase, and so on. For example, if an analysis is performed with four forcing frequencies and three DLOAD subcases, the solution matrix has 12 columns in which the first 4 columns correspond all forcing frequencies in the first subcase. If multiple FREQUENCY command subcases are requested, there is a separate solution matrix for each subcase. For a description of matrix trailers see “Data Blocks” .

2.3 Table Data Blocks This section discusses common attributes across tables.

IFP Tables The IFP module processes the Bulk Data Section and creates data blocks which contain images of each Bulk Data entry. Modules IFP2 through IFP9, MODEPT, MODGM2, GP0, SEQP, and MODGM4 then create pseudo-images based on the presence of elements used in hydroelastic, axisymmetric, laminated composite, composite beam, acoustic, hyperelastic, beam library and p-version analyses. For example, the IFP6 module converts PCOMP and MAT8 images to MAT2 and PSHELL pseudo-images. All of the tables produced by these modules are also called "IFP Tables." In an IFP Table there is one record written for each image type present in, or derived from, the Bulk Data Section and that record contains all of the images for that type. If the image type is not present, no record is written.

IFP Table Header Words and Trailer Bits The first three words in all IFP Tables uniquely identify or label the contents of the record and are called "header words." The second header word indicates a bit position, called a "trailer bit", in the table trailer. The trailer bit indicates the presence of record type in the data block; that is, if the record is present in the table, the bit is turned on in the trailer.

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There are a total of 176 trailer bits. The first 96 trailer bits correspond to bit positions 1 through 16, numbered from the right, in each trailer word and beginning with trailer word 1. The second 80 trailer bits correspond to bit positions 17 through 32, numbered from the right, in each trailer word and beginning with trailer word 1. The table below shows the correspondence between a trailer bit and its word and bit location in the trailer. Trailer Bit

Location in trailer Word

Position

1 – 16

1

16 – 1

17 – 32

2

16 – 1

33 – 48

3

16 – 1

49 – 64

4

16 – 1

65 – 80

5

16 – 1

81 – 96

6

16 – 1

97 – 112

1

32 – 17

113 – 128

2

32 – 17

129 – 144

3

32 – 17

145 – 160

4

32 – 17

161 – 176

5

32 – 17

For example, the GRID record in the GEOM1 data block is assigned to trailer bit 45 which corresponds to the 4th bit position, numbered from the right, in trailer word 3. Based on the trailer bit, the following FORTRAN statements can be used to determine the corresponding trailer word and bit position: WORD = MOD(TBIT-1,96)/16 + 1 BIT = 16*(1+TBIT/97) - MOD(TBIT-1,16)

where TBIT = trailer bit from the second word of the header record WORD = trailer word BIT = trailer word bit position numbered from the right

and all variables are defined as integers.

OFP Tables The header record of all OFP tables contains codes which indicate how the output should be labeled, formatted, and printed. Word 1

Name approach_code

Contains Analysis type and output device type(s)

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Overview of Data Blocks

Name

Word

Contains

2

table_code

Header, labeling, and sort types

9

format_code

Data types (real or complex)

11

stress_code

Stress/strain, von Mises/max. shear, strain-curvature/strain-fiber flags. Also, SPCForce/MPCForce flag.

12

jflag

Acoustic element output flag

13

iacflg

Acoustic displacement (pressure) output request flag: 2 = Yes and 0 = No.

14

q4cstr

CQUAD4 corner output stress option

21

metrik

Electromagnetic units code (1 thru 6 or 10, default=10)

22

emssol

Electromagnetic static solution code (0=CF+MAG,1=CF,2=ELEC,3=MAGN)

23

thermal

Thermal (heat transfer) element output

Note Note: In some OFP table descriptions (OEE, OEF, OES for example), you will see formats such as ACODE,4=05, or TCODE,1=02 (versus ACODE=05 or TCODE=02). The integer values 4 and 1 in these examples are function codes. Function codes specify operations to perform on the value in the data block. The operation result will then be used to determine the data format. The following lists the available function codes and their operation: Function codes

Operation

1

if (item_name/1000 = 2,3,6) then return 2, else return 1

2

mod(item_name,100)

3

mod(item_name,1000)

4

item_name/10

5

mod(item_name,10)

6

if iand(item_name,8) then set to 0, else set to 1

7

if item_name/1000 = 0 or 2, then set to 0 = 1 or 3, then set to 1

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Overview of Data Blocks

> 3, then set to 2. >65535

iand(item_name,iand(func_code,65535))

For example, if a value of 100 is found in an ACODE,4 field, the function_code of 4 results in the operation item_name/10 = 100/10 = 10. Thus the data format under the ACODE,4=10 row would be used.

Approach_Code Approach_code indicates the analysis type and device type(s). 1. Analysis type is equal to approach_code/10 indicates: Type

Description

1

Statics

2

Normal modes or buckling (real eigenvalues)

3

Differential stiffness 0

4

Differential stiffness 1

5

Frequency

6

Transient

7

Pre-buckling

8

Post-buckling

9

Complex eigenvalues

10

Nonlinear statics

11

Geometric nonlinear statics

2. Device type(s) are extracted from the bit pattern equal to MOD(approach_code,10). The bits numbered from the right are: Bit

Description

1

Print

2

Plot

3

Punch

Therefore, MOD(approach_code,10) can be one of the following values:

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Overview of Data Blocks

Chapter 2

Value

Device type(s)

0

None

1

Print

2

Plot

3

Print and plot

4

Punch

5

Print and punch

6

Plot and punch

7

Print, plot, and punch

Examples: Approach_code

Description

61

Print transient response results

15

Print and punch statics results

106

Plot and punch nonlinear statics results

Table_code Table_code indicates basic table content (displacements, stresses, and so on), data format (Real or complex), and sort type (SORT1 or SORT2). 1. MOD(table_code,1000) indicates table content; displacements, stresses, and so on. Type

2-6

Data Block Description Name

Description

1

OUG

Displacement Vector

2

OPG

Load Vector

3

OQG

SPCforce or MPCforceVector

4

OEF

Element Force (or Flux)

5

OES

Element Stress (or Strain)

6

LAMA

Eigenvalue Summary

7

OUG

Eigenvector

DMAP Programmer’s Guide

Overview of Data Blocks

Type

Data Block Description Name

Description

8

None

Grid Point Singularity Table (Obsolete)

9

OEIGS

Eigenvalue Analysis Summary

10

OUG

Velocity Vector

11

OUG

Acceleration Vector

12

OPG

Nonlinear Force Vector

13

OGPWG

Grid Point Weight Generator

14

OUG

Eigenvector (Solution Set)

15

OUG

Displacement Vector (Solution Set)

16

OUG

Velocity Vector (Solution Set)

17

OUG

Acceleration Vector (Solution Set)

18

OEE

Element Strain Energy

19

OGF

Grid Point Force Balance

20

Stresses at grid points

21

OES

Strain / Curvature at Grid Points

22

OELOF1

Element Internal Forces and Moments

23

OELOP1

Summation of Element Oriented Forces on Adjacent Elements

24

OEP

Element Pressures

25

OEF

Composite Failure Indices

26

OGS

Grid Point Stresses (Surface)

27

OGS

Grid Point Stresses (Volume – Direct)

28

OGS

Grid Point Stresses (Volume – Principal)

29

OGS

Element Stress Discontinuities (Surface)

30

OGS

Element Stress Discontinuities (Volume – Direct)

31

OGS

Element Stress Discontinuities (Volume – Principal)

32

OGS

Grid Point Stress Discontinuities (Surface)

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Type

2-8

Overview of Data Blocks

Data Block Description Name

Description

33

OGS

Grid Point Stress Discontinuities (Volume – Direct)

34

OGS

Grid Point Stress Discontinuities (Volume – Principal)

35

OGS

Grid Point Stresses (Plane Strain)

36

OEE

Element Kinetic Energy

37

OEE

Element Energy Loss

38

OMSEC

Constant modal strain energy

39

OMSED

Oscillating modal strain energy

40

OMKEC

Constant modal kinetic energy

41

OMKED

Oscillating modal kinetic energy

42

OMECON

Constant total modal energy

43

OMEOSC

Oscillating total modal energy

44

OUGMC

Displacement/velocity/acceleration modal contributions

45

OEFMC

Element force modal contributions

46

OESMC

Element stress modal contributions

47

OSTRMC

Element strain modal contributions

48

OQGMC

SPC force modal contributions

49

OUGPC

Panel contributions

50

OUGGC

Grid contributions

51

OUGRC

Reciprocal panel contributions

61

OGK

Gasket Element Results

62

OBC

Contact Pressure and Traction Results

63

OQG

Contact Force Results

64

OSPDSI

Contact Separation Distance - Initial

65

OSPDS

Contact Separation Distance

66

OBG

Glue force results (normal and in-plane tractions)

DMAP Programmer’s Guide

Overview of Data Blocks

Type

67

Data Block Description Name OQG

68

Description

Glue force results Tosca normalized material properties

2. Data format and sort types are extracted from the bit pattern equal to table_code/1000. Bits numbered from the right are: Bit

Description

1

Complex (on) flag

2

SORT2 (on) flag

3

Random (on) flag

Therefore, table_code/1000 can be one of the following values: Value

Sort type

Data format

Random

0

SORT1

Real

No

1

SORT1

Complex

No

2

SORT2

Real

No

3

SORT2

Complex

No

4

SORT1

Real

Yes

6

SORT2

Real

Yes

Examples: table_code

Description

4

Real Force in SORT1

5

Real Stress/Strain in SORT1

1005

Complex Stress/Strain in SORT1

2010

Real Displacements in SORT2

3005

Complex Stress/Strain in SORT2

6003

Random SPCforces in SORT2

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Chapter 2

Format_code Format_code is somewhat redundant and can conflict with table_code. In regard to real or complex data formats, table_code/1000 always overrides format_code. However, when table_code indicates complex data, format_code is used to determine whether the output is real, real/imaginary, or magnitude/phase. Value

Data format

1

Real

2

Real/Imaginary

3

Magnitude/Phase

Stress_code In the OES data block description, word 11 (stress_code) of the header record determines the following: •

Octahedral (or maximum shear) or Hencky-von Mises.

•

Stress or strain.

•

If the strain is curvature or fibre.

Stress_code is a bit pattern and the bits numbered from the right are: Bit

Description

1

Hencky von Mises (on) flag

2

Strain (on) flag

3

Strain/fiber (on) flag

4

Same as bit 2

5

Material coordinate system (on) flag

Therefore, stress_code can be one of the following values: Value

On bits

Description

0

0000

Stress maximum shear or octahedral

1

0001

Stress von Mises

10

1010

Strain Curvature maximum shear or octahedral

11

1011

Strain Curvature von Mises

14

1110

Strain Fibre maimum shear or octahedral

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Value 15

On bits 1111

Description Strain Fibre von Mises

In the OQG data block description, stress_code can be one of the following values: Value

Description

0

SPCForce

1

MPCForce

Element Type Some tables reference an element type number. For example, EST, KDICT, OES, and EGPSF. The element type numbers are unique across all tables but do not necessarily appear in all tables. Some element types are pseudo-elements for data recovery purposes only; see types 85 through 98, 100, 144, and 201 through 223. Type

Name

00

Description Grid

01

ROD

Rod

02

BEAM

Beam

03

TUBE

Tube

04

SHEAR

Shear panel

05

FORCE1, MOMENTi

FORCEi/MOMENTi follower stiffness

06

Unused (Pre-V69 CTRIA1)

07

PLOAD4

PLOAD4 follower stiffness

08

PLOADX1

PLOADX1 follower stiffness

09

PLOAD/PLOAD2

PLOAD/PLOAD2 follower stiffness

10

CONROD

Rod with properties

11

ELAS1

Scalar spring

12

ELAS2

Scalar spring with properties

13

ELAS3

Scalar spring to scalar points only

14

ELAS4

Scalar spring to scalar points only with properties

15

AEROT3

DMAP Programmer’s Guide

2-11

Chapter 2

Overview of Data Blocks

Type 16

Name

Description

AEROBEAM

17

Unused (Pre-V69 CTRIA2)

18

Unused (Pre-V69 CQUAD2)

19

Unused (Pre-V69 CQUAD1)

20

DAMP1

Scalar damper

21

DAMP2

Scalar damper with properties

22

DAMP3

Scalar damper to scalar points only

23

DAMP4

Scalar damper to scalar points only with properties

24

VISC

Viscous damper

25

MASS1

Scalar mass

26

MASS2

Scalar mass with properties

27

MASS3

Scalar mass to scalar points only

28

MASS4

Scalar mass to scalar points only with properties

29

CONM1

Concentrated mass – general form

30

CONM2

Concentrated mass – rigid body form

31

PLOTEL

Plot

32

Unused

33

QUAD4

Quadrilateral plate with centroid force and stress recovery

34

BAR

Simple beam (see also Type=100)

35

CONE

Axisymmetric shell

36

Unused (Pre-V69 CTRIARG)

37

Unused (Pre-V69 CTRAPRG)

38

GAP

Gap

39

TETRA

Four-sided solid

40

BUSH1D

Rod type spring and damper

41

2-12

Unused (Pre-V69 CHEXA1)

DMAP Programmer’s Guide

Overview of Data Blocks

Type

Name

42

Description Unused (Pre-V69 CHEXA2)

43

FLUID2

Fluid with 2 points

44

FLUID3

Fluid with 3 points

45

FLUID4

Fluid with 4 points

46

FLMASS

47

AXIF2

Fluid with 2 points

48

AXIF3

Fluid with 3 points

49

AXIF4

Fluid with 4 points

50

SLOT3

Three-point slot

51

SLOT4

Four-point slot

52

HBDY

Heat transfer plot for CHBDYG and CHBDYP

53

TRIAX6

Axisymmetric triangular

54

Unused (Pre-V69 TRIM6)

55

DUM3

Three-point dummy

56

DUM4

Four-point dummy

57

DUM5

Five-point dummy

58

DUM6

Six-point dummy

59

DUM7

Seven-point dummy

60

DUM8

Eight-point dummy (also two-dimensional crack tip CRAC2D)

61

DUM9

Nine-point dummy (also three-dimensional crack tip CRAC3D)

62

Unused (Pre-V69 CQDMEM1)

63

Unused (Pre-V69 CQDMEM2)

64

QUAD8

Curved quadrilateral shell

65

Unused (Pre-V69 CHEX8)

66

Unused (Pre-V69 CHEX20)

DMAP Programmer’s Guide

2-13

Chapter 2

Overview of Data Blocks

Type

Name

Description

67

HEXA

Six-sided solid

68

PENTA

Five-sided solid

69

BEND

Curved beam or pipe

70

TRIAR

Triangular plate with corner force and stress recovery

71 72

Unused AEROQ4

73

Unused (Pre-V69 CFTUBE)

74

TRIA3

Triangular plate

75

TRIA6

Curved triangular shell

76

HEXPR

Acoustic velocity/pressures in six-sided solid

77

PENPR

Acoustic velocity/pressures in five-sided solid

78

TETPR

Acoustic velocity/pressures in four-sided solid

79

Unused

80

Unused

81

Unused

82

QUADR

Quadrilateral plate with corner force and stress recovery

83

HACAB

Acoustic absorber

84

HACBR

Acoustic barrier

85

TETRA

Nonlinear data recovery four-sided solid

86

GAP

Nonlinear data recovery gap

87

TUBE

Nonlinear data recovery tube

88

TRIA3

Nonlinear data recovery triangular plate

89

ROD

Nonlinear data recovery rod

90

QUAD4

Nonlinear data recovery quadrilateral plate

91

PENTA

Nonlinear data recovery five-sided solid

92

CONROD

Nonlinear data recovery rod with properties

2-14

DMAP Programmer’s Guide

Overview of Data Blocks

Type

Name

Description

93

HEXA

Nonlinear data recovery six-sided solid

94

BEAM

Nonlinear data recovery beam

95

QUAD4

Composite data recovery quadrilateral plate

96

QUAD8

Composite data recovery curved quadrilateral shell

97

TRIA3

Composite data recovery triangular shell

98

TRIA6

Composite data recovery curved triangular shell

99

Unused

100

BAR

Simple beam with intermediate station data recovery

101

AABSF

Acoustic absorber with frequency dependence

102

BUSH

Generalized spring and damper

103

QUADP

p-version quadrilateral shell

104

TRIAP

p-version triangular shell

105

BEAMP

p-version beam

106

DAMP5

Heat transfer scalar damper with material property

107

CHBDYE

Heat transfer geometric surface – element form

108

CHBDYG

Heat transfer geometric surface – grid form

109

CHBDYP

Heat transfer geometric surface – property form

110

CONV

Heat transfer boundary with free convection

111

CONVM

Heat transfer boundary with forced convection

112

QBDY3

Heat transfer boundary heat flux load for a surface

113

QVECT

Heat transfer thermal vector flux load

114

QVOL

Heat transfer volume heat addition

115

RADBC

Heat transfer space radiation

116

SLIF1D

Slideline contact

117

Unused

118

Unused

DMAP Programmer’s Guide

2-15

Chapter 2

Overview of Data Blocks

Type

Name

Description

119

Unused

120

Unused

121

Unused

122

Unused

123

Unused

124

Unused

125

Unused

126

Unused

127

Unused

128

Unused

129

Unused

130

Unused

131

Unused

132

Unused

133

Unused

134

Unused

135

Unused

136

Unused

137

Unused

138

Unused

139

QUAD4FD

Hyperelastic 4-noded quadrilateral shell

140

HEXA8FD

Hyperelastic 8-noded solid

141

HEXAP

p-version six-sided solid

142

PENTAP

p-version five-sided solid

143

TETRAP

p-version four-sided solid

144

QUAD144

Quadrilateral plate with data recovery for corner forces and stresses

2-16

DMAP Programmer’s Guide

Overview of Data Blocks

Type

Name

Description

145

VUHEXA

p-version six-sided solid display

146

VUPENTA

p-version five-sided solid display

147

VUTETRA

p-version four-sided solid display

148

Unused

149

Unused

150

Unused

151

Unused

152

Unused

153

Unused

154

Unused

155

Unused

156

Unused

157

Unused

158

Unused

159

Unused

160

PENTA6FD

Hyperelastic pentahedron 6-noded

161

TETRA4FD

Hyperelastic tetrahedron 4-noded

162

TRIA3FD

Hyperelastic triangular 3-noded

163

HEXAFD

Hyperelastic hexahedron 20-noded

164

QUADFD

Hyperelastic quadrilateral 9-noded

165

PENTAFD

Hyperelastic pentahedron 15-noded

166

TETRAFD

Hyperelastic tetrahedron 10-noded

167

TRIAFD

Hyperelastic triangular 6-noded

168

TRIAX3FD

Hyperelastic axisymmetric triangular 3-noded

169

TRIAXFD

Hyperelastic axisymmetric triangular 6-noded

170

QUADX4FD

Hyperelastic axisymmetric quadrilateral 4-noded

DMAP Programmer’s Guide

2-17

Chapter 2

Overview of Data Blocks

Type 171

Name QUADXFD

Description Hyperelastic axisymmetric quadrilateral 9-noded

172

Unused

173

Unused

174

Unused

175

Unused

176

Unused

177

Unused

178

Unused

179

Unused

180

Unused

181

Unused

182

Unused

183

Unused

184

Unused

185

Unused

186

Unused

187

Unused

188

Unused

189

VUQUAD

p-version quadrilateral shell display

190

VUTRIA

p-version triangular shell display

191

VUBEAM

p-version beam display

192

CVINT

Curve interface

193

Unused

194

Unused

195

Unused

196

Unused

2-18

DMAP Programmer’s Guide

Overview of Data Blocks

Type

Name

Description

197

SFINT

198

CNVPEL

199

VUHBDY

p-version HBDY display

200

CWELD

Weld or fastener

201

QUAD4FD

Hyperelastic quadrilateral 4-noded nonlinear d.r. Gaus/Grid

202

HEXA8FD

Hyperelastic hexahedron 8-noded nonlinear d.r. Gaus/Grid

203

SLIF1D

Slideline contact

204

PENTA6FD

Hyperelastic pentahedron 6-noded nonlinear format Gaus/Grid

205

TETRA4FD

Hyperelastic tetrahedron 4-noded nonlinear format Gaus

206

TRIA3FD

Hyperelastic triangular 3-noded nonlinear format Gaus

207

HEXAFD

Hyperelastic hexahedron 20-noded nonlinear format Gaus

208

QUADFD

Hyperelastic quadrilateral 8-noded nonlinear format Gaus

209

PENTAFD

Hyperelastic pentahedron 15-noded nonlinear format Gaus

210

TETRAFD

Hyperelastic tetrahedron 10-noded nonlinear format Grid

211

TRIAFD

Hyperelastic triangular 6-noded nonlinear format Gaus/Grid

212

TRIAX3FD

Hyperelastic axisymmetric triangular 3-noded nonlinear format Gaus

213

TRIAXFD

Hyperelastic axisymmetric triangular 6-noded nonlinear format Gaus/Grid

214

QUADX4FD

Hyperelastic axisymmetric quadrilateral 4-noded nonlinear format Gaus/Grid

215

QUADXFD

Hyperelastic axisymmetric quadrilateral 8-noded nonlinear format Gaus

Surface interface

DMAP Programmer’s Guide

2-19

Chapter 2

Overview of Data Blocks

Type

Name

Description

216

TETRA4FD

Hyperelastic tetrahedron 4-noded nonlinear format Grid

217

TRIA3FD

Hyperelastic triangular 3-noded nonlinear format Grid

218

HEXAFD

Hyperelastic hexahedron 20-noded nonlinear format Grid

219

QUADFD

Hyperelastic quadrilateral 8-noded nonlinear format Grid

220

PENTAFD

Hyperelastic pentahedron 15-noded nonlinear format Grid

221

TETRAFD

Hyperelastic tetrahedron 10-noded nonlinear format Gaus

222

TRIAX3FD

Hyperelastic axisymmetric triangular 3-noded nonlinear format Grid

223

QUADXFD

Hyperelastic axisymmetric quadrilateral 8-noded nonlinear format Grid

224

ELAS1

Nonlinear ELAS1

225

ELAS3

Nonlinear ELAS3

226

BUSH

Nonlinear BUSH

227

TRIAR

New quadrilateral plate with data recovery for center forces and stresses

228

QUADR

New quadrilateral plate with data recovery for center forces and stresses

229

Reserved

230

Reserved

231

Reserved

232

QUADR – Composite

Composite data recovery for new quadrilateral plate

233

TRIAR – Composite

Composite data recovery for new quadrilateral plate

234

Reserved

235

Reserved

236

Reserved

237

Reserved

2-20

DMAP Programmer’s Guide

Overview of Data Blocks

Type

Name

Description

238

Reserved

239

Reserved

240

CTRIA6

Nonlinear Format (Center and Corners)

241

CQUAD8

Nonlinear Format (Center and Corners)

242

CTRAX3

Linear Format, Grid or Gauss (Center and Corners)

243

CQUADX4

Linear Format, Grid and Gauss (Center and Corners)

244

CTRAX6

Linear Format, Grid and Gauss (Center and Corners)

245

CQUADX8

Linear Format, Grid and Gauss (Center and Corners)

246

CTRAX3

Nonlinear Format (Center and Corners)

247

CQUADX4

Nonlinear Format (Center and Corners)

248

CTRAX6

Nonlinear Format (Center and Corners)

249

CQUADX8

Nonlinear Format

255

CPYRAM

Linear Format

256

CPYRAM

Nonlinear Format

257

CPYRAMFD

Pyramid with 5-grids

258

CPYRAMFD

Pyramid with 13-grids hyperelastic

261

CTRAX3FD

Hyperelastic (261) Grid and Gauss

262

CQUADX4FD

Hyperelastic, Grid or Gauss (Center and Corners)

263

CTRAX6FD

Grid or Gauss hyperelastic (Center and Corners)

264

CQUADX8FD

Hyperelastic (Center and Corners)

266

CQUADX8FD

Hyperelastic GAUSS Locations

271

CPLSTN3

Triangle plane strain linear format (Center Only)

272

CPLSTN4

Quadrilateral plane strain linear format (Center and Corners)

273

CPLSTN6

Triangle plane strain linear format (Center and Corners)

DMAP Programmer’s Guide

2-21

Chapter 2

Type

Overview of Data Blocks

Name

Description

274

CPLSTN8

Quadrilateral plane strain linear format (Center and Corners)

275

CPLSTS3

Triangle plane stress linear Format (Center Only)

276

CPLSTS4

Quadrilateral plane stress linear format (Center and Corners)

277

CPLSTS6

Triangle plane stress linear format (Center and Corners)

278

CPLSTS8

Quadrilateral plane stress linear format (Center and Corners)

281

CPLSTN3

Triangle plane strain nonlinear format (Center Only)

283

CPLSTN6

Triangle plane strain nonlinear format (Center and Corners)

284

CPLSTN8

Quadrilateral plane strain nonlinear format (Center and Corners)

285

CPLSTS3

Triangle plane stress nonlinear format (Center Only)

287

CPLSTS6

Triangle plane stress nonlinear format (Center and Corners)

288

CPLSTS8

Quadrilateral plane stress nonlinear format (Center and Corners)

289

CPLSTN4

Quadrilateral plane strain nonlinear format (Center and Corners)

290

CPLSTS4

Quadrilateral plane stress nonlinear format (Center and Corners)

291

CPLSTN3)

Triangle plane strain hyperelastic (Grid)

292

CPLSTN4

Quadrilateral plane strain hyperelastic (Grid)

293

CPLSTN6

Triangle plane strain hyperelastic (Grid)

294

CPLSTN8

Quadrilateral plane strain hyperelastic (Grid)

295

CPLSTS3

Triangle plane stress hyperelastic (Grid)

296

CPLSTS4

Quadrilateral plane stress hyperelastic (Grid)

297

CPLSTS6

Triangle plane stress hyperelastic (Grid)

298

CPLSTS8

Quadrilateral plane stress hyperelastic (Grid)

2-22

DMAP Programmer’s Guide

Chapter

3

•

AXIC

•

AXIC68

•

BGPDT

•

BGPDT68

•

CASECC

•

CLAMA

Data Block Descriptions A-E

•

CONTAB

•

CONTACT

•

CSTM

•

CSTM68

•

DBCOPT

•

DESTAB

•

DIT

•

DSCMCOL

•

DVPTAB

•

DYNAMIC

•

EDOM

•

EDT

•

EGPSF

•

EGPSTR

•

ELDCT

•

EPT

•

EPT705

•

EQEXIN

•

ERROR

DMAP Programmer’s Guide

3-1

Data Block Descriptions A-E

Chapter 3

3.1 AXIC Element property table.

RECORD – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

RECORD – AXIC(515,5,144) Conical shell problem flag. Name

Word

Type

1

H

I

2

UNDEF

None

Description Highest harmonic

RECORD – AXIF(8815,88,212) Fluid related axisymmetric parameters. Name

Word

Type

Description

1

FCID

I

Fluid coordinate system identification

2

GRAV

RS

Value of gravity in axial direction

3

DRHO

RS

Default mass density for fluid elements

4

DBULK

RS

Default bulk modulus for fluid elements

5

NOSYM

I

Request for nonsymmetric series terms

6

NHARM

I

Number of harmonic numbers

7

N

I

Harmonic numbers

Words 7 repeats until -1 occurs

RECORD – AXSLOT(1115,11,223) Axisymmetric slot analysis parameters. Word 1

3-2

Name RHOD

DMAP Programmer’s Guide

Type RS

Description Density of fluids

Data Block Descriptions A-E

Name

Word

Type

Description

2

BD

RS

Bulk modulus

3

N

I

Harmonic index

4

WD

RS

Slot width

5

MD

I

Number of slots

RECORD – BDYLIST(8915,89,213) Fluid boundary list. Name

Word

Type

Description

1

RHO

RS

Fluid density at boundary

2

IDF

I

Identification number of a RINGFL entry

Word 2 repeats until -1 occurs

RECORD – CCONEAX(2315,23,146) Axisymmetric shell element connection. Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

RA

I

RINGAX identification number

4

RB

I

RINGAX identification number

RECORD – CFLUID2(8515,85,209) Fluid element connections. Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL identification number

3

IDF2

I

RINGFL identification number

4

RHO

RS

Mass density

5

B

RS

Bulk modulus

DMAP Programmer’s Guide

3-3

Data Block Descriptions A-E

Chapter 3

RECORD – CFLUID3(8615,86,210) Fluid element connections. Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL identification number

3

IDF2

I

RINGFL identification number

4

IDF3

I

RINGFL identification number

5

RHO

RS

Mass density

6

B

RS

Bulk modulus

RECORD – CFLUID4(8715,87,211) Fluid element connections. Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL identification number

3

IDF2

I

RINGFL identification number

4

IDF3

I

RINGFL identification number

5

IDF4

I

RINGFL identification number

6

RHO

RS

Mass density

7

B

RS

Bulk modulus

RECORD – FLSYM(9115,91,222) Axisymmetric symmetry control. Name

Word

Type

Description

1

M

I

Number of symmetric sections

2

S1

I

Boundary constraint

3

S2

I

Boundary constraint

3-4

DMAP Programmer’s Guide

Data Block Descriptions A-E

RECORD – FORCE(4201,42,18) Static force. Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

F

RS

Scale factor

5

N1

RS

Vector component in the coordinate system defined by CID

6

N2

RS

Vector component in the coordinate system defined by CID

7

N3

RS

Vector component in the coordinate system defined by CID

RECORD – FORCEAX(2115,21,156) Conical shell static force. Name

Word

Type

Description

1

SID

I

Load set identification number

2

RID

I

RINGAX identification number

3

HID1

I

Harmonic identification number (starting value if a sequence)

4

HID2

I

Harmonic identification number (ending value if a sequence)

5

S

RS

Scale factor for force

6

FR

RS

Force component (radial)

7

FP

RS

Force component (phi)

8

FZ

RS

Force component (z)

RECORD – FREEPT(9015,90,214) Fluid free surface point.

DMAP Programmer’s Guide

3-5

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

1

IDF

I

RINGFL identification number

2

IDP

I

Free point

3

PHI

RS

Azimuthal position

RECORD – FSLIST(8215,82,206) Free surface list. Name

Word

Type

Description

1

RHO

RS

Mass density

2

IDF

I

RINGFL identification number

Word 2 repeats until -1 occurs

RECORD – GRAV(4401,44,26) Acceleration or gravity load. Name

Word

Type

Description

1

SID

I

Load set identification number

2

CID

I

Coordinate system identification number

3

A

RS

Acceleration scale factor

4

N1

RS

Vector component in the coordinate system defined by CID

5

N2

RS

Vector component in the coordinate system defined by CID

6

N3

RS

Vector component in the coordinate system defined by CID

7

MB

I

Bulk data section with CID definition: -1=main, 0=partitioned

RECORD – GRIDB(8115,81,205) Axisymmetric grid point. Name

Word 1

3-6

ID

DMAP Programmer’s Guide

Type I

Description Grid identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

CD

I

Coordinate system identification number

3

PA

I

Permanent single-point constraint

4

IDF

I

RINGFL identification number

5

PHI

RX

Azimuthal position

RECORD – GRIDF(1215,12,229) Fluid point. Name

Word

Type

Description

1

ID

I

Point identification number

2

R

RX

Radial location of point

3

Z

RX

Axial location of point

RECORD – GRIDS(1315,13,230) Slot surface point. Name

Word

Type

Description

1

ID

I

Slot identification number

2

IDF

I

GRIDF identification number

3

R

RX

Radial location of point

4

Z

RX

Axial location of point

5

W

RX

Slot width

RECORD – LOAD(4551,61,84) Static load combination. Name

Word

Type

Description

1

SID

I

Load set identification number

2

S

RS

Overall scale factor

3

Si

RS

Scale factor on Li

DMAP Programmer’s Guide

3-7

Data Block Descriptions A-E

Chapter 3

Name

Word 4

Type

Li

I

Description Load set identification number

Words 3 and 4 repeat until (-1,-1) occurs

RECORD – MOMAX(3815,38,157) Conical shell static moment. Name

Word

Type

Description

1

SID

I

Load set identification number

2

RID

I

RINGAX identification number

3

HID1

I

Harmonic identification number (starting value if a sequence)

4

HID2

I

Harmonic identification number (ending value if a sequence)

5

S

RS

Scale factor for moment

6

MR

RS

Moment component (radial)

7

MP

RS

Moment component (phi)

8

MZ

RS

Moment component (z)

RECORD – MOMENT(4801,48,19) Static moment. Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

M

RS

Moment scale factor

5

N1

RS

Vector component in the coordinate system defined by CID

6

N2

RS

Vector component in the coordinate system defined by CID

7

N3

RS

Vector component in the coordinate system defined by CID

3-8

DMAP Programmer’s Guide

Data Block Descriptions A-E

RECORD – MPCADD(4891,60,83) Multipoint constraint set combination. Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Set identification number of multipoint constraint set

Word 2 repeats until -1 occurs

RECORD – MPCAX(4015,40,149) Conical shell multipoint constraint. Name

Word

Type

Description

1

SID

I

Load set identification number

2

RID

I

RINGAX identification number

3

HID

I

Harmonic identification number

4

C

I

Component number of dependent degree-of-freedom

5

A

RX

Coefficient

6

RID1

I

RINGAX identification number

7

HID1

I

Harmonic identification number

8

C

I

Component number of independent degree-of-freedom

9

A

RX

Coefficient

Words 6 through 9 repeat until (-1,-1,-1,-1) occurs

RECORD – OMITAX(4315,43,150) Omitted conical shell degrees-of-freedom. Name

Word

Type

Description

1

RID

I

Ring identification number

2

HID

I

Harmonic identification number

3

C

I

Component number

DMAP Programmer’s Guide

3-9

Data Block Descriptions A-E

Chapter 3

RECORD – POINTAX(4915,49,152) Conical shell point. Name

Word

Type

Description

1

ID

I

Point identification number

2

RID

I

RINGAX identification number

3

PHI

RX

Azimuthal angle

RECORD – PRESAX(5215,52,154) Conical shell pressure load. Name

Word

Type

Description

1

SID

I

Load set identification number

2

P

RS

Pressure value

3

RID1

I

Ring identification number

4

RID2

I

Ring identification number

5

PHI1

RS

Azimuthal angle

6

PHI2

RS

Azimuthal angle

RECORD – PRESPT(8415,84,208) Fluid pressure point. Name

Word

Type

Description

1

IDF

I

Fluid point identification number

2

IDP

I

Pressure point identification number

3

PHI

RS

Azimuthal angle

RECORD – RINGAX(5615,56,145) Conical shell ring. Name

Word

Type

Description

1

ID

I

Ring identification number

2

R

RX

Ring radius

3-10

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

3

Z

RX

Ring axial location

4

PS

I

Permanent single-point constraint

RECORD – RINGFL(8315,83,207) Axisymmetric fluid point. Name

Word

Type

Description

1

IDF

I

2

UNDEF

None

3

X1

RX

Coordinate of point

4

X2

RX

Coordinate of point

5

X3

RX

Coordinate of point

Fluid identification number

RECORD – SECTAX(6015,70,153) Conical shell sector. Name

Word

Type

Description

1

ID

I

Sector identification number

2

RID

I

Ring identification number

3

R

RX

Effective radius

4

PHI1

RX

Azimuthal angle limit of sector

5

PHI2

RX

Azimuthal angle limit of sector

RECORD – SEQGP(5301,53,4) Grid and scalar point resequencing. Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

SEQID

I

Sequenced identification number

DMAP Programmer’s Guide

3-11

Data Block Descriptions A-E

Chapter 3

RECORD – SLBDY(1415,14,231) Slot boundary list. Name

Word

Type

Description

1

RHO

RS

Density of fluid

2

M

I

Number of slots

3

ID

I

Identification number of GRIDS slot point

Word 3 repeats until -1 occurs

RECORD – SPCADD(5491,59,13) Single-point constraint set combination. Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Single-point constraint set identification number

Word 2 repeats until -1 occurs

RECORD – SPCAX(6215,62,148) Conical shell single-point constraint. Name

Word

Type

Description

1

SID

I

Set identification number

2

RID

I

Ring identification number

3

HID

I

Harmonic identification number

4

C

I

Component identification number

5

D

RS

Enforced displacement value

RECORD – SUPAX(6415,64,151) Conical shell fictitious support. Word 1

3-12

Name RID

DMAP Programmer’s Guide

Type I

Description Ring identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

HID

I

Harmonic identification number

3

C

I

Component identification number

RECORD – TEMPAX(6815,68,155) Conical shell temperature. Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

RID

I

Ring identification number

3

PHI

RS

Azimuthal angle

4

TEMP

RS

Temperature

RECORD – TEMPD(5641,65,98) Grid point temperature field default. Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

T

RS

Temperature

TRAILER Word 1-6

Name UNDEF(6)

Type

Description

None

Notes: 1. The following records are used with conical shell elements: AXIC, CCONEAX, FORCEAX, MOMAX, MPCAX, OMITAX, POINTAX, PRESAX, RINGAX, SECTAX, SPCAX, SUPAX, and TEMPAX. 2. The following records are used with hydroelastic elements: AXIF, BDYLIST, CFLUID2, CFLUID3, CFLUID4, FLSYM, FREEPT, FSLIST, GRIDB, PRESPT, and RINGFL. 3. The following records are used with acoustic cavity elements: AXSLOT, GRIDF, GRIDS, and SLBDY.

DMAP Programmer’s Guide

3-13

Data Block Descriptions A-E

Chapter 3

3.2 AXIC68 Element property table (Pre-MSC Nastran Version 69). Note See the Note 4 for a listing of the differences between AXIC68 and AXIC.

RECORD – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

RECORD – AXIC(515,5,144) Conical shell problem flag. Name

Word

Type

1

H

I

2

UNDEF

None

Description Highest harmonic

RECORD – AXIF(8815,88,212) Fluid related axisymmetric parameters. Name

Word

Type

Description

1

FCID

I

Fluid coordinate system identification

2

GRAV

RS

Value of gravity in axial direction

3

DRHO

RS

Default mass density for fluid elements

4

DBULK

RS

Default bulk modulus for fluid elements

5

NOSYM

I

Request for nonsymmetric series terms

6

NHARM

I

Number of harmonic numbers

7

N

I

Harmonic numbers

Words 7 repeats until -1 occurs

RECORD – AXSLOT(1115,11,223) Axisymmetric slot analysis parameters.

3-14

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

RHOD

RS

Density of fluids

2

BD

RS

Bulk modulus

3

N

I

Harmonic index

4

WD

RS

Slot width

5

MD

I

Number of slots

RECORD – BDYLIST(8915,89,213) Fluid boundary list. Name

Word

Type

Description

1

RHO

RS

Fluid density at boundary

2

IDF

I

Identification number of a RINGFL entry

Word 2 repeats until -1 occurs

RECORD – CCONEAX(2315,23,146) Axisymmetric shell element connection. Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

RA

I

RINGAX identification number

4

RB

I

RINGAX identification number

RECORD – CFLUID2(8515,85,209) Fluid element connections. Word

Name

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL identification number

3

IDF2

I

RINGFL identification number

DMAP Programmer’s Guide

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

RHO

RS

Mass density

5

B

RS

Bulk modulus

RECORD – CFLUID3(8615,86,210) Fluid element connections. Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL identification number

3

IDF2

I

RINGFL identification number

4

IDF3

I

RINGFL identification number

5

RHO

RS

Mass density

6

B

RS

Bulk modulus

RECORD – CFLUID4(8715,87,211) Fluid element connections. Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL identification number

3

IDF2

I

RINGFL identification number

4

IDF3

I

RINGFL identification number

5

IDF4

I

RINGFL identification number

6

RHO

RS

Mass density

7

B

RS

Bulk modulus

RECORD – FLSYM(9115,91,222) Axisymmetric symmetry control. Name

Word 1

3-16

M

DMAP Programmer’s Guide

Type I

Description Number of symmetric sections

Data Block Descriptions A-E

Name

Word

Type

Description

2

S1

I

Boundary constraint

3

S2

I

Boundary constraint

RECORD – FORCE(4201,42,18) Static force. Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

F

RS

Scale factor

5

N1

RS

Vector component in the coordinate system defined by CID

6

N2

RS

Vector component in the coordinate system defined by CID

7

N3

RS

Vector component in the coordinate system defined by CID

RECORD – FORCEAX(2115,21,156) Conical shell static force. Name

Word

Type

Description

1

SID

I

Load set identification number

2

RID

I

RINGAX identification number

3

HID1

I

Harmonic identification number (starting value if a sequence)

4

HID2

I

Harmonic identification number (ending value if a sequence)

5

S

RS

Scale factor for force

6

FR

RS

Force component (radial)

7

FP

RS

Force component (phi)

8

FZ

RS

Force component (z)

DMAP Programmer’s Guide

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Data Block Descriptions A-E

Chapter 3

RECORD – FREEPT(9015,90,214) Fluid free surface point. Name

Word

Type

Description

1

IDF

I

RINGFL identification number

2

IDP

I

Free point

3

PHI

RS

Azimuthal position

RECORD – FSLIST(8215,82,206) Free surface list. Name

Word

Type

Description

1

RHO

RS

Mass density

2

IDF

I

RINGFL identification number

Word 2 repeats until -1 occurs

RECORD – GRAV(4401,44,26) Acceleration or gravity load. Name

Word

Type

Description

1

SID

I

Load set identification number

2

CID

I

Coordinate system identification number

3

A

RS

Acceleration scale factor

4

N1

RS

Vector component in the coordinate system defined by CID

5

N2

RS

Vector component in the coordinate system defined by CID

6

N3

RS

Vector component in the coordinate system defined by CID

7

MB

I

Bulk data section with CID definition: -1=main, 0=partitioned

RECORD – GRIDB(8115,81,205) Axisymmetric grid point.

3-18

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

ID

I

Grid identification number

2

PHI

RS

Azimuthal position

3

CD

I

Coordinate system identification number

4

PA

I

Permanent single-point constraint

5

IDF

I

RINGFL identification number

RECORD – GRIDF(1215,12,229) Fluid point. Name

Word

Type

Description

1

ID

I

Point identification number

2

R

RS

Radial location of point

3

Z

RS

Axial location of point

RECORD – GRIDS(1315,13,230) Slot surface point. Name

Word

Type

Description

1

ID

I

Slot identification number

2

R

RS

Radial location of point

3

Z

RS

Axial location of point

4

W

RS

Slot width

5

IDF

I

GRIDF identification number

RECORD – LOAD(4551,61,84) Static load combination. Name

Word

Type

Description

1

SID

I

Load set identification number

2

S

RS

Overall scale factor

DMAP Programmer’s Guide

3-19

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

3

Si

RS

Scale factor on Li

4

Li

I

Load set identification number

Words 3 and 4 repeat until (-1,-1) occurs

RECORD – MOMAX(3815,38,157) Conical shell static moment. Name

Word

Type

Description

1

SID

I

Load set identification number

2

RID

I

RINGAX identification number

3

HID1

I

Harmonic identification number (starting value if a sequence)

4

HID2

I

Harmonic identification number (ending value if a sequence)

5

S

RS

Scale factor for moment

6

MR

RS

Moment component (radial)

7

MP

RS

Moment component (phi)

8

MZ

RS

Moment component (z)

RECORD – MOMENT(4801,48,19) Static moment. Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

M

RS

Moment scale factor

5

N1

RS

Vector component in the coordinate system defined by CID

6

N2

RS

Vector component in the coordinate system defined by CID

3-20

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word 7

Type

N3

RS

Description Vector component in the coordinate system defined by CID

RECORD – MPCADD(4891,60,83) Multipoint constraint set combination. Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Set identification number of multipoint constraint set

Word 2 repeats until -1 occurs

RECORD – MPCAX(4015,40,149) Conical shell multipoint constraint. Name

Word

Type

Description

1

SID

I

Load set identification number

2

RID

I

RINGAX identification number

3

HID

I

Harmonic identification number

4

C

I

Component number of dependent degree-of-freedom

5

A

RS

Coefficient

6

RID1

I

RINGAX identification number

7

HID1

I

Harmonic identification number

8

C

I

Component number of independent degree-of-freedom

9

A

RS

Coefficient

Words 6 through 9 repeat until (-1,-1,-1,-1) occurs

RECORD – OMITAX(4315,43,150) Omitted conical shell degrees-of-freedom.

DMAP Programmer’s Guide

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

1

RID

I

Ring identification number

2

HID

I

Harmonic identification number

3

C

I

Component number

RECORD – POINTAX(4915,49,152) Conical shell point. Name

Word

Type

Description

1

ID

I

Point identification number

2

RID

I

RINGAX identification number

3

PHI

RS

Azimuthal angle

RECORD – PRESAX(5215,52,154) Conical shell pressure load. Name

Word

Type

Description

1

SID

I

Load set identification number

2

P

RS

Pressure value

3

RID1

I

Ring identification number

4

RID2

I

Ring identification number

5

PHI1

RS

Azimuthal angle

6

PHI2

RS

Azimuthal angle

RECORD – PRESPT(8415,84,208) Fluid pressure point. Word

Name

Type

Description

1

IDF

I

Fluid point identification number

2

IDP

I

Pressure point identification number

3

PHI

RS

Azimuthal angle

3-22

DMAP Programmer’s Guide

Data Block Descriptions A-E

RECORD – RINGAX(5615,56,145) Conical shell ring. Name

Word

Type

Description

1

ID

I

Ring identification number

2

R

RS

Ring radius

3

Z

RS

Ring axial location

4

PS

I

Permanent single-point constraint

RECORD – RINGFL(8315,83,207) Axisymmetric fluid point. Name

Word

Type

Description

1

IDF

I

Fluid identification number

2

X1

RS

Coordinate of point

3

X2

RS

Coordinate of point

4

X3

RS

Coordinate of point

RECORD – SECTAX(6015,70,153) Conical shell sector. Name

Word

Type

Description

1

ID

I

Sector identification number

2

RID

I

Ring identification number

3

R

RS

Effective radius

4

PHI1

RS

Azimuthal angle limit of sector

5

PHI2

RS

Azimuthal angle limit of sector

RECORD – SEQGP(5301,53,4) Grid and scalar point resequencing. Name

Word 1

ID

Type I

Description Grid or scalar point identification number

DMAP Programmer’s Guide

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Data Block Descriptions A-E

Chapter 3

Name

Word 2

Type I

SEQID

Description Sequenced identification number

RECORD – SLBDY(1415,14,231) Slot boundary list. Name

Word

Type

Description

1

RHO

RS

Density of fluid

2

M

I

Number of slots

3

ID

I

Identification number of GRIDS slot point

Word 3 repeats until -1 occurs

RECORD – SPCADD(5491,59,13) Single-point constraint set combination. Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Single-point constraint set identification number

Word 2 repeats until -1 occurs

RECORD – SPCAX(6215,62,148) Conical shell single-point constraint. Name

Word

Type

Description

1

SID

I

Set identification number

2

RID

I

Ring identification number

3

HID

I

Harmonic identification number

4

C

I

Component identification number

5

D

RS

Enforced displacement value

RECORD – SUPAX(6415,64,151) Conical shell fictitious support.

3-24

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

RID

I

Ring identification number

2

HID

I

Harmonic identification number

3

C

I

Component identification number

RECORD – TEMPAX(6815,68,155) Conical shell temperature. Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

RID

I

Ring identification number

3

PHI

RS

Azimuthal angle

4

TEMP

RS

Temperature

RECORD – TEMPD(5641,65,98) Grid point temperature field default. Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

T

RS

Temperature

TRAILER Word 1-6

Name UNDEF(6)

Type

Description

None

Notes: 1. The following records are used with conical shell elements: AXIC, CCONEAX, FORCEAX, MOMAX, MPCAX, OMITAX, POINTAX, PRESAX, RINGAX, SECTAX, SPCAX, SUPAX, and TEMPAX. 2. The following records are used with hydroelastic elements: AXIF, BDYLIST, CFLUID2, CFLUID3, CFLUID4, FLSYM, FREEPT, FSLIST, GRIDB, PRESPT, and RINGFL. 3. The following records are used with acoustic cavity elements: AXSLOT, GRIDF, GRIDS, and SLBDY.

DMAP Programmer’s Guide

3-25

Data Block Descriptions A-E

Chapter 3

4. AXIC68 is the same as AXIC except that: •

In RECORD - GRIDB, PHI is converted from RX to RS and is moved from Word 5 to Word 2. CD, PA, and IDF are moved to Words 3, 4, and 5, respectively.

•

In RECORD - GRIDF, R and Z are converted from RX to RS.

•

In RECORD - GRIDS, R, Z, and W are converted from RX to RS and are moved from Words 3, 4, and 5 to Words 2, 3, and 4, respectively.

•

In RECORD - MPCAX, A is converted from RX to RS in both Word 5 and Word 9.

•

In RECORD - POINTAX, PHI is converted from RX to RS.

•

In RECORD - RINGAX, R, and Z are converted from RX to RS.

•

In RECORD - RINGFL, X1, X2, and X3 are converted from RX to RS and UNDEF is stripped from the record. The record size is reduced from 5 words to 4 words.

•

In RECORD - SECTAX, R, PHI1, and PHI2 are converted from RX to RS.

3.3 BGPDT Basic grid point definition table. Contains a list of all grid points in internal sort, with (for grid points) their x, y, z locations in the basic coordinate system along with a displacement coordinate system identification number.

Record 0 – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record 1 – DATA Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

SIL

I

Internal (scalar) identification number

3

EXTID

I

External (User) identification number

4

DOF_TYPE

I

Degree of freedom/Point Type

5

PSC

I

Permanent Set Constraint

6

BGID

I

Boundary Grid ID of –EXTID

7

XCOORD

RX

x in basic coordinate system

3-26

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

8

YCOORD

RX

y in basic coordinate system

9

ZCOORD

RX

z in basic coordinate system

Words 1 through 9 repeat until End of Record

Record 2 – XIDMAP Word

Name

Type

Description

1

EXTID

I

External identification number

2

INTID

I

Internal identification number

Words 1 through 2 repeat until End of Record

Record 3 – BIDMAP Word

Name

Type

Description

1

BGID

I

Boundary (System) identification number

2

INTID

I

Internal identification number

Words 1 through 2 repeat until End of Record

Record 4 – NORMAL Word

Name

Type

Description

1

XNORM

RX

X normal in aerodynamic system

2

YNORM

RX

Y normal in aerodynamic system

3

ZNORM

RX

Z normal in aerodynamic system

Words 1 through 3 repeat until End of Record

Record 5 – TRAILER Word

Name

Type

Description

1

WORD1

I

Number of grid points and scalar points

2

WORD2

I

Number of boundary points

3

WORD3

I

Number of degrees-of-freedom

DMAP Programmer’s Guide

3-27

Chapter 3

Word

Data Block Descriptions A-E

Name

Type

Description

4

WORD4

I

Precision of the real values; for example, type=RX

5

WORD5

I

Number of scalar points

6

WORD6

I

Maximum external identification number

Notes: 1. For partitioned superelements the locations are in the superelement’s basic coordinate system. In other words, each partitioned superelement has its own basic coordinate system. 2. Scaler points are identified by CID=-1 and XCOORD = YCOORD = ZCOORD = 0. 3. If WORD2, the number of boundary grids, is zero, record BIDMAP does not exist and XIDMAP is used. 4. When grid point data is written to an OP2 file, by default the MAKEOLD module will convert the grid point data to BGPDT68 format. PARAM,OMACHPR,YES can be included in the input file to prevent this conversion, but be aware that post-processors may not recognize the BGPDT format as described above.

3.4 BGPDT68 Basic grid point definition table (Pre-MSC Nastran Version 69). Contains a list of all grid points in internal sort, with (for grid points) their x, y, z locations in the basic coordinate system along with a displacement coordinate system identification number. Note See the Note 3 for a listing of the differences between BGPDT68 and BGPDT.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – DATA Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

XCOORD

RS

x in basic coordinate system

3

YCOORD

RS

y in basic coordinate system

3-28

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word 4

ZCOORD

Type RS

Description z in basic coordinate system

Words 1 through 4 repeat until End of Record

Record 2 – TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of grid and scalar points

Notes: 1. Scaler points are identified by CID=-1 and XCOORD = YCOORD = ZCOORD = 0. 2. When the BGPDT68 data block is written by the MAKEOLD module, the data is named BGPDT although the BGPDT68 format is written. 3. BGPDT68 is the same as BGPDT except that: •

In Record - DATA, X1, X2, and X3 are converted from RX to RS.

•

SIL, EXTID, DOF_TYPE, PSC, and BGID are stripped from Record - DATA. The record size is reduced from 9 words to 4 words.

•

Record - XIDMAP is removed.

•

Record - BIDMAP is removed.

•

Record - NORMAL is removed.

•

In Record - TRAILER, WORD2 through WORD6 are undefined.

3.5 CASECC Case control information

Record – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name

DMAP Programmer’s Guide

3-29

Chapter 3

Data Block Descriptions A-E

Record – REPEAT Name

Word

Type

Description

1

SID

I

Subcase identification number

2

MPCSET

I

Multipoint constraint set (MPC)

3

SPCSET

I

Single point constraint set (SPC)

4

ESLSET

I

External static load set (LOAD)

5

REESET

I

Real eigenvalue extraction set (METHOD(STRUCTURE))

6

ELDSET

I

Element deformation set (DEFORM)

7

THLDSET

I

Thermal load set (TEMP(LOAD))

8

THMATSET

I

Thermal material set TEMP(MAT or INIT)

9

TIC

I

Transient initial conditions (IC)

10

NONPTSET

I

Nonlinear load output set (NLLOAD)

11

NONMEDIA

I

Nonlinear load output media (NLLOAD)

12

NONFMT

I

Nonlinear load output format (NLLOAD)

13

DYMLDSET

I

Dynamic load set (DLOAD)

14

FEQRESET

I

Frequency response set (FREQUENCY)

15

TFSET

I

Transfer function set (TFL)

16

SYMFLG

I

Symmetry flag (SYMSEQ and SUBSEQ)

17

LDSPTSET

I

Load output set (OLOAD)

18

LDSMEDIA

I

Load output media (OLOAD)

19

LDSFMT

I

Load output format (OLOAD)

20

DPLPTSET

I

Displ., temp., or pressure output set (DISP,THERM,PRES)

21

DPLMEDIA

I

Displ., temp., or pressure output media (DISP,THERM,PRES)

22

DPLFMT

I

Displ., temp., or pressure output format (DISP,THERM,PRES)

23

STSPTSET

I

Stress output set (STRESS)

3-30

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

24

STSMEDIA

I

Stress output media (STRESS)

25

STSFMT

I

Stress output format (STRESS)

26

FCEPTSET

I

Force (or flux) output set (FORCE or FLUX)

27

FCEMEDIA

I

Force (or flux) output media (FORCE or FLUX)

28

FCEFMT

I

Force (or flux) output format (FORCE or FLUX)

29

ACCPTSET

I

Acceleration (or enthalpy delta) output set (ACCEL or HDOT)

30

ACCMEDIA

I

Acceleration (or enthalpy delta) output media (ACCE, HDOT)

31

ACCFMT

I

Acceleration (or enthalpy delta) output format (ACCE, HDOT)

32

VELPTSET

I

Velocity (or enthalpy) output set (VELOCITY or ENTHALPY)

33

VELMEDIA

I

Velocity (or enthalpy) output media (VELOCITY) or ENTHALPY)

34

VELFMT

I

Velocity (or enthalpy) output format (VELOCITY) or ENTHALPY)

35

FOCPTSET

I

Forces of single-point constraint output set (SPCFORCE)

36

FOCMEDIA

I

Forces of single-point constraint output media (SPCFORCE)

37

FOCFMT

I

Forces of single-point constraint output format (SPCFORCE)

38

TSTEPTRN

I

Time step set for transient analysis (TSTEP)

39

TITLE(32)

CHAR4

Title character string (TITLE)

71

SUBTITLE(32)

CHAR4

Subtitle character string (SUBTITLE)

103

LABEL(32)

CHAR4

LABEL character string (LABEL)

135

STPLTFLG

I

Model plot flag: set to 1 if OUTPUT(PLOT) is specified

136

AXSYMSET

I

Axisymmetric set (AXISYMMETRIC)

DMAP Programmer’s Guide

3-31

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

137

NOHARMON

I

Number of harmonics to output (HARMONICS)

138

TSTRV

I

Need definition

139

K2PP(2)

CHAR4

Name of direct input (p-set) stiffness matrix (K2PP)

141

M2PP(2)

CHAR4

Name of direct input (p-set) mass matrix (M2PP)

143

B2PP(2)

CHAR4

Name of direct input (p-set) damping matrix (B2PP)

145

OUTRESPV

I

Output frequencies or times (OFREQ or OTIME)

146

SEDR

I

Data recovery superelement list (SEDR)

147

FLDBNDY

I

Fluid boundary element selection (MFLUID)

148

CEESET

I

Complex eigenvalue extraction set (CMETHOD)

149

DAMPTBL

I

Structural damping table set (SDAMP(STRUCT)

151

SSDSET

I

Solution set displacements output set (SDISP)

152

SSDMEDIA

I

Solution set displacements output media (SDISP)

153

SSDFMT

I

Solution set displacements output format (SDISP)

154

SSVSET

I

Solution set velocities output set (SVELO)

155

SSVMEDIA

I

Solution set velocities output media (SVELO)

156

SSVFMT

I

Solution set velocities output format (SVELO)

157

SSASET

I

Solution set accelerations output set (SACCE)

158

SSAMEDIA

I

Solution set accelerations output media (SACCE)

159

SSAFMT

I

Solution set accelerations output format (SACCE)

3-32

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

160

NONLINLD

I

Nonlinear load set in transient problems (NONLINEAR)

161

PARTIT

I

Partitioning set (PARTN)

162

CYCLIC

I

Symmetry option in cyclic symmetry (DSYM)

163

RANDOM

I

Random analysis set (RANDOM)

164

NONPARAM

I

Nonlinear static analysis control parameters (NLPARM)

165

FLUTTER

I

Flutter set (FMETHOD)

166

LCC

I

Number of words in this record up to LSEM

167

GPFSET

I

Grid point force output set (GPFORCE)

168

GPFMEDIA

I

Grid point force output media (GPFORCE)

169

GPFFMT

I

Grid point force output format (GPFORCE)

170

ESESET

I

Strain energy output set (ESE)

171

ESEMEDIA

I

Strain energy output media (ESE)

172

ESEFMT

I

Strain energy output format (ESE)

173

ARFPTSET

I

Aerodynamic force output set (AEROF)

174

ARFMEDIA

I

Aerodynamic force output media (AEROF)

175

ARFFMT

I

Aerodynamic force output format (AEROF)

176

SEID

I

Superelement ID (SUPER)

177

LCN

I

Load column number (SUPER)

178

GUST

I

Gust load selection (GUST)

179

SEFINAL

I

Final Superelement ID (SEFINAL)

180

SEMG

I

Generate matrices (K,M,B,K4) for superelement set or ID (SEMG)

181

SEKR

I

Reduce stiffness matrix (K) for superelement set or ID (SEKR)

182

SELG

I

Generate static loads for superelement set or ID (SELG)

DMAP Programmer’s Guide

3-33

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

183

SELR

I

Reduce static loads for superelement set or ID (SELR)

184

SEEX

I

Superelement set or ID to be excluded (SEEXCLUDE)

185

K2GG(2)

CHAR4

Name of direct input (g-set) stiffness matrix (K2GG)

187

M2GG(2)

CHAR4

Name of direct input (g-set) stiffness matrix (M2GG)

189

B2GG(2)

CHAR4

Name of direct input (g-set) stiffness matrix (B2GG)

191

SVSET

I

Solution eigenvector output set (SVECTOR)

192

SVMEDIA

I

Solution eigenvector output media (SVECTOR)

193

SVFMT

I

Solution eigenvectors output format (SVECTOR)

194

FLUPTSET

I

Fluid pressure output set (MPRES)

195

FLUMEDIA

I

Fluid pressure output media (MPRES)

196

FLUFMT

I

Fluid pressure output format (MPRES)

197

HOUT(3)

I

Cyclic symmetry harmonic output (HOUTPUT)

200

NOUT(3)

I

Cyclic symmetry physical output (NOUTPUT)

203

P2G(2)

CHAR4

Name of direct input (g-set) static loads matrix (P2G)

205

LOADSET

I

Sequence of static loads sets (LOADSET)

206

SEMR

I

Generate matrices (M,B,K4) for superelement set or ID (SEMG)

207

VONMISES

I

von Mises fiber (STRESS)

208

SECMDFLG

I

Superelement command existence flag

209

GPSPTSET

I

Grid point stress output set (GPSTRESS)

210

GPSMEDIA

I

Grid point stress output media (GPSTRESS)

211

GPSFMT

I

Grid point stress output format (GPSTRESS)

3-34

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

212

STFSET

I

Grid point stress field output set (STRFIELD)

213

STFMEDIA

I

Grid point stress field output media (STRFIELD

214

STFFMT

I

Grid point stress field output format (STRFIELD)

215

CLOAD

I

Superelement static load combination set (CLOAD)

216

SET2ID

I

Legacy design sensitivity contraint and variable set (SET2)

217

DSAPRT

I

Legacy design sensitivity analysis print option (SENSITY)

218

DSASTORE

I

Legacy design sensitivity analysis store option (SENSITY)

219

DSAOUTPT

I

Legacy design sensitivity analysis OUTPUT4 option (SENSITY)

220

STNSET

I

Strain output set (STRAIN)

221

STNMEDIA

I

Strain output media (STRAIN)

222

STNFMT

I

Strain output format (STRAIN)

223

APRESS

I

Aerodynamic pressure output set (APRESSURE)

224

TRIM

I

Aerostatic trim variable constrain set (TRIM)

225

MODLIST

I

Output modes list set (OMODES)

226

REESETF

I

Real eigenvalue extraction set for fluid (METHOD(FLUID))

227

ESDPTSET

I

Element stress discontinuity output set (ELSDCON)

228

ESDMEDIA

I

Element stress discontinuity output media (ELSDCON)

229

ESDFMT

I

Element stress discontinuity output format (ELSDCON)

230

GSDPTSET

I

Grid point stress discontinuity output set (GPSDCON)

DMAP Programmer’s Guide

3-35

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

231

GSDMEDIA

I

Grid point stress discontinuity output media (GPSDCON)

232

GSDFMT

I

Grid point stress discontinuity output format (GPSDCON)

233

SEDV

I

Generate pseudo-loads for superelement set or identification number (SEDV)

234

SERE

I

Generate responses for superelement set or ID (SERESP)

235

SERS

I

Restart processing for superelement set or ID (SERS)

236

CNTSET

I

Slideline contact output set (BOUTPUT)

237

CNTMEDIA

I

Slideline contact output media (BOUTPUT)

238

CNTFMT

I

Slideline contact output format (BOUTPUT)

239

DIVERG

I

Aerostatic divergence control parameter set (DIVERG)

240

OUTRCV

I

P-element output control parameters (OUTRCV)

241

STATSUBP

I

Static subcase identification number for pre-load (STATSUB(PRELOAD))

242

MODESELS

I

Mode selection set identification number for the structure (MODESELECT)

243

MODESELF

I

Mode selection set identification number for the fluid (MODESELECT)

244

SOLNUM

I

Solution sequence number

245

ANLOPT

I

SOL 601 analysis option: 106, 129, 153 or 159

246

ADAPT

I

P-element adaptivity control parameter set (ADAPT)

247

DESOBJ

I

Design objective set (DESOBJ)

248

DESSUB

I

Design constraint set for current subcase (DESSUB)

249

SUBSPAN

I

DRSPAN defined set ID of DRESP1 responses specific to this subcase.

3-36

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

250

DESGLB

I

Design constraint set for all subcases (DESGLB)

251

ANALYSIS

CHAR4

Type of analysis (ANALYSIS)

252

GPQSTRS

I

CQUAD4 grid point corner stress option (STRESS)

253

GPQFORC

I

CQUAD4 grid point corner force option (STRESS)

254

GPQSTRN

I

CQUAD4 grid point corner strain option (STRESS)

255

SUPORT1

I

Supported degree-of-freedom set (SUPORT1)

256

STATSUBB

I

Static subcase ID for buckling (STATSUB(BUCKLE))

257

BCID

I

Boundary condition ID (BC)

258

AUXMODEL

I

Auxiliary model ID (AUXMODEL)

259

ADACT

I

P-element adaptivity active subcase flag (ADACT)

260

DATSET

I

P-element output set (DATAREC)

261

DATMEDIA

I

P-element output media (DATAREC)

262

DATFMT

I

P-element output format (DATAREC)

263

VUGSET

I

View-grid and element output set (VUGRID)

264

VUGMEDIA

I

View-grid and element output media (VUGRID)

265

VUGFMT

I

View-grid and element output format (VUGRID)

266

MPCFSET

I

Forces of multipoint constraint output set (MPCFORCE)

267

MPCMEDIA

I

Forces of multipoint constraint output media (MPCFORCE)

268

MPCFFMT

I

Forces of multipoint constraint output format (MPCFORCE)

269

REUESET

I

Real unsymmetric eigenvalue extraction set (UMETHOD)

DMAP Programmer’s Guide

3-37

Chapter 3

Word

Data Block Descriptions A-E

Name

Type

Description

270

DAMPTBLF

I

Structural damping table set for the fluid (SDAMP(FLUID)

271

ITERMETH

I

Iterative solver control parameters (SMETHOD)

272

NLSSET

I

Nonlinear stress output set (NLSTRESS)

273

NLSMEDIA

I

Nonlinear stress output media (NLSTRESS)

274

NLSFMT

I

Nonlinear stress output format (NLSTRESS)

275

MODTRKID

I

Mode tracking control parameter set (MODTRAK)

276

DSAFORM

I

Design sensitivity output format: 1=yes,2=no (DSAPRT)

277

DSAEXPO

I

Design sensitivity output export: 1=no,2=yes (DSAPRT)

278

DSABEGIN

I

Design sensitivity output start iteration (DSAPRT)

279

DSAINTVL

I

Design sensitivity output interval (DSAPRT)

280

DSAFINAL

I

Design sensitivity output final iteration (DSAPRT)

281

DSASETID

I

Design sensitivity output set (DSAPRT)

282

SORTFLG

I

Overall SORT1/SORT2 flag: 1 means SORT1 and 2 means SORT2.

283

RANDBIT

I

Random analysis request bit pattern (DISP,VELO, and so on)

284

AECONFIG(2)

CHAR4

Aerodynamic configuration name

286

AESYMXY

I

Symmetry flag for aerodynamic xy plane

287

AESYMXZ

I

Symmetry flag for aerodynamic xz plane

288

UNDEF

None

289

UNDEF

None

290

UNDEF

None

291

GPEPTSET

I

Grid point strain output set (GPSTRAIN)

292

GPEMEDIA

I

Grid point strain output media (GPSTRAIN)

3-38

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

293

GPEFMT

I

Grid point strain output format (GPSTRAIN)

294

TEMPMAT

I

Thermal material set TEMP(MAT).

295

AECSSSET

I

Aerodynamic Control Surface Schedule (CSSCHD)

296

EKEPTSET

I

Element kinetic energy output set (EKE)

297

EKEMEDIA

I

Element kinetic energy media (EKE)

298

EKEFMT

I

Element kinetic energy format (EKE)

299

EKETHRSH

RS

Element kinetic energy threshold (EKE)

300

EDEPTSET

I

Element damping energy output set (EDE)

301

EDEMEDIA

I

Element damping energy media (EDE)

302

EDEFMT

I

Element damping energy format (EDE)

303

EDETHRSH

RS

Element damping energy threshold (EDE)

304

PANCON

I

Panel contributions set (PANCON)

305

PCMEDIA

I

Panel contributions media (PANCON)

306

PCFMT

I

Panel contributions format (PANCON)

307

PCFORM

I

Panel contributions form (PANCON)

308

PCTOPP

I

Panel contributions TOPP (PANCON)

309

PCTOPG

I

Panel contributions TOPG (PANCON)

310

PCSOL

I

Panel contributions SOLUTION (PANCON)

311

PCPAN

I

Panel contributions PANEL (PANCON)

312

PCGRID

I

Panel contributions GRID (PANCON)

313

MODSLF

I

Mode selection set (fluid)

314

EFFMASET

I

Modal effective mass output set (MEFFMASS)

315

EFFMAGID

I

Modal effective mass GID (MEFFMASS)

316

EFFMATHR

RS

Modal effective mass fraction threshold (MEFFMASS)

DMAP Programmer’s Guide

3-39

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

317

A2GG(2)

CHAR4

Name of direct input (g-set) acoustic coupling matrix (A2GG)

319

RCRSET

I

RCROSS output set

320

RCRFMT

I

RCROSS format

321

AEUXREF

I

AEUXREF

322

GCHK

I

Ground Check Flag (GROUNDCHECK)

323

GCHKOUT

I

Ground Check Output (GROUNDCHECK)

324

GCHKSET

I

Ground Check Set (GROUNDCHECK)

325

GCHKGID

I

Ground Check Gid (GROUNDCHECK)

326

GCHKTHR

RS

Ground Check Thresh (GROUNDCHECK)

327

GCHKRTHR

RS

Ground Check RThresh (GROUNDCHECK)

328

GCHKDREC

I

Ground Check Data recovery (GROUNDCHECK)

329

ASPCMED

I

Output Media Request (AUTOSPC)

330

ASPCEPS

RS

EPS value for fixup (AUTOSPC)

331

ASPCPRT

I

EPS value for printing (AUTOSPC)

332

ASPCPCH

I

Punch Set Id (AUTOSPC)

333

EXSEGEOM

I

External superelement geometry flag (EXTSEOUT)

334

NA2GG

I

Internal set id for A2GG

335

NK2PP

I

Internal set id for K2PP

336

NM2PP

I

Internal set id for M2PP

337

NB2PP

I

Internal set id for B2PP

338

NK2GG

I

Internal set id for K2GG

339

NM2GG

I

Internal set id for M2GG

340

NB2GG

I

Internal set id for B2GG

341

NP2G

I

Internal set id for P2G

3-40

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

342

GEODSET

I

Geometry Check DISP Set identification number (GEOMCHECK)

343

GEODMXMN

I

Geometry Check DISP Max/Min (GEOMCHECK)

344

GEODOCID

I

Geometry Check DISP Max/Min Output Cor. Sys. (GEOMCHECK)

345

GEODNUMB

I

Geometry Check No. of DISP Max/Min Output (GEOMCHECK)

346

GEOLSET

I

Geometry Check OLOAD Set identification number (GEOMCHECK)

347

GEOLMXMN

I

Geometry Check OLOAD Max/Min (GEOMCHECK)

348

GEOLOCID

I

Geometry Check OLOAD Max/Min Output Cor. Sys. (GEOMCHECK)

349

GEOLNUMB

I

Geometry Check No. of OLOAD Max/Min Output (GEOMCHECK)

350

GEOSSET

I

Geometry Check SPCF Set identification number (GEOMCHECK)

351

GEOSMXMN

I

Geometry Check SPCF Max/Min (GEOMCHECK)

352

GEOSOCID

I

Geometry Check SPCF Max/Min Output Cor. Sys. (GEOMCHECK)

353

GEOSNUMB

I

Geometry Check No. of SPCF Max/Min Output (GEOMCHECK)

354

GEOMSET

I

Geometry Check MPCF Set identification number (GEOMCHECK)

355

GEOMMXMN

I

Geometry Check MPCF Max/Min (GEOMCHECK)

356

GEOMOCID

I

Geometry Check MPCF Max/Min Output Cor. Sys. (GEOMCHECK)

357

GEOMNUMB

I

Geometry Check No. of MPCF Max/Min Output (GEOMCHECK)

358

GEOASET

I

Geometry Check ACCE Set identification number (GEOMCHECK)

DMAP Programmer’s Guide

3-41

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

359

GEOAMXMN

I

Geometry Check ACCE Max/Min (GEOMCHECK)

360

GEOAOCID

I

Geometry Check ACCE Max/Min Output Cor. Sys. (GEOMCHECK)

361

GEOANUMB

I

Geometry Check No. of ACCE Max/Min Output (GEOMCHECK)

362

GEOVSET

I

Geometry Check VELO Set identification number (GEOMCHECK)

363

GEOVMXMN

I

Geometry Check VELO Max/Min (GEOMCHECK)

364

GEOVOCID

I

Geometry Check VELO Max/Min Output Cor. Sys. (GEOMCHECK)

365

GEOVNUMB

I

Geometry Check No. of VELO Max/Min Output (GEOMCHECK)

366

NTFL

I

Internal set id for TFL

367

BCONTACT

I

BCONTACT Set identification number

368

GPKESET

I

Grid point kinetic energy output set (GPKE)

369

GPKEMEDI

I

Grid point kinetic energy media (GPKE)

370

GPKEFMT

I

Grid point kinetic energy format (GPKE)

371

ELMSUM

I

Element Summary Output (ELSUM)

372

WCHK

I

Weight Check Flag (WEIGHTCHECK)

373

WCHKOUT

I

Weight Check Output (WEIGHTCHECK)

374

WCHKSET

I

Weight Check Set identification number (WEIGHTCHECK)

375

WCHKGID

I

Weight Check GID (WEIGHTCHECK)

376

WCHKCGI

I

Weight Check CGI (WEIGHTCHECK)

377

WCHKWM

I

Weight Check Weight/Mass units (WEIGHTCHECK)

378

EXSEOUT

I

External Superelement Output Flag

379

EXSEMED

I

External Superelement Output Media

380

EXSEUNIT

I

External Superelement Output Unit

3-42

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

381

EXSEASMB

I

External Superelement Output ASMBULK Flag

382

EXSEEXTB

I

External Superelement Output EXTBULK Flag

383

K42GG(2)

CHAR4

Name of direct input (g-set) structural damping matrix K42GG

385

NK42GG

I

Internal set id for K42GG

386

EXSESTIF

I

External Superelement Output STIFFNESS Flag

387

EXSEMASS

I

External Superelement Output MASS Flag

388

EXSEDAMP

I

External Superelement Output DAMPING Flag

389

EXSEK4DA

I

External Superelement Output K4DAMP Flag

390

EXSELOAD

I

External Superelement Output LOADS Flag

391

EXSESEID

I

External Superelement Output SE ID

392

EXSEDMFX(2)

CHAR4

External Superelement DMIGSFIX String

394

NSMID

I

Non-Structural Mass Set ID

395

UNDEF(2)

None

397

OP4UNIT

I

398

UNDEF

None

399

CHECK

I

ADAMSMNF/MBDEXPORT CHECK flag

400

ADMOUT

I

ADAMSMNF ADMOUT flag//MBDEXPORT RECVROP2 flag

401

FLEXBODY

I

ADAMSMNF/MBDEXPORT FLEXBODY flag

402

FLEXONLY

I

ADAMSMNF/MBDEXPORT FLEXONLY flag

403

MINVAR

I

ADAMSMNF/MBDEXPORT MINVAR parameter

404

PSETID

I

ADAMSMNF/MBDEXPORT PSETID parameter

MBDEXPORT OP4 logical unit number

DMAP Programmer’s Guide

3-43

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

405

OUTGSTRS

I

ADAMSMNF/MBDEXPORT OUTGSTRS flag

406

OUTGSTRN

I

ADAMSMNF/MBDEXPORT OUTGSTRN flag

407

UNDEF(6)

None

413

BCSET

I

Contact Set ID

414

BCRESU

I

Contact results output

415

BCMEDIA

I

Contact results media code

416

BCFMT

I

Contact results format code

417

BCTYPE

I

Traction=1, Force=2, Both=3

418

GKRESU

I

Gasket results output

419

GKMEDIA

I

Gasket results media code

420

GKFMT

I

Gasket results format code

421

UNDEF(5)

None

426

RSMETHOM

I

RSMETHOD parameter

427

ESETHRSH

I

ESE THRESHOLD

428

MDESET

I

Modal energy output set (MODALE)

429

MDEMEDI

I

Modal energy media (MODALE)

430

MCSOL

I

Modal contributions SOLUTION (MODCOM)

431

MCPAN

I

Modal contributions PANELMC (MODCOM)

432

MDEFMT

I

Modal energy output format (MODALE)

433

UNDEF

None

434

MDECMPT

I

Modal energy computation set (MODALE)

435

MDESORT

I

Modal energy sort flag (MODALE)

436

MDETYPE

I

Modal energy type flag (MODALE)

437

MDECALC

I

Modal energy calculation flag (MODALE)

438

RMETSET

I

RMETHOD set id

3-44

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

439

RIGID

I

Rigid element type

440

BOLTPRE

I

Bolt preload set

441

BGSET

I

Glue set id

442

MCTOPF

I

Modal contributions TOPF (MODCON)

443

IPRPU

I

RANDOM print/punch option

444

ADMCHK

I

ADMRECVR ADMCHK flag

445

MODSEL

I

Mode selection set (structural)

446

ADMREC

I

ADMRECVR activation flag

447

ADMFORM

I

ADMRECVR ADMFORM parameter

448

MSRMODE

I

ADMRECVR MSRMODE parameter

449

RGBODY

I

ADMRECVR RGBODY flag

450

MSGLVL

I

ADMRECVR MSGLVL parameter

451

EBDSET

I

Element birth/death set

452

SHELLTHK

I

Shell thickness results output flag

453

STMEDIA

I

Shell thickness results media code

454

STFMT

I

Shell thickness results format code

455

UNDEF(14)

None

469

MCTOPS

I

Modal contributions TOPS (MODCON)

470

PSDD

I

SOL200: int. set no. for grids w/ PSDDISP design response

471

PSDV

I

SOL200: int. set no. for grids w/ PSDVELO design response

472

PSDA

I

SOL200: int. set no. for grids w/ PSDACCL design response

473

ISTAR

I

Start subcase id (RMAXMIN)

474

ISTOP

I

End subcase id (RMAXMIN)

475

FK2PP

I

Internal set id for K2PP scale factor

476

FM2PP

I

Internal set id for M2PP scale factor

DMAP Programmer’s Guide

3-45

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

477

FB2PP

I

Internal set id for B2PP scale factor

478

FK2GG

I

Internal set id for K2GG scale factor

479

FM2GG

I

Internal set id for M2GG scale factor

480

FB2GG

I

Internal set id for B2GG scale factor

481

FK42GG

I

Internal set id for K42GG scale factor

482

FP2G

I

Internal set id for P2G scale factor

483

FA2GG

I

Internal set id for A2GG scale factor

484

GPRSORT

I

Global ply results sorted with global ply ID numbers

485

EFLOAD1

I

External field load orientation

486

EFLOAD2

I

External field coordinate system

487

BGRESU

I

Glue results output

488

BGMEDIA

I

Glue results media code

489

UNDEF

None

490

BGTYPE

I

Glue results type

491

RSVCOMP

I

Residual vector component flag

492

RSVOPTC

I

Residual vector component options

493

RSVSYST

I

Residual vector system flag

494

RSVOPTS

I

Residual vector system options

495

PLSLOC

I

Ply strain or stress locations

496

ELSMOP

I

ELSUM output option

497

UNDEF(103)

None

600

LSEM(C)

I

Number of symmetry subcase coefficients from item SYMFLG

601

COEF

RS

Symmetry subcase coefficients (SUBSEQ or SYMSEQ)

I

Set identification number

Word 601 repeats LSEM times 602

3-46

SETID

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

603

SETLEN(C)

I

Length of this set

604

SETMEM

I

Set member identification number

Word 604 repeats SETLEN times Words 602 through 604 repeat NSETS times 605

PARA

CHAR4

Hard-coded to "PARA"

606

PARLEN(C)

I

Length of this parameter value specification

607

CHTYPE(C)

I

Character type flag: 3 means character, 2 otherwise

608

PARAM(2)

CHAR4

Hard-coded to "PARA" and "M "

610

PNAME(2)

CHAR4

Name of parameter

PARLEN =8 612

Length INTEGER

PARLEN =9

I

Integer value

Real-double parameter value

612

TYPE

I

Real type - hard-coded to -4

613

REAL

RD

Real-double value

PARLEN =10

Complex-single parameter value

612

RTYPE

I

Real part type - hard-coded to -2

613

REAL

RS

Real part value

614

ITYPE

I

Imaginary part type - hard-coded to -2

615

IMAG

RS

Imaginary part value

PARLEN =12

Complex-double parameter value

612

RTYPE

I

Real part type - hard-coded to -4

613

REAL

RD

Real part value

614

ITYPE

I

Imaginary part type - hard-coded to -4

615

IMAG

RD

Imaginary part value

End PARLEN Words 605 through max repeat until NANQ occurs

DMAP Programmer’s Guide

3-47

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

Words 605 through 615 repeat until End of Record

Record – TRAILER Name

Word

Type

Description

1

WORD1

I

Number of records

2

WORD2

I

Number of records

3

WORD3

I

Maximum record length

4

WORD4

I

Plot flag

5

UNDEF(2)

None

Notes: 1. Possible values for output media (___MEDIA) are: •

1 = print

•

2 = plot

•

4 = punch

and their sums; for example, 3 indicates print and plot. 2. Possible values for SORT1 output format (___FMT) are: •

1 = real

•

2 = real/imaginary

•

3 = magnitude/phase

For SORT2, the same values are negative. 3. Possible values for SYMFLG are: •

0 = no symmetry

•

-1 = REPCASE and

•

N = number of SYMSEQ or SUBSEQ coefficients

4. Possible values for DSAPRT are:

3-48

•

1 = Print (default)

•

0 = No print

DMAP Programmer’s Guide

Data Block Descriptions A-E

5. Possible values for DSASTORE are: •

1 = Store on data base and

•

0 = Don’t store on data base (default)

6. Possible values for DSAOUTPT are: •

1 = Store via OUTPUT2 and

•

0 = Don’t store via OUTPUT2 (default)

7. Possible values for AXSYMSET are: •

1 = Sine

•

2 = Cosine or fluid

8. Possible values for the SECMDFLG are: •

0 = at least one of SEMG, SEKR, SEMR, SELG, SELR or SEALL is specified

•

-1 = None are specified

9. DSAFINAL=-1 means the last iteration. 10. DSASETID=-1 means the all design sensitivities. 11. RANDBIT contains bit pairs for the selection of PSDF and ATOC beginning with left handed bits 1 and 2 for DISP and continuing with VELO, ACCE, OLOAD, SPCF, STRESS, FORCE, STRAIN, and MPCF Case Control commands for bits 3 through 18. The bit pair value of "00" means none, "01" means ATOC, "10" means PSDF, and "11" means RALL. 12. Possible values for AESYMXY and AESYMXZ are: •

2 = antisymmetric

•

3 = asymmetric

•

4 = antisymmetric

3.6 CDDATA Campbell diagram data table.

Record 0 – HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

METH

I

Mode tracking method. = 1 : method 1 is used = 2 : method 2 is used

DMAP Programmer’s Guide

3-49

Chapter 3

Data Block Descriptions A-E

Record 1 – List of rotor speeds (METH=1 only) Name

Word

Type

Description

1

NVAL

I

2

UNDEF

None

3

KEYW

I

Keyword=10001

4

ROTS(NVAL)

RS

List of rotor speeds in user-defined units

Number of values

Record 2 – List of eigenfrequencies in the analysis system (METH=1 only) Word

Name

Type

Description

1

NVAL

I

2

UNDEF

None

3

KEYW

I

Keyword=20000+SOLN, where SOLN=solution number

4

EIGF(NVAL)

RS

Eigenfrequencies for solution SOLN

Number of values

Words 3 and 4 repeat for all solutions.

Record 3 – List of Lehr damping values (METH=1 only) Word

Name

Type

Description

1

NVAL

I

2

UNDEF

None

3

KEYW

I

Keyword=30000+SOLN, where SOLN=solution number

4

DAMP(NVAL)

RS

Damping values for solution SOLN

Number of values

Words 3 and 4 repeat for all solutions.

Record 4– List of real eigenvalues (METH=1 only) Word

Name

Type

1

NVAL

I

2

UNDEF

None

3-50

DMAP Programmer’s Guide

Description Number of values

Data Block Descriptions A-E

Word

Name

Type

Description

3

KEYW

I

Keyword=40000+SOLN, where SOLN=solution number

4

EIGV(NVAL)

RS

Eigenvalues for solution SOLN

Words 3 and 4 repeat for all solutions.

Record 5 – List of whirl direction codes (2.0=backwards, 3.0 forward, 4.0=linear) (METH=1 only) Word

Name

Type

Description

1

NVAL

I

2

UNDEF

None

3

KEYW

I

Keyword=50000+SOLN, where SOLN=solution number

4

WHRD(NVAL)

RS

Whirl direction codes for solution SOLN

Number of values

Words 3 and 4 repeat for all solutions.

Record 6 – List of converted frequencies in analysis system (METH=1 only) Word

Name

Type

Description

1

NVAL

I

2

UNDEF

None

3

KEYW

I

Keyword=60000+SOLN, where SOLN=solution number

4

FREQ(NVAL)

RS

Converted frequencies for solution SOLN

Number of values

Words 3 and 4 repeat for all solutions.

Record 7– List of whirl direction codes for converted solution (2.0=backwords, 3.0 forward, 4.0=linear) (METH=1 only) Word

Name

Type

1

NVAL

I

2

UNDEF

None

Description Number of values

DMAP Programmer’s Guide

3-51

Chapter 3

Word

Data Block Descriptions A-E

Name

Type

3

KEYW

4

CWHRD(NVAL) RS

I

Description Keyword=70000+SOLN, where SOLN=solution number Whirl direction codes for solution SOLN

Words 3 and 4 repeat for all solutions.

Record 1 – Data (METH=2 only) Name

Word

Type

Description

1

NVAL

I

Number of values

2

NCRV

I

Number of sections/solution (i.e., number of curves)

3

KEYW

I

Keyword=10000+(SOLN*10)+DATTYP, where: SOLN=solution number DATTYP=1 for list of rotor speeds in user-defined units DATTYP=2 for list of eigenfrequencies in the analysis system DATTYP=3 for list of Lehr damping values DATTYP=4 for list of real part of eigenvalues DATTYP=5 for list of imaginary part of eigenvalues DATTYP=6 for list of whirl direction codes (2.0=backwards, 3.0=forward, 4.0=linear) DATTYP=7 for list of converted frequencies in analysis system DATTYP=8 for list of whirl directions codes for converted solution (2.0=backwards, 3.0=forward, 4.0=linear)

4

VALS(NVAL)

RS

List of values

Words 1–4 repeat for NCRV curves. For DATTYP≠1, NVAL and NCRV=0 Record 1 repeats NSOL times.

Record 8 – TRAILER Word

Name

Type

Description

1

NOMG

I

Number of speed values

2

NSOL

I

Number of solutions

3-52

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

3

WORD3

I

4

UNDEF

None

5

METH

I

6

UNDEF

None

Description Number of records (METH=1); number of sections per solution (i.e. NCRV, METH=2)

Mode tracking method. = 1 : method 1 is used = 2 : method 2 is used

3.7 CLAMA Complex eigenvalue summary table

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – OFPID Name

Word

Type

Description

1

RECID(2)

I

3

UNDEF(7 )

None

10

SIX

I

11

UNDEF(40 )

None

51

TITLE(32)

CHAR4

Title character string (TITLE)

83

SUBTITLE(32)

CHAR4

Subtitle character string (SUBTITLE)

115

LABEL(32)

CHAR4

LABEL character string (LABEL)

Constants 90 and 1006

Constant 6

Record 2 – LAMA Repeats for each eigenvalue. Word 1

Name MODE

Type I

Description Mode number

DMAP Programmer’s Guide

3-53

Chapter 3

Word

Data Block Descriptions A-E

Name

Type

Description

2

ORDER

I

Extraction order

3

REIGEN

RS

Eigenvalue – real part

4

IEIGEN

RS

Eigenvalue – imaginary part

5

FREQ

RS

Frequency: ABS(IEIGEN)/(2*Pi)

6

DAMP

RS

Damping Coefficient: (-2*REIGEN)/ABS(IEIGEN)

Record 3 – TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(3 )

None

5

SIX

I

6

UNDEF

None

Description 1006

Constant 6

3.8 CONTAB Design constraint table Contains a record for each design constraint. Records are sorted by the internal constraint identification number.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – Repeat – Repeated for each design constraint Word

Name

Type

Description

1

IDCID

I

Internal design constraint identification number

2

DCID

I

DCONSTR Bulk Data entry identification number

3

IRID

I

Internal response identification number

4

RTYPE

I

Response type

3-54

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

5

TYPE

I

Type of response (1 or 2)

6

LUFLAG

I

Bound Type (1=lower,2=upper)

7

BOUND

RS

Bound value

8

REGION

I

Internal region identification number

9

SCID

I

Subcase identification number

Record 2 – TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of records; that is, design constraints

3.9 CONTACT Table of Bulk Data entry related to surface contact

Record – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record – BCMATL (7310,73,590) Name

Word

Type

Description

1

ID

I

Identification number

2-n

IPi

I

Material ID

n+1

-1

I

Delimiter

Record – BCPROP (7210,72,589) Name

Word

Type

Description

1

ID

I

Identification number

2-n

IPi

I

Physical Property ID

DMAP Programmer’s Guide

3-55

Data Block Descriptions A-E

Chapter 3

Name

Word n+1

-1

Type I

Description Delimiter

Record – BCPROPS (8301,83,605) Name

Word

Type

Description

1

ID

I

Identification number

2-n

IPi

I

Physical Property ID

n+1

-1

I

Delimiter

Record – BCRPARA (7710,77,594) Name

Word

Type

Description

1

CRID

I

Region ID

2

SURF

I

TOP=1, BOT=2

3

OFFSET

RS

≥ 0.0 offset distance

4

TYPE

I

FLEX=1, RIGID=2

5

MGP

I

Master grid point

Record – BCTADD (7510,75,592) Name

Word

Type

Description

1

CSID

I

Combined contact set ID

2-n

Si

I

Contact set ID

n+1

-1

I

Delimiter

Record – BCTPARA (7610,76,593) Note: entry 2-5 repeats for each parameter Word

Name

Type

Description

1

CSID

I

Contact set ID

2-3

Param(i)

CHAR4

Parameter name

4

TYPE

I

Parameter data type

3-56

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

5

Value(i)

I or RS

Parameter value

6

-1

I

Delimiter

Record – BCTPARM (8110,81,598) Note: entry 2-5 repeats for each parameter Name

Word

Type

Description

1

CSID

I

Contact set ID

2-3

Param(i)

CHAR4

Parameter name

4

TYPE

I

Parameter data type

5

Value(i)

I or RS

Parameter value (See Note 1 below)

6

-1

I

Delimiter

Note: 1. The parameter NCHG can now be entered as a real or an integer value, but is always written to the OP2 file as a real value. For example, the integer value NCHG=1 is written to the OP2 file as NCHG=1.0.

Record – BCTSET (7410,74,591) Note: entry 2-6 repeats for each additional region pair. Name

Word

Type

Description

1

CSID

I

Contact set ID

2

SIDi

I

Source region ID

3

TIDi

I

Target region ID

4

FRICi

RS

Coefficient of Friction

5

MIND

RS

Minimum search distance

6

MAXD

RS

Maximum search distance

7

-1

I

Delimiter

DMAP Programmer’s Guide

3-57

Data Block Descriptions A-E

Chapter 3

Record – BGADD (8810,88,603) Name

Word

Type

Description

1

GSID

I

Combined glue set ID

2-n

Si

I

Glue set ID

n+1

-1

I

Delimiter

Record – BGPARM (8710,87,449) Note: entry 2-5 repeats for each parameter Name

Word

Type

Description

1

CSID

I

Contact set ID

2-3

Param(i)

CHAR4

Parameter name

4

TYPE

I

Parameter data type

5

Value(i)

I or RS

Parameter value

6

-1

I

Delimiter

Record – BGSET (1224,12,446) Name

Word

Type

Description

1

CSID

I

Contact set ID

2

SIDi

I

Source region ID

3

TIDi

I

Target region ID

4

SDIST

RS

Search distance

5

PEN

RS

Penalty value

6

EXT

RS

Extension factor for target region

7

-1

I

Delimiter

Record – BLSEG (0224,02,436) Name

Word 1

3-58

ID

DMAP Programmer’s Guide

Type I

Description Identification number.

Data Block Descriptions A-E

Name

Word

Type

Description

2-n

Gi

I

Grid point identification numbers.

n+1

-1

I

Delimiter

Record – BSURF (724,7,441) Name

Word

Type

Description

1

ID

I

Identification number

2-n

EIDi

I

Element ID

n+1

-1

I

Delimiter

Record – BSURFS (7110,71,588) Note: entry 2-5 repeats for each element/grids Name

Word

Type

Description

1

ID

I

Identification number

2

EIDi

I

Element ID

3-5

G1 - G3

I

Grid point ID

6

-1

I

Delimiter

Record – EBDADD (8610,86,448) Name

Word

Type

Description

1

ID

I

Resulting Birth/Death set ID number

2-n

BDID

I

Birth/Death set ID’s defined via EBDSET entries

n+1

-1

I

Delimiter

Record – EBDSET (8510,85,447) Name

Word

Type

Description

1

ID

I

Birth/Death set ID number

2

TBIRTH

RS

Element birth time

3

TDEATH

RS

Element death time

DMAP Programmer’s Guide

3-59

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

EID

I

Element ID’s

6

-1

I

Delimiter

Record – NXSTRAT (7810,78,595) Note: entry 2-5 repeats for each parameter Name

Word

Type

Description

1

ID

I

ID (not used)

2-3

Param (i)

CHAR4

Parameter name

4

TYPE

I

Parameter data type

5

Value(i)

I or RS

Parameter value

6

-1

I

Delimiter

Record – TMCPARA (7910,79,989) Note: entry 2-5 repeats for each parameter Name

Word

Type

Description

1

CSID

I

Contact set ID

2-3

Param(i)

CHAR4

Parameter name

4

TYPE

I

Parameter data type

5

Value(i)

I or RS

Parameter value

6

-1

I

Delimiter

TRAILER Name

Word 1-6

UNDEF(6)

Type None

3.10 CSTM Coordinate system transformation matrices table The transformation is from global to basic.

3-60

DMAP Programmer’s Guide

Description

Data Block Descriptions A-E

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – IDENT Word

Name

Type

Description

1

CID

I

Coordinate system identification number

2

TYPE

I

Type of system

3

IINDEX

I

Index into INTDATA record

4

RINDEX

I

Index into REALDATA record

Record 2 – REALDATA Word 1

Name

Type RX

REALDATA

Description Real data

Record 3 – INTDATA Word 1

Name

Type I

INTDATA

Description Integer data

Record 4 – TRAILER Word

Name

Type

Description

1

WORD1

I

Number of grid points + number of scalar points

2

WORD2

I

Number of coordinate systems

3

WORD3

I

Type of systems present – see Note 1.

4

WORD4

I

Precision of REALDATA record - 1 or 2

5

WORD5

I

Length of REALDATA record

6

WORD6

I

Length of INTDATA record

DMAP Programmer’s Guide

3-61

Data Block Descriptions A-E

Chapter 3

Notes: 1. Coordinate system type as specified in IDENT:TYPE and by bit numbers numbered right to left in TRAILER:WORD3: 1 = rectangular 2 = cylindrical 3 = spherical 4 = convective – defined on a GMCURV+GMSURF pair 5 = convective – defined on a GMSURF 6 = convective – defined on a FEEDGE+FEFACE pair 7 = convective – defined on a FEFACE 8 = general – sequence of rotational angles on CORD3G entry 2. REALDATA is intended for IDENT:TYPE’s 1, 2, and 3 and contains real data similar to CSTM68. 3. INTDATA is intended for IDENT:TYPE’s 4 through 8 and contains GMCURV, and so on. Identification numbers similar to CSTM68. XYZi data found in CSTM68 are converted to grid entry indices into BGPDT.

3.11 CSTM68 Coordinate system transformation matrices table (Pre-MSC Nastran Version 69). The transformation is from global to basic. Note See the Note 2 for a listing of the differences between CSTM68 and CSTM.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data Block Name

Record 1 – HEADER Word

Name

Type

Description

1

CID

I

Coordinate system identification number

2

CIDTYPE

I

Coordinate system type

Word

Name

CIDTYPE =0

3-62

DMAP Programmer’s Guide

Type Unknown

Description

Data Block Descriptions A-E

Word

Name

Type

Description

3

TR1

RS

Translation in direction 1

4

TR2

RS

Translation in direction 2

5

TR3

RS

Translation in direction 3

6

R11

RS

Direction cosine in 1-1

7

R12

RS

Direction cosine in 1-2

8

R13

RS

Direction cosine in 1-3

9

R21

RS

Direction cosine in 2-1

10

R22

RS

Direction cosine in 2-2

11

R23

RS

Direction cosine in 2-3

12

R31

RS

Direction cosine in 3-1

13

R32

RS

Direction cosine in 3-2

14

R33

RS

Direction cosine in 3-3

Word

Name

CIDTYPE =1

Type

Description

Rectanglar

3

TR1

RS

Translation in direction 1

4

TR2

RS

Translation in direction 2

5

TR3

RS

Translation in direction 3

6

R11

RS

Direction cosine in 1-1

7

R12

RS

Direction cosine in 1-2

8

R13

RS

Direction cosine in 1-3

9

R21

RS

Direction cosine in 2-1

10

R22

RS

Direction cosine in 2-2

11

R23

RS

Direction cosine in 2-3

12

R31

RS

Direction cosine in 3-1

13

R32

RS

Direction cosine in 3-2

14

R33

RS

Direction cosine in 3-3

DMAP Programmer’s Guide

3-63

Chapter 3

Word

Data Block Descriptions A-E

Name

CIDTYPE =2

Type

Description

Cylindrical

3

TR1

RS

Translation in direction 1

4

TR2

RS

Translation in direction 2

5

TR3

RS

Translation in direction 3

6

R11

RS

Direction cosine in 1-1

7

R12

RS

Direction cosine in 1-2

8

R13

RS

Direction cosine in 1-3

9

R21

RS

Direction cosine in 2-1

10

R22

RS

Direction cosine in 2-2

11

R23

RS

Direction cosine in 2-3

12

R31

RS

Direction cosine in 3-1

13

R32

RS

Direction cosine in 3-2

14

R33

RS

Direction cosine in 3-3

Word

Name

CIDTYPE =3

Type

Description

Spherical

3

TR1

RS

Translation in direction 1

4

TR2

RS

Translation in direction 2

5

TR3

RS

Translation in direction 3

6

R11

RS

Direction cosine in 1-1

7

R12

RS

Direction cosine in 1-2

8

R13

RS

Direction cosine in 1-3

9

R21

RS

Direction cosine in 2-1

10

R22

RS

Direction cosine in 2-2

11

R23

RS

Direction cosine in 2-3

12

R31

RS

Direction cosine in 3-1

13

R32

RS

Direction cosine in 3-2

3-64

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word 14

Name R33

Word

Type

CIDTYPE =4

Direction cosine in 3-3

RS

Name

Description

Type

Description

Convective defined on a GMCURV+GMSURF pair

3

UNDEF(2 )

None

Reserved

5

CURVID

I

GMCURV identification number

6

SURFID

I

GMSURF identification number

7

CURCID

I

Coordinate System where GMCURV is defined

8

SURCID

I

Coordinate System where GMSURF is defined

9

UNDEF(6 )

None

Reserved

Word

Name

CIDTYPE =5

Type

Description

Convective defined on a GMSURF

3

UNDEF(2 )

None

Reserved

5

SURFID

I

GMSURF identification number

6

SURCID

I

Coordinate System where GMSURF is defined

7

UNDEF(8 )

None

Reserved

Word

Name

CIDTYPE =6 3

Type

Description

Convective defined on a FEEDGE+FEFACE pair RECINDX

RECINDX =1

I

Record index number

Index 1

4

RECTOTAL

I

Total number of records ( = 8 )

5

EDGEID

I

FEEDGE identification number

6

FACEID

I

FEFACE identification number

7

GP(4)

I

Grid identification numbers of 4 FEEDGE grids

11

GFACE(4)

I

Grid identification numbers of 1st 4 of 12 FEFACE grids

DMAP Programmer’s Guide

3-65

Chapter 3

Word

Data Block Descriptions A-E

Name

RECINDX =2

Type

Description

Index 2

4

RECTOTAL

I

Total number of records ( = 8 )

5

GFACE(8)

I

Grid identification number of next 8 of 12 FEFACE grids

13

UNDEF(2 )

None

Reserved

RECINDX =3

Index 3

4

RECTOTAL

I

Total number of records ( = 8 )

5

XYZ1(3)

RS

Basic Coordinates of FEEDGE grid 1

8

XYZ2(3)

RS

Basic Coordinates of FEEDGE grid 2

11

XYZ(3)

RS

Basic Coordinates of FEEDGE grid 3

14

UNDEF

None

Reserved

RECINDX =4

Index 4

4

RECTOTAL

I

Total number of records ( = 8 )

5

XYZ1(3)

RS

Basic Coordinates of FEEDGE grid 4

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 1

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 2

14

UNDEF

None

Reserved

RECINDX =5

Index 5

4

RECTOTAL

I

Total number of records ( = 8 )

5

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 3

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 4

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 5

14

UNDEF

None

Reserved

RECINDX =6

Index 6

4

RECTOTAL

I

Total number of records ( = 8 )

5

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 6

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 7

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Data Block Descriptions A-E

Name

Word

Type

Description

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 8

14

UNDEF

None

Reserved

RECINDX =7

Index 7

4

RECTOTAL

I

Total number of records ( = 8 )

5

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 9

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 10

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 11

14

UNDEF

None

Reserved

RECINDX =8

Index 8

4

RECTOTAL

I

Total number of records ( = 8 )

5

XYZ(3)

RS

Basic Coordinates of FEFACE grid 12

8

UNDEF(7 )

None

Reserved

End RECINDX Word

Name

CIDTYPE =7 3

Type

Description

Convective defined on a FEFACE RECINDX

RECINDX =1

I

Record index number

Index 1

4

RECTOTAL

I

Total number of records ( = 6 )

5

FACEID

I

FEFACE identification number

6

GFACE(9)

I

Grid IDs of first 9 of 12 FEFACE grids

RECINDX =2

Index 2

4

RECTOTAL

I

Total number of records ( = 6 )

5

GFACE(3)

I

Grid IDs of next 3 of 12 FEFACE grids

8

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 1

11

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 2

14

UNDEF

None

Reserved

DMAP Programmer’s Guide

3-67

Data Block Descriptions A-E

Chapter 3

Name

Word RECINDX =3

Type

Description

Index 3

4

RECTOTAL

I

Total number of records ( = 6 )

5

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 3

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 4

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 5

14

UNDEF

None

Reserved

RECINDX =4

Index 4

4

RECTOTAL

I

Total number of records ( = 6 )

5

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 6

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 7

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 8

14

UNDEF

None

Reserved

RECINDX =5

Index 5

4

RECTOTAL

I

Total number of records ( = 6 )

5

XYZ1(3)

RS

Basic Coordinates of FEFACE grid 9

8

XYZ2(3)

RS

Basic Coordinates of FEFACE grid 10

11

XYZ(3)

RS

Basic Coordinates of FEFACE grid 11

14

UNDEF

None

Reserved

RECINDX =6

Index 6

4

RECTOTAL

I

Total no of records. Should be 6

5

XYZ(3)

RS

Basic Coordinates of FEFACE grid 12

8

UNDEF(7 )

None

Reserved

End RECINDX End CIDTYPE

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Data Block Descriptions A-E

Record 2 – TRAILER Word

Name

Type

Description

1

WORD1

I

Number of grid and scalar points

2

WORD2

I

Number of coordinate systems

3

UNDEF(4 )

None

Notes: 1. Coordinate system type: •

1 = rectangular

•

2 = cylindrical

•

3 = spherical

•

4 = convective coordinate system defined on a GMCURV+GMSURF pair

•

5 = convective coordinate system defined on a GMSURF

•

6 = convective coordinate system defined on a FEEDGE+FEFACE pair

•

7 = convective coordinate system defined on a FEFACE

2. CSTM68 contains the same data as CSTM. However, CSTM68 and CSTM are organized differently. For details, compare individual records between CSTM68 and CSTM.

3.12 DBCOPT Design optimization history table for postprocessing

Record 0 – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data Block Name

Record 1 – EXACT Word 1

Name REAL

Type RS

Description Objective function values, exact from analysis

Word 1 repeats until End of Record

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Data Block Descriptions A-E

Record 2 – APPRX Word 1

Name

Type

REAL

RS

Description Objective function values, optimal w.r.t approximation

Word 1 repeats until End of Record

Record 3 – MAXIM Word 1

Name

Type

REAL

RS

Description Objective function values, maximum values of constraints

Word 1 repeats until End of Record

Record 4 – DVIDS Word 1

Name

Type I

INTGR

Description Design variable identification number

Word 1 repeats until End of Record

Record 5 – INITV Word 1

Name REAL

Type RS

Description Design variable values, 1st cycle ?

Word 1 repeats until End of Record

Record 6 – COL17 Word 1

Name REAL

Type RS

Description Design variable value, Nth cycle ?

Word 1 repeats until End of Record

Record 7 – DVLABEL Word 1

3-70

Name IDVID

DMAP Programmer’s Guide

Type I

Description Internal design variable identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

DVID

I

External design variable identification number

3

LABEL1

CHAR4

First part of design variable

4

LABEL2

CHAR4

Second part of design variable

Record 8 – TRAILER Name

Word

Type

Description

1

NFEA

I

Number of finite element analyses

2

NAOP

I

Number of optimization cycles w.r.t. approximate model

3

NDV

I

Number of design variables

4

NCC

I

Convergence criterion

5

UNDEF(2 )

None

Notes: Convergence criterion 1 = Hard convergence 2 = Soft convergence 3 = Compromise 4 = Maximum design cycles reached

3.13 DESCYC Defines the design cycle to which the results data blocks that follow belong, up to the next design cycle data block (i.e. the next DESCYC).

Record – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data Block Name

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Chapter 3

Data Block Descriptions A-E

Record – DATA Name

Word

Type

Description

1

DESCYCL

I

Design cycle number

2

CONDIS(2)

CHAR4

Design cycle type; “D” for discretized design cycle; Blank for continuous design cycle

Record – TRAILER Name

Word

Type

Description

1

“1”

I

Always “1”

2

DESCYCL

I

Design cycle number

3

CYCTYP

I

Design cycle type; “0” for a continuous design cycle; “1” for a discretized design cycle

4

UNDEF(3)

None

3.14 DESTAB Design variable attributes

Record – HEADER Word 1

Name

Type CHAR4

NAME(2)

Description Data Block Name

Record – Repeat Word

Name

Type

Description

1

IDVID

I

Internal design variable identification number

2

DVID

I

External design variable identification number

3

LABEL1

CHAR4

First part of design Variable

4

LABEL2

CHAR4

Second part of design Variable

5

VMIN

RS

Lower bound

6

VMAX

RS

Upper bound

7

DELX

RS

Move limit for a design cycle

3-72

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Data Block Descriptions A-E

Record – TRAILER Name

Word

Type

Description

1

NDV

I

Number of design variables

2

NDVI

I

Number of independent design variables

3

NDVD

I

Number of dependent design variables

4

UNDEF(3 )

None

Notes: Independent design variables are given first in ascending IDVID followed by dependent design variables in ascending IDVID order.

3.15 DISTL Direct table input table for RS Contains the load set labels on DTI bulk data entries.

Record – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record – REPEAT Name

Word

Type

Description

1

ID

I

Load set identification number

2

STRING(2)

CHAR4

String label

Words 2 and 3 repeat until End of Record

Record – TRAILER Word

Name

Type

Description

1

WORD1

I

= 32767

2

WORD2

I

= 32767

3

WORD3

I

= 32767

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

WORD4

I

= 32767

5

WORD5

I

= 32767

6

WORD6

I

= 32767

3.16 DIT Direct input tables Contains images of TABLEij, TABDMP1 and GUST Bulk Data entries.

Record 0 – HEADER Name

Word 1

Type

Description

CHAR4

NAME(2)

Data Block Name

Record 1 – GUST(1005,10,174) Name

Word

Type

Description

1

SID

I

Gust load identification number

2

DLOAD

I

TLOADi or RLOADi identification number

3

WG

RS

Scale factor

4

X0

RS

Streamwise location of the gust reference point

5

V

RS

Velocity of vehicle

Record 2 – TABDMP1(15,21,162) Name

Word

Type

Description

1

ID

I

2

UNDEF(7 )

None

9

F

RS

Natural frequency

10

G

RS

Damping

Table identification number

Words 9 through 10 repeat until (-1,-1) occurs

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Data Block Descriptions A-E

Record 3 – TABLE3D(4000,40,460) Name

Word

Type

Description

1

ID

I

Table identification number

2

X0

RS

X offset of the independent variable

3

Y0

RS

Y offset of the independent variable

4

Z0

RS

Z offset of the independent variable

5

F0

RS

Offset of the dependent variable

6

UNDEF(3 )

None

9

XI

RS

X independent variable

10

YI

RS

Y independent variable

11

ZI

RS

Z independent variable

12

FI

RS

Dependent variable

Words 9 through 12 repeat until End of Record

Record 4 – TABLED1(1105,11,133) Name

Word

Type

Description

1

ID

I

Table identification number

2

CODEX

I

Type of interpolation for the x-axis

3

CODEY

I

Type of interpolation for the y-axis

4

UNDEF(5 )

None

9

X

RS

X tabular value

10

Y

RS

Y tabular value

Words 9 through 10 repeat until (-1,-1) occurs

Record 5 – TABLED2(1205,12,134) Name

Word

Type

Description

1

ID

I

Table identification number

2

X1

RS

X-axis shift

DMAP Programmer’s Guide

3-75

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

3

UNDEF(6 )

None

9

X

RS

X value

10

Y

RS

Y value

Words 9 through 10 repeat until (-1,-1) occurs

Record 6 – TABLED3(1305,13,140) Name

Word

Type

Description

1

ID

I

Table identification number

2

X1

RS

X-axis shift

3

X2

RS

X-axis normalization

4

UNDEF(5 )

None

9

X

RS

X value

10

Y

RS

Y value

Words 9 through 10 repeat until (-1,-1) occurs

Record 7 – TABLED4(1405,14,141) Name

Word

Type

Description

1

ID

I

Table identification number

2

X1

RS

X-axis shift

3

X2

RS

X-axis normalization

4

X3

RS

X value when x is less than X3

5

X4

RS

X value when x is greater than X4

6

UNDEF(3 )

None

9

A

RS

Word 9 repeats until End of Record

Record 8 – TABLEM1(105,1,93) Same as record TABLED1 description Record 4 – TABLED1(1105,11,133)

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Data Block Descriptions A-E

Record 9 – TABLEM2(205,2,94) Same as record TABLED2 description Record 5 – TABLED2(1205,12,134)

Record 10 – TABLEM3(305,3,95) Same as record TABLED3 description Record 10 – TABLEM3(305,3,95)

Record 11 – TABLEM4(405,4,96) Same as record TABLED4 description Record 7 – TABLED4(1405,14,141)

Record 12 – TABLES1(3105,31,97) Name

Word

Type

Description

1

ID

I

2

UNDEF(7 )

None

9

X

RS

X value

10

Y

RS

Y value

Table identification number

Words 9 through 10 repeat until (-1,-1) occurs

Record 13 – TABLEST(1905,19,178) Name

Word

Type

Description

1

ID

I

2

UNDEF(7 )

None

9

TI

RS

Temperature

10

TIDI

I

TABLES1 Bulk Data entry identification number

Table identification number

Words 9 through 10 repeat until (-1,-1) occurs

Record 14 – TABRND1(55,25,191) Name

Word

Type

Description

1

ID

I

Table identification number

2

CODEX

I

Type of interpolation for the x-axis

3

CODEY

I

Type of interpolation for the y-axis

DMAP Programmer’s Guide

3-77

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

UNDEF(5 )

None

9

F

RS

Frequency

10

G

RS

Power spectral density

Words 9 through 10 repeat until (-1,-1) occurs

Record 15 – TABRNDG(56,26,303) Power spectral density for gust loads in aeroelastic analysis Name

Word

Type

Description

1

ID

I

Table identification number

2

TYPE

I

Power spectral density type

3

LU

RS

Scale of turbulence divided by velocity

4

WG

RS

Root-mean-square gust velocity

5

UNDEF(4 )

None

Words 1 through 8 repeat until (-1,-1) occurs

Record 16 – TRAILER Word

Name

Type

Description

1

WORD1

I

Record presence trailer word 1

2

WORD2

I

Record presence trailer word 2

3

UNDEF(4 )

None

Notes: Type of interpolation (CODEX and CODEY): 0 = linear 1 = log

3.17 DSCMCOL Design sensitivity parameters

3-78

DMAP Programmer’s Guide

Data Block Descriptions A-E

Record 0 – HEADER Name

Word 1

Type

Description

CHAR4

NAME(2)

Data Block Name

Record 1 – TYPE1 – Type 1 Responses Word

Name

Type

Description

1

IRID

I

Internal response identification number

2

RID

I

External response identification number

3

RTYPE

I

Response Type

Word

Name

RTYPE =1

Type Weight

4

UNDEF(5 )

None

9

SEID

I

Word

Name

RTYPE =2

Superelement identification number Type

UNDEF(5 )

None

9

SEID

I

Name

RTYPE =3

Superelement identification number Type

MODE

I

5

UNDEF

None

6

SUBCASE

I

7

UNDEF(2 )

None

9

SEID

I

RTYPE =4

Description

Buckling

4

Word

Description

Volume

4

Word

Description

Name

Mode number

Subcase identification number

Superelement identification number Type

Description

Normal modes

DMAP Programmer’s Guide

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Chapter 3

Data Block Descriptions A-E

Name

Word

Type

4

MODE

I

5

UNDEF

None

6

SUBCASE

I

7

UNDEF(2 )

None

9

SEID

I

Name

Word RTYPE =5

Description Mode number

Subcase identification number

Superelement identification number Type

Description

Static displacement

4

GRID

I

Grid identification number

5

COMP

I

Displacement component number

6

SUBCASE

I

Subcase identification number

7

UNDEF(2 )

None

9

SEID

I

Name

Word RTYPE =6

Superelement identification number Type

Description

Static stress

4

EID

I

Element identification number

5

COMP

I

Stress component number

6

SUBCASE

I

Subcase identification number

7

UNDEF(2 )

None

9

SEID

I

Name

Word RTYPE =7

Superelement identification number Type

Description

Static strain

4

EID

I

Element identification number

5

COMP

I

Strain component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

3-80

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

8

VIEWID

I

View element identification number

9

SEID

I

Superelement identification number

Name

Word RTYPE =8

Type

Description

Static force

4

EID

I

Element identification number

5

COMP

I

Force component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

VIEWID

I

View element identification number

9

SEID

I

Superelement identification number

Name

Word RTYPE =9

Type

Description

Composite failure

4

EID

I

Element identification number

5

COMP

I

Failure component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

PLY

I

Ply number

9

SEID

I

Superelement identification number

Name

Word RTYPE =10

Type

Description

Composite stress

4

EID

I

Element identification number

5

COMP

I

Stress component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

PLY

I

Ply number

DMAP Programmer’s Guide

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Chapter 3

Data Block Descriptions A-E

Name

Word 9

SEID

Type I

Name

Word RTYPE =11

Description Superelement identification number

Type

Description

Composite strain

4

EID

I

Element identification number

5

COMP

I

Strain component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

PLY

I

Ply number

9

SEID

I

Superelement identification number

Name

Word RTYPE =13

Type

Description

Static SPC force

4

GRID

I

Grid identification number

5

COMP

I

SPC force component number

6

SUBCASE

I

Subcase identification number

7

UNDEF(2)

None

9

SEID

I

Name

Word RTYPE =14

Superelement identification number Type

Description

Element static strain energy

4

EID

I

Element identification number

5

COMP

I

Strain energy component number

6

SUBCASE

I

Subcase identification number

7

UNDEF(2)

None

9

SEID

I

3-82

DMAP Programmer’s Guide

Superelement identification number

Data Block Descriptions A-E

Word

Name

RTYPE =20

Type

Description

Frequency response displacement

4

GRID

I

Grid identification number

5

COMP

I

Displacement component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =21

Superelement identification number Type

Description

Frequency response velocity

4

GRID

I

Grid identification number

5

COMP

I

Velocity component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =22

Superelement identification number Type

Description

Frequency response acceleration

4

GRID

I

Grid identification number

5

COMP

I

Acceleration component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

UNDEF

None

9

SEID

I

Word RTYPE =23

Name

Superelement identification number Type

Description

Frequency response SPC Force

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Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

4

GRID

I

Grid identification number

5

COMP

I

SPC Force component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

UNDEF

None

9

SEID

I

Name

Word RTYPE =24

Superelement identification number Type

Description

Frequency response stress

4

EID

I

Element identification number

5

COMP

I

Stress component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

UNDEF

None

9

SEID

I

Name

Word RTYPE =25

Superelement identification number Type

Description

Frequency response force

4

EID

I

Element identification number

5

COMP

I

Force component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =26 4

3-84

Superelement identification number Type

Description

RMS displacement GRID

DMAP Programmer’s Guide

I

Grid identification number

Data Block Descriptions A-E

Word

Name

Type

Description

5

COMP

I

RMS displacement component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

RANDPS

I

RANDPS ID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =27

Type

Description

RMS velocity

4

GRID

I

Grid identification number

5

COMP

I

RMS velocity component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

RANDPS

I

RANDPS ID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =28

Type

Description

RMS acceleration

4

GRID

I

Grid identification number

5

COMP

I

RMS acceleration component number

6

SUBCASE

I

Subcase identification number

7

UNDEF

None

8

RANDPS

I

RANDPS ID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =29

Type

Description

PSD displacement

4

GRID

I

Grid identification number

5

COMP

I

PSD displacement component number

DMAP Programmer’s Guide

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Chapter 3

Word

Data Block Descriptions A-E

Name

Type

Description

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

RANDPS

I

RANDPS ID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =30

Type

Description

PSD velocity

4

GRID

I

Grid identification number

5

COMP

I

PSD velocity component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

RANDPS

I

RANDPS ID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =31

Type

Description

PSD acceleration

4

GRID

I

Grid identification number

5

COMP

I

PSD acceleration component number

6

SUBCASE

I

Subcase identification number

7

FREQ

RS

Frequency

8

RANDPS

I

RANDPS ID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =60

Type

Description

Transient response displacement

4

GRID

I

Grid identification number

5

COMP

I

Displacement component number

6

SUBCASE

I

Subcase identification number

3-86

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

7

TIME

RS

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =61

Description Time

Superelement identification number Type

Description

Transient response velocity

4

GRID

I

Grid identification number

5

COMP

I

Velocity component number

6

SUBCASE

I

Subcase identification number

7

TIME

RS

Time

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =62

Superelement identification number Type

Description

Transient response acceleration

4

GRID

I

Grid identification number

5

COMP

I

Acceleration component number

6

SUBCASE

I

Subcase identification number

7

TIME

RS

Time

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =63

Superelement identification number Type

Description

Transient response SPC Force

4

GRID

I

Grid identification number

5

COMP

I

SPC force component number

6

SUBCASE

I

Subcase identification number

7

TIME

RS

Time

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Data Block Descriptions A-E

Name

Word

Type

8

UNDEF

None

9

SEID

I

Name

Word RTYPE =64

Description

Superelement identification number Type

Description

Transient response stress

4

EID

I

Element identification number

5

COMP

I

Stress component number

6

SUBCASE

I

Subcase identification number

7

TIME

RS

Time

8

UNDEF

None

9

SEID

I

Name

Word RTYPE =65

Superelement identification number Type

Description

Transient response force

4

EID

I

Element identification number

5

COMP

I

Force component number

6

SUBCASE

I

Subcase identification number

7

TIME

RS

Time

8

UNDEF

None

9

SEID

I

Word

Name

RTYPE =81

Superelement identification number Type

Description

Aeroelastic divergence

4

SUBCASE

I

5

UNDEF

None

6

ROOT

I

Root

7

MACH

RS

Mach number

8

UNDEF

None

3-88

DMAP Programmer’s Guide

Subcase identification number

Data Block Descriptions A-E

Name

Word 9

SEID

Type I

Name

Word RTYPE =82

Description Superelement identification number

Type

Description

Aeroelastic trim

4

SUBCASE

I

5

UNDEF

None

6

XID

I

7

UNDEF(2)

None

9

SEID

I

Name

Word RTYPE =83

Subcase identification number

XID

Superelement identification number Type

Description

Aeroelastic stability derivative

4

SUBCASE

I

Subcase identification number

5

RU

I

R/U

6

COMP

I

Component number

7

UNDEF

None

8

XID

I

XID

9

SEID

I

Superelement identification number

Word

Name

RTYPE =84

Type

Description

Aeroelastic flutter damping

4

SUBCASE

I

Subcase identification number

5

MODE

I

Mode number

6

DENSITY

RS

Density

7

MACH

RS

Mach number

8

VEL

RS

Velocity

9

SEID

I

Superelement identification number

End RTYPE

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3-89

Chapter 3

Data Block Descriptions A-E

Record 2 – TYPE2 – Type 2 Responses Name

Word

Type

Description

1

IRID

I

Internal response identification number

2

RID

I

External response identification number

3

SUBCASE

I

Subcase identification number

4

DFLAG

I

Dynamic response flag (See Note)

5

FREQTIME

RS

Frequency or time step

6

SEID

I

Superelement identification number

Record 3 – TRAILER Word

Name

Type

Description

1

NR1

I

Number of Type 1 responses

2

NR2

I

Number of Type 2 responses

3

UNDEF(4 )

None

Notes: 1. Record 1 contains NR1 * 9 words. 2. Record 2 contains NR2 * 6 words. 3. If the Subcase ID on record 2 is ’SPAN’, the response spans subcases (not currently supported). 4. The DFLG attribute identifies the dynamic response type. 5. 1 – Response is not dynamic. FREQ/TIME is not required. 6. 2 – Response is dynamic. FREQ/TIME is required. 7. ? – Response is dynamic and spans frequency or time steps. FREQ/TIME is not defined. 8. If the Superlement ID attribute on record 2 is ’SPAN’, the response spans superelements (not currently supported).

3.18 DVPTAB Designed property table

3-90

DMAP Programmer’s Guide

Data Block Descriptions A-E

Record – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data Block Name

Record – REPEAT By ascending internal property identification number order. Type one properties are first and type two follow. Word

Name

Type

Description

1

IPID

I

Internal property identification number

2

DVTYP

I

DVPRELi Bulk Data entry identification number

3

EPPNT

I

Property type (1 or 2 or 3) (Type 1 includes both DVPREL1 defined properties and internally generated PBAR/PBEAM properties that are linearly dependent on designed PBARL/PBEAML dimensions. Type 2 is for DVPREL2 defined properties. Type 3 is for internally generated PBAR/PBEAM properties that are nonlinearly dependent on designed PBARL/PBEAML dimensions.)

4

PTYP1

CHAR4

First word of the property type

5

PTYP2

CHAR4

Second word of the property type

6

PID

I

Property identification number

7

FID

I

Property field position

8

PMIN

RS

Minimum property value

9

PMAX

RS

Maximum property value

10

PNAME1

CHAR4

First word of property name

11

PNAME2

CHAR4

Second word of property name

12

FREQ

RS

Frequency, if relevant, for which the property is defined

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Data Block Descriptions A-E

Record – TRAILER Name

Word

Type

Description

1

NPROP

I

Number of designed properties (number of “Repeat” records in table)

2

NENT1

I

Number of Type 1 entries (see definition of EPPNT in “Repeat” record above)

3

NENT2

I

Number of Type 2 entries (see definition of EPPNT in “Repeat” record above)

4

NENT3

I

Number of Type 3 entries (see definition of EPPNT in “Repeat” record above)

5

UNDEF(2)

None

Notes: There are as many records as there are designed properties. (NPROP = NENT1 + NENT2 + NENT3)

3.19 DYNAMIC Table of Bulk Data entry images related to dynamics

Record – HEADER Name

Word 1

Type

Description

CHAR4

NAME(2)

Data Block Name

Record – ACSRCE(5307,53,379) Power vs. frequency for a simple acoustic source Name

Word

Type

Description

1

SID

I

Load set identification number

2

DAREA

I

DAREA Bulk Data entry identification number

3

DPHASE

I

DPHASE Bulk Data entry identification number

4

DELAY

I

DELAY Bulk Data entry identification number

5

TC

I

TABLEDi Bulk Data entry identification number for C(f)

3-92

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

6

RHO

RS

Density of the fluid

7

B

RS

Bulk modulus of the fluid

Record – DAREA(27,17,182) Scale factor for dynamic loads Name

Word

Type

Description

1

SID

I

Load set identification number

2

P

I

Grid, scalar, or extra point identification number

3

C

I

Component number

4

A

RS

Scale factor

Record – DELAY(37,18,183) Time delay parameter for dynamic loads Name

Word

Type

Description

1

SID

I

Set identification number

2

P

I

Grid, scalar, or extra point identification number

3

C

I

Component number

4

T

RS

Time delay

Record – DLOAD(57,5,123) Linear combination of dynamic loads Name

Word

Type

Description

1

SID

I

Load set identification number

2

S

RS

Overall scale factor

3

SI

RS

Scale factor i

4

LI

I

Load set identification number i

Words 3 through 4 repeat until (-1,-1) occurs

DMAP Programmer’s Guide

3-93

Data Block Descriptions A-E

Chapter 3

Record – DPHASE(77,19,184) Phase lead parameter in dynamic loading Name

Word

Type

Description

1

SID

I

Set identification number

2

P

I

Grid, scalar, or extra point identification number

3

C

I

Component number

4

TH

RS

Phase lead

Record – EIGB(107,1,86) Name

Word

Type

Description

1

SID

I

Set identification number

2

METHOD(2)

CHAR4

Method of eigenvalue extraction

4

L1

RS

Lower bound of eigenvalue range of interest

5

L2

RS

Upper bound of eigenvalue range of interest

6

NEP

I

Estimate of number of roots in positive range

7

NDP

I

Desired number of positive roots

8

NDN

I

Desired number of negative roots

9

UNDEF

None

10

NORM(2)

CHAR4

Method for normalizing eigenvectors

12

G

I

Grid or scalar point identification number

13

C

I

Component number

14

UNDEF(5 )

None

Record – EIGC(207,2,87) Name

Word

Type

Description

1

SID

I

Set identification number

2

METHOD(2)

CHAR4

Method of eigenvalue extraction

4

NORM(2)

CHAR4

Method for normalizing eigenvectors

3-94

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

6

G

I

Grid or scalar point identification number

7

C

I

Component number

8

E

RS

Convergence criterion

9

ND1

I

Number of desired eigenvectors

10

CONTFLG

I

Continuation flag

CONTFLG =0

With continuation

11

AAJ

RS

Location of A on real axis

12

WAJ

RS

Location of A on imaginary axis

13

ABJ

RS

Location of B on real axis

14

WBJ

RS

Location of B on imaginary axis

15

LJ

RS

Width of search region

16

NEJ

I

Number of estimated roots

17

NDJ

I

Number of desired eigenvectors

Words 11 through 17 repeat until (-1,-1,-1,-1,-1,-1,-1) occ CONTFLG =–1

Without continuation

End CONTFLG

Record – EIGP(257,4,158) Name

Word

Type

Description

1

SID

I

Set identification number

2

ALPHA

RS

Location of pole on real axis

3

OMEGA

RS

Location of pole on imaginary axis

4

M

I

Multiplicity of complex root at pole

Record – EIGR(307,3,85) Name

Word 1

SID

Type I

Description Set identification number

DMAP Programmer’s Guide

3-95

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

2

METHOD(2)

CHAR4

Method of eigenvalue extraction

4

F1

RS

Lower bound of frequency range of interest

5

F2

RS

Upper bound of frequency range of interest

6

NE

I

Number of estimated roots

7

ND

I

Number of desired roots

8

UNDEF(2 )

None

10

NORM(2)

CHAR4

Method for normalizing eigenvectors

12

G

I

Grid or scalar point identification number

13

C

I

Component number

14

UNDEF(5 )

None

Record – EIGRL(308,8,348) Name

Word

Type

Description

1

SID

I

Set identification number

2

V1

RS

Lower bound of frequency range of interest

3

V2

RS

Upper bound of frequency range of interest

4

ND

I

Number of desired eigenvectors

5

MSGLVL

I

Diagnostic level

6

MAXSET

I

Number of vectors in block or set

7

SHFSCL

RS

Estimate of first flexible mode

8

FLAG1

I

V1 specification flag – set to 1 if V1 is specified

9

FLAG2

I

V2 specification flag – set to 1 if V2 is specified

10

NORM(2)

CHAR4

Method for normalizing eigenvectors

12

ALPH

RS

Constant for quadratic frequency segment distribution

13

NUMS

I

Number of frequency segments

14

FI

RS

Frequency at the upper boundary of the i-th segment

3-96

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

Word 14 repeats NUMS times

Record – EPOINT(707,7,124) Name

Word 1

ID

Type I

Description Extra point identification number

Record – FREQ(1307,13,126) Name

Word

Type

Description

1

SID

I

Set identification number

2

F

RS

Frequency

Word 2 repeats until End of Record

Record – FREQ1(1007,10,125) Word

Name

Type

Description

1

SID

I

Set identification number

2

F1

RS

First frequency

3

DF

RS

Frequency increment

4

NDF

I

Number of frequency increments

Record – FREQ2(1107,11,166) Word

Name

Type

Description

1

SID

I

Set identification number

2

F1

RS

First frequency

3

F2

RS

Last frequency

4

NF

I

Number of logarithmic intervals

DMAP Programmer’s Guide

3-97

Chapter 3

Data Block Descriptions A-E

Record – FREQ3(1407,14,39) Name

Word

Type

Description

1

SID

I

Set identification number

2

F1

RS

Lower bound of modal frequency range

3

F2

RS

Upper bound of modal frequency range

4

TYPE

CHAR4

Type of interpolation: LINE or LOG

5

NEF

I

Number of frequencies

6

BIAS

RS

Clustering bias parameter

Record – FREQ4(1507,15,40) Name

Word

Type

Description

1

SID

I

Set identification number

2

F1

RS

Lower bound of modal frequency range

3

F2

RS

Upper bound of modal frequency range

4

FSPD

RS

Frequency spread

5

NFM

I

Number of evenly spaced frequencies per spread

Record – FREQ5(1607,16,41) Word

Name

Type

Description

1

SID

I

Load set identification number

2

F1

RS

Lower bound of modal frequency range

3

F2

RS

Upper bound of modal frequency range

4

FRI

RS

Fractions of natural frequencies

Word 4 repeats until End of Record

Record – NLRGAP(3707,37,556) Defines a nonlinear transient radial gap. Word 1

3-98

Name SID

DMAP Programmer’s Guide

Type I

Description Load set identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

GA

I

Inner grid identification number

3

GB

I

Outer grid identification number

4

PLANE

I

Radial gap orientation plane (xy = 100; yz = 200, zx = 300)

5

TABK

I

Table identification number for gap stiffness vs. time

6

TABG

I

Table identification number for radial gap clearance

7

TABU

I

Table identification number for radial coefficient

8

RADIUS

RS

Shaft radius

Record – NOLIN1(3107,31,127) Name

Word

Type

Description

1

SID

I

Load set identification number

2

GI

I

Grid, scalar, or extra point identification number of I

3

CI

I

Component number for GI.

4

S

RS

Scale factor

5

GJ

I

Grid, scalar, or extra point identification number of J

6

CJ

I

Component number for GJ

7

T

I

Identification number of a TABLEDi Bulk Data entry.

8

UNDEF

None

Record – NOLIN2(3207,32,128) Word

Name

Type

Description

1

SID

I

Load set identification number

2

GI

I

Grid, scalar, or extra point identification number of I

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3-99

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

3

CI

I

Component number for GI.

4

S

RS

Scale factor

5

GJ

I

Grid, scalar, or extra point identification number of J

6

CJ

I

Component number for GJ

7

GK

I

Grid, scalar, or extra point identification number of K

8

CK

I

Component number for GK

Record – NOLIN3(3307,33,129) Name

Word

Type

Description

1

SID

I

Load set identification number

2

GI

I

Grid, scalar, or extra point identification number of I

3

CI

I

Component number for GI.

4

S

RS

Scale factor

5

GJ

I

Grid, scalar, or extra point identification number of J

6

CJ

I

Component number for GJ

7

A

RS

Exponent of the forcing function

8

UNDEF

None

Record – NOLIN4(3407,34,130) Name

Word

Type

Description

1

SID

I

Load set identification number

2

GI

I

Grid, scalar, or extra point identification number of I

3

CI

I

Component number for GI.

4

S

RS

Scale factor

3-100

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

5

GJ

I

Grid, scalar, or extra point identification number of J

6

CJ

I

Component number for GJ

7

A

RS

Exponent of the forcing function

8

UNDEF

None

Record – RANDPS(2107,21,195) Name

Word

Type

Description

1

SID

I

Set identification number

2

J

I

Subcase identification number of the excited set

3

K

I

Subcase identification number of the applied load set

4

X

RS

X component

5

Y

RS

Y component

6

TID

I

Identification number of a TABRNDi entry that defines G(F)

Record – RANDT1(2207,22,196) Name

Word

Type

Description

1

SID

I

Set identification number

2

N

I

Number of time lag intervals

3

TO

RS

Starting time lag

4

TMAX

RS

Maximum time lag

Record – RLOAD1(5107,51,131) Name

Word

Type

Description

1

SID

I

Load set identification number

2

DAREA

I

DAREA Bulk Data entry identification number

3

DPHASE

RS

DPHASE Bulk Data entry identification number

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3-101

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

4

DELAY

RS

DELAY Bulk Data entry identification number

5

TC

I

TABLEDi Bulk Data entry identification number for C(f)

6

TD

I

TABLEDi Bulk Data entry identification number for D(f)

7

TYPE

I

Nature of the dynamic excitation

Record – RLOAD2(5207,52,132) Name

Word

Type

Description

1

SID

I

Load set identification number

2

DAREA

I

DAREA Bulk Data entry identification number

3

DPHASE

I

DPHASE Bulk Data entry identification number

4

DELAY

I

DELAY Bulk Data entry identification number

5

TB

I

TABLEDi Bulk Data entry identification number for B(f)

6

TP

I

TABLEDi Bulk Data entry identification number for Phi(f)

7

TYPE

I

Nature of the dynamic excitation

Record – ROTORB (8910,89,606) Word

Name

Type

Description

1

SID

I

Set identification number of rotor

2

ID

I

Grid or scalar point ID’s which define bearing locations on a rotor

Record – ROTORD(8210,82,599) Word

Name

Type

Description

1

SID

I

Set identification number

2

NUMROT

I

Number of rotors (i=1, NUMROT below)

3

RSTART

RS

Starting rotor speed (in RPM)

3-102

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

4

RSTEP

RS

Rotor speed step size (in RPM)

5

NUMSTEP

I

Number of steps for rotor speed

6,7

REFSYS

CHAR8

Rotational reference system (YHROT,YH or YHFIX,YH

8

CMOUT

RS

Complex mode output request

9,10

RUNIT

CHAR8

Revolution input/output units for rotor (YHRPM or YHRAD or YHCPS or YHHZ)

11,12

FUNIT

CHAR8

Frequency output units (YHRPM or YHRAD or YHCPS or YHHZ)

13,14

ZSTEIN

CHAR8

Flag to incorpoate Steiner inertia terms (YHYES,YH or YHNO,YH)

15

ORBEPS

RS

Threshold value for detection of whirl direction

16

ROTPRT

I

Optimal flag

17

SYNC

I

Optional printout flag

18

ETYPE

I

Optional printout flag

19

EORDER

RS

Optional printout flag

20–21

(not used)

22+8*(i-1)

RIDi

I

Rotor ID for ith rotor

23+8*(i-1)

RSETi

I

Set number for rotor speed for multiple rotors

24+8*(i-1)

RSPEEDi

RS

Relative rotor speed for multiple rotors

25+8*(i-1)

RCOORDI

I

Coordinate system ID number specifying rotation axis as Z

26+8*(i-1)

W3i

RS

Damping coefficient like PARAM,W3

27+8*(i-1)

W4i

RS

Damping coefficient like PARAM,W4

28+8*(i-1)

RFORCEi

I

RFORCE bulk data ID number specifying rotational force to be applied

29+8*(i-1)

(not used)

DMAP Programmer’s Guide

3-103

Chapter 3

Data Block Descriptions A-E

Record – ROTORG(8410,84,600) Name

Word

Type

Description

1

SID

I

Set identification number of rotor

2

ID

I

Grid or scalar point ID’s which define a rotor

Record – SEQEP(5707,57,135) Name

Word

Type

Description

1

ID

I

Extra point identification number

2

SEQID

I

Sequenced identification number

Record – TF(6207,62,136) Name

Word

Type

Description

1

SID

I

Set identification number

2

GD

I

Grid, scalar, or extra point identification number

3

CD

I

Component number for point GD

4

B0

RS

Transfer function coefficient

5

B1

RS

Transfer function coefficient

6

B2

RS

Transfer function coefficient

7

GI

I

Grid, scalar, or extra point identification number

8

CI

I

Component number for point GI

9

A0I

RS

Transfer function coefficient

10

A1I

RS

Transfer function coefficient

11

A2I

RS

Transfer function coefficient

Words 7 through 11 repeat until (-1,-1,–1,-1,-1) occurs

Record – TIC(6607,66,137) Word

Name

1

SID

3-104

DMAP Programmer’s Guide

Type I

Description Load set identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

G

I

Grid, scalar, or extra point identification number

3

C

I

Component number for point GD

4

U0

RS

Initial displacement

5

V0

RS

Initial velocity

Record – TLOAD1(7107,71,138) Name

Word

Type

Description

1

SID

I

Load set identification number

2

DAREA

I

DAREA Bulk Data entry identification number

3

DELAY

I

DELAY Bulk Data entry identification number

4

TYPE

I

Nature of the dynamic excitation

5

TID

I

Identification number of TABLEDi entry that gives F(t)

Record – TLOAD2(7207,72,139) Name

Word

Type

Description

1

SID

I

Load set identification number

2

DAREA

I

DAREA Bulk Data entry identification number

3

DELAY

I

DELAY Bulk Data entry identification number

4

TYPE

I

Nature of the dynamic excitation

5

T1

RS

Time constant 1

6

T2

RS

Time constant 2

7

F

RS

Frequency

8

P

RS

Phase angle

9

C

RS

Exponential coefficient

10

B

RS

Growth coefficient

DMAP Programmer’s Guide

3-105

Data Block Descriptions A-E

Chapter 3

Record – TSTEP(8307,83,142) Name

Word

Type

Description

1

SID

I

Set identification number

2

N

I

Number of time steps of value DTi

3

DT

RS

Time increment

4

NO

I

Skip factor for output

Words 2 through 4 repeat until (-1,-1,-1) occurs

TRAILER Name

Word 1

BIT(6)

Type I

Description Record presence trailer words

3.20 EDOM SOL 200 design optimization and sensitivity analysis bulk entries.

Record – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record – DCONADD(5106,51,471) Design constraint set combinations. Name

Word

Type

Description

1

DCID

I

Design constraint set identification number

2

DCi

I

DCONSTR entry identification number

Word 2 repeats until -1 occurs

Record – DCONSTR(4106,41,362) Design constraints.

3-106

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

DCID

I

Design constraint set identification number

2

RID

I

DRESPi entry identification number

3

LALLOW

RS

Lower bound on the response quantity. Undefined if LTID is nonzero

4

UALLOW

RS

Upper bound on the response quantity. Undefined if UTID is nonzero

5

LOWFQ

RS

Low end of frequency range in Hz

6

HIGHFQ

RS

High end of frequency range in Hz

7

LTID

I

Identification number of TABLEDi entry giving lower bound on the response quantity as a function of frequency or 0 if not specified

8

UTID

I

Identification number of TABLEDi entry giving upper bound on the response quantity as a function of frequency or 0 if not specified

Record – DDVAL(7000,70,563) Discrete design variable values. Name

Word

Type

Description

1

ID

I

Unique discrete value set identification number

2

DVALi

RS

Discrete values for the variable

Word 2 repeats until -1 occurs

Record – DESVAR(3106,31,352) Design variables. Name

Word

Type

Description

1

ID

I

Unique design variable identification number

2

LABEL(2)

CHAR4

User-supplied name for printing purposes

4

XINIT

RS

Initial value

5

XLB

RS

Lower bound

6

XUB

RS

Upper bound

DMAP Programmer’s Guide

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

7

DELXV

RS

Fractional change allowed for the design variable during approximate optimization

8

DDVAL

I

ID of a DDVAL entry that provides a set of allowable discrete values

Record – DLINK(3206,32,353) Multiple design variable linking. Name

Word

Type

Description

1

ID

I

Unique identification number

2

DDVID

I

Dependent design variable identification number

3

C0

RS

Constant term

4

CMULT

RS

Constant multiplier

5

IDVi

I

Independent design variable identification number

6

Ci

RS

Coefficient corresponding to IDV

Words 5 and 6 repeat until -1 occurs

Record – DOPTPRM(4306,43,364) Design optimization parameters. Word

Name

Type

Description

1

APRCOD

I

Approximation method

2

IPRINT

I

Print control during approximate optimization phase with DOT

3

DESMAX

I

Maximum number of design cycles

4

METHOD

I

DOT optimization method

5

DELP

RS

Fractional change allowed in each property during any optimization design cycle

6

DPMIN

RS

Minimum move limit imposed

3-108

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

7

PTOL

RS

Maximum tolerance on differences allowed between the property values on property entries and the property values calculated from the design variable values on the DESVAR entry

8

CONV1

RS

Relative objective function convergence criterion

9

CONV2

RS

Absolute objective function convergence criterion

10

GMAX

RS

Maximum constraint violation allowed at the converged optimum

11

DELX

RS

Fractional change allowed in each design variable during any optimization cycle

12

DXMIN

RS

Minimum absolute limit on design variable move

13

DELB

RS

Relative finite difference move parameter

14

GSCAL

RS

Constraint normalization factor

15

CONVDV

RS

Relative convergence criterion on design variables

16

CONVPR

RS

Relative convergence criterion on properties

17

P1

I

Design cycles in which output is printed

18

P2

I

Items to be printed at the design cycles defined by P1

19

CT

RS

Constraint tolerance

20

CTMIN

RS

Constraint violation threshold

21

DABOBJ

RS

DOT absolute objective function convergence criterion

22

DELOBJ

RS

DOT relative objective function convergence criterion

23

DOBJ1

RS

DOT 1–D search absolute objective limit

24

DOBJ2

RS

DOT 1–D search relative objective limit

25

DX1

RS

DOT 1–D search absolute DV limit

26

DX2

RS

DOT 1–D search relative DV limit

27

ISCAL

I

Design variables are rescaled every ISCAL iterations

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3-109

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

28

ITMAX

I

Maximum DOT MFD iterations per cycle

29

ITRMOP

I

Maximum consecutive DOT MFD iterations at convergence

30

IWRITE

I

File number for DOT optimizer printout

31

IGMAX

I

Active constraint counter

32

JTMAX

I

Maximum DOT SLP iterations per cycle

33

ITRMST

I

Maximum consecutive DOT SLP iterations at convergence

34

JPRINT

I

SLP subproblem print within DOT

35

IPRNT1

I

Print scaling factors for design variable vector within DOT

36

IPRNT2

I

DOT 1–D search or miscellaneous information print

37

JWRITE

I

File number on which iteration history is written within DOT

38

STPSCL

RS

Scale factor for shape finite difference step sizes applied to all shape design variables

39

FSDMAX

I

Number of FSD cycles to be performed

40

FSDALP

RS

Relaxation parameter applied in FSD

41

DISCOD

I

Discrete processing method code

42

DISBEG

I

Design cycle ID for discrete variable processing initiation

43

PLVIOL

I

Flag for handling property limit violation

44

P2RSET

I

ID of a SET1 entry listing constrained responses to be printed if retained

Record – DRESP1(3806,38,359) First level design response quantities. (If applicable, see the Quick Reference Guide for detailed information on response attributes.) Name

Word 1

3-110

ID

DMAP Programmer’s Guide

Type I

Description Unique entry identifier

Data Block Descriptions A-E

Word

Name

Type

Description

2

LABEL(2)

CHAR4

User-defined label

4

FLAG

I

Flag indicating response type

FLAG = 1

WEIGHT

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

MONE

I

Entry is -1

FLAG = 2

VOLUME

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

MONE

I

Entry is -1

FLAG = 3

LAMA

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

MONE

I

Entry is -1

FLAG = 4

EIGN

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

MONE

I

Entry is -1

DMAP Programmer’s Guide

3-111

Chapter 3

Word

Data Block Descriptions A-E

Name

FLAG = 5

Type

Description

DISP

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 6

STRESS

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 7

STRAIN

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 8

FORCE

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

3-112

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 9

CFAILURE

5

PTYPE(2)

CHAR4

Element flag (ELEM) or composite property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or composite property IDs

Word 10 repeats until -1 occurs FLAG = 10

CSTRESS

5

PTYPE(2)

CHAR4

Element flag (ELEM) or composite property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or composite property IDs

Word 10 repeats until -1 occurs FLAG = 11

CSTRAIN

5

PTYPE(2)

CHAR4

Element flag (ELEM) or composite property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or composite property IDs

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Chapter 3

Word

Data Block Descriptions A-E

Name

Type

Description

Word 10 repeats until -1 occurs FLAG = 12

FREQ

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

MONE

I

Entry is -1

FLAG = 13

SPCFORCE

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 14

ESE

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 15

CEIG

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

3-114

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word 10

Name MONE

FLAG = 20

Type I

Description Entry is -1

FRDISP

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 21

FRVELO

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 22

FRACCL

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

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Chapter 3

Word 10

Data Block Descriptions A-E

Name ATTi

Type I

Description Grid point IDs

Word 10 repeats until -1 occurs FLAG = 23

FRSPCF

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 24

FRSTRE

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 25

FRFORC

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

3-116

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 26

RMSDISP

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Random ID

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 27

RMSVELO

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Random ID

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 28

RMSACCL

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Random ID

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs

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Chapter 3

Word

Data Block Descriptions A-E

Name

FLAG = 29

Type

Description

PSDDISP

5

UNDEF

None

6

PTYPE

I

Random ID

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 30

PSDVELO

5

UNDEF

None

6

PTYPE

I

Random ID

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 31

PSDACCL

5

UNDEF

None

6

PTYPE

I

Random ID

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

3-118

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

9

ATTB

RS

Frequency value; -1 (integer) spawn for all frequencies in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 60

TDISP

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Time value; -1 (integer) spawn for all time steps in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 61

TVELO

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Time value; -1 (integer) spawn for all time steps in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 62

TACCL

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

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Chapter 3

Word

Data Block Descriptions A-E

Name

Type

Description

8

ATTA

I

Response attribute

9

ATTB

RS

Time value; -1 (integer) spawn for all time steps in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 63

TSPCF

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Time value; -1 (integer) spawn for all time steps in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Grid point IDs

Word 10 repeats until -1 occurs FLAG = 64

TSTRE

5

PTYPE(2)

CHAR4

Element flag (ELEM) or property entry name

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Time value; -1 (integer) spawn for all time steps in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 65 5

3-120

TFORC PTYPE(2)

DMAP Programmer’s Guide

CHAR4

Element flag (ELEM) or property entry name

Data Block Descriptions A-E

Word

Name

Type

Description

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

RS

Time value; -1 (integer) spawn for all time steps in set; -1.10000E+08 for SUM; -1.20000E+08 for AVG; -1.30000E+08 for SSQ; -1.40000E+08 for RSS; -1.50000E+08 for MAX; -1.60000E+08 for MIN

10

ATTi

I

Element numbers (if Word 5 is ELEM) or property IDs

Word 10 repeats until -1 occurs FLAG = 81

DIVERG

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATT1

RS

Mach number

11

MONE

I

Entry is -1

TRIM

FLAG = 82 5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Entry is 0

10

ATT1

I

Entry is 0

11

MONE

I

Entry is -1

FLAG = 83

STABDER

5

UNDEF(2)

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

DMAP Programmer’s Guide

3-121

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

10

ATT1

I

Component

11

MONE

I

Entry is -1

FLUTTER

FLAG = 84 5

METHOD

CHAR4

6

UNDEF

None

7

REGION

I

Region identifier for constraint screening

8

ATTA

I

Response attribute

9

ATTB

I

Response attribute

10

ATTi

I

ATT1 is the identification number of a SET1 entry that specifies a set of modes; ATT2 is the identification number of an FLFACT entry that specifies a list of densities; ATT3 is the identification number of an FLFACT entry that specifies a list of Mach numbers; ATT4 is the identification number of an FLFACT entry that specifies a list of velocities

Analysis type: PK or PKNL

Word 10 repeats until -1 occurs

Record – DRESP2(3906,39,360) Design equation response quantities. Name

Word

Type

Description

1

ID

I

Unique entry identifier

2

LABEL(2)

CHAR4

User-defined label

4

EQID

I

DEQATN entry identification number if integer > 0. Function to be applied to arguments (FUNC) if integer < 0: -2 for AVG; -3 for SSQ; -4 for RSS; -5 for MAX; -6 for MIN

5

REGION

I

Region identifier for constraint screening

6

FLAG

I

FLAG = 1000

DESVAR

7

I

DVIDi

Word 7 repeats until -1000

3-122

DMAP Programmer’s Guide

DESVAR entry identification number

Data Block Descriptions A-E

Name

Word

Type

FLAG = 2000

DTABLE

7

CHAR4

LABLi(2)

Description

Label for a constant in the DTABLE entry

Word 7 repeats until -2000 FLAG = 3000

DFRFNC

7

I

DFRFIDi

Identification number for a DFRFNC record in the DTI, DFRFNC table

Word 7 repeats until -3000 FLAG = 4000

DRESP1

7

I

NRi

DRESP1 entry identification number

Word 7 repeats until -4000 FLAG = 5000

DNODE

7

Gi

I

Grid point identification number

8

Ci

I

Component number of grid point

Words 7 and 8 repeat until -5000 FLAG = 6000

DVPREL1

7

I

DPIPi

DVPREL1 entry identification number

Word 7 repeats until -6000 FLAG = 7000

DVCREL1

7

I

DCICi

DVCREL1 entry identification number

Word 7 repeats until -7000 FLAG = 8000

DVMREL1

7

I

DMIMi

DVMREL1 entry identification number

Word 7 repeats until -8000 occurs FLAG = 9000

DVPREL2

7

I

DPI2Pi

DVPREL2 entry identification number

Word 7 repeats until -9000 occurs FLAG = 10000

DVCREL2

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Data Block Descriptions A-E

Chapter 3

Name

Word 7

DCI2Ci

Type I

Description DVCREL2 entry identification number

Word 7 repeats until -10000 occurs FLAG = 11000

DVMREL2

7

I

DMI2Mi

DVMREL2 entry identification number

Word 7 repeats until -11000 occurs FLAG = 12000

DRESP2

7

I

NRRi

Nested DRESP2 entry identification number

Word 7 repeats until -12000 occurs End entry when -1 occurs

Record – DRESP3(6700,67,433) Externally computed design responses. Name

Word

Type

Description

1

ID

I

Unique entry identifier

2

LABEL(2)

CHAR4

User-defined label referenced by a constraint bulk entry or by the objective function

4

GROUP(2)

CHAR4

Selects a specific external response routine

6

TYPE(2)

CHAR4

Refers to a specific user-created response calculation type in the external function evaluator

8

REGION

I

Region identifier for constraint screening

9

FLAG

I

FLAG = 1000

DESVAR

10

I

DVIDi

DESVAR entry identification number

Word 10 repeats until -1000 FLAG = 2000

DTABLE

10

CHAR4

LABLi(2)

Word 10 repeats until -2000

3-124

DMAP Programmer’s Guide

Label for a constant in the DTABLE entry

Data Block Descriptions A-E

Name

Word

Type

FLAG = 3000

DFRFNC

10

I

DFRFIDi

Description

Identification number for a DFRFNC record in the DTI, DFRFNC table

Word 10 repeats until -3000 FLAG = 4000

DRESP1

10

I

NRi

DRESP1 entry identification number

Word 10 repeats until -4000 FLAG = 5000

DNODE

10

Gi

I

Grid point identification number

11

Ci

I

Component number of grid point

Words 10 and 11 repeat until -5000 FLAG = 6000

DVPREL1

10

I

DPIPi

DVPREL1 entry identification number

Word 10 repeats until -6000 FLAG = 7000

DVCREL1

10

I

DCICi

DVCREL1 entry identification number

Word 10 repeats until -7000 FLAG = 8000

DVMREL1

10

I

DMIMi

DVMREL1 entry identification number

Word 10 repeats until -8000 occurs FLAG = 9000

DVPREL2

10

I

DPI2Pi

DVPREL2 entry identification number

Word 10 repeats until -9000 occurs FLAG = 10000

DVCREL2

10

I

DCI2Ci

DVCREL2 entry identification number

Word 10 repeats until -10000 occurs FLAG = 11000

DVMREL2

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Data Block Descriptions A-E

Chapter 3

Name

Word 10

DMI2Mi

Type I

Description DVMREL2 entry identification number

Word 10 repeats until -11000 occurs FLAG = 12000

DRESP2

10

I

NRRi

Nested DRESP2 entry identification number

Word 10 repeats until -12000 occurs FLAG = 13000

USRDATA

10

CHAR4

USRDATA(2)

Character strings in user-defined format for any use in the evaluator

Words 10 and 11 repeat until -13000 occurs End entry when -1 occurs

Record – DSCREEN(4206,42,363) Design constraint screening data. Name

Word

Type

Description

1

RTYPE

I

Response type for which the screening criteria apply

2

TRS

RS

Truncation threshold

3

NSTR

I

Maximum number of constraints to be retained per region per load case

Record – DTABLE(3706,37,358) Table constants. Word

Name

Type

Description

1

LABLi(2)

CHAR4

Label for the constant

3

VALUi

RS

Value of the constant

Words 1 thru 3 repeat until -1 occurs

Record – DVBSHAP(5806,58,474) Design variable to boundary shapes.

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DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

DVID

I

Design variable identification number of a DESVAR entry

2

AUXMID

I

Auxiliary model identification number

3

COLi

I

Load sequence identification number from AUXMODEL command

4

SFi

RS

Scaling factor for load sequence identification number

Words 1 thru 4 repeat for i = 2 and 3

Record – DVCREL1(6100,61,429) Design variable to connectivity property relation. Name

Word

Type

Description

1

ID

I

Unique identification number

2

TYPE(2)

CHAR4

Name of an element connectivity entry

4

EID

I

Element identification number

5

FID

I

Entry is 0

6

CPMIN

RS

Minimum value allowed for this property

7

CPMAX

RS

Maximum value allowed for this property

8

C0

RS

Constant term of relation

9

CPNAME(2)

CHAR4

Name of connectivity property

11

DVIDi

I

DESVAR entry identification number

12

COEFi

RS

Coefficient of linear relation

Words 11 and 12 repeat until -1 occurs

Record – DVCREL2(6200,62,430) Design variable to connectivity property relation based on a user-supplied equation. Name

Word

Type

Description

1

ID

I

Unique identification number

2

TYPE(2)

CHAR4

Name of an element connectivity entry

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Name

Word

Type

Description

4

EID

I

Element identification number

5

FID

I

Entry is 0

6

CPMIN

RS

Minimum value allowed for this property

7

CPMAX

RS

Maximum value allowed for this property

8

EQID

I

DEQATN entry identification number

9

CPNAME(2)

CHAR4

Name of connectivity property

11

FLAG

I

DESVAR/DTABLE

FLAG = 1000 12

DESVAR DVIDi

I

A DESVAR entry identification number

Word 12 repeats until -1000 FLAG = 2000 12

DTABLE LABLi(2)

CHAR4

Label for a constant on the DTABLE entry

Words 12 and 13 repeat until -2000 End flag when -1 occurs

Record – DVGEOM(5906,59,356) Design variable to geometry relation. Name

Word

Type

Description

1

DVID

I

DESVAR entry identification number

2

ENTITY(2)

CHAR4

Designed entity

4

ID

I

Identification number of the parent entity specified by ENTITY

5

IDPRTB

I

Identification number of the perturbed entity specified by ENTITY

Record – DVGRID(4406,44,372) Design variable to grid point relation.

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Name

Word

Type

Description

1

DVID

I

DESVAR entry identification number

2

GID

I

Grid point or geometric point identification number

3

CID

I

Coordinate system identification number

4

COEFF

RS

Multiplier of the vector defined by N(3)

5

N1

RS

Component of the vector measured in the coordinate system defined by CID

6

N2

RS

Component of the vector measured in the coordinate system defined by CID

7

N3

RS

Component of the vector measured in the coordinate system defined by CID

Record – DVMREL1(6300,63,431) Design variable to material relation. Name

Word

Type

Description

1

ID

I

Unique identification number

2

TYPE(2)

CHAR4

Name of a material property entry

4

MID

I

Material identification number

5

FID

I

Entry is 0

6

MPMIN

RS

Minimum value allowed for this property

7

MPMAX

RS

Maximum value allowed for this property

8

C0

RS

Constant term of relation

9

MPNAME(2)

CHAR4

Name of material property

11

DVIDi

I

DESVAR entry identification number

12

COEFi

RS

Coefficient of linear relation

Words 11 and 12 repeat until -1 occurs

Record – DVMREL2(6400,64,432) Design variable to material relation based on a user-supplied equation.

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Name

Word

Type

Description

1

ID

I

Unique identification number

2

TYPE(2)

CHAR4

Name of a material property entry

4

MID

I

Material identification number

5

FID

I

Entry is 0

6

MPMIN

RS

Minimum value allowed for this property

7

MPMAX

RS

Maximum value allowed for this property

8

EQID

I

DEQATN entry identification number

9

MPNAME(2)

CHAR4

Name of material property

11

FLAG

I

DESVAR/DTABLE

FLAG = 1000 12

DESVAR DVIDi

I

A DESVAR entry identification number

Word 12 repeats until -1000 FLAG = 2000 12

DTABLE LABLi(2)

CHAR4

Label for a constant on the DTABLE entry

Words 12 and 13 repeat until -2000 End flag when -1 occurs

Record – DVPREL1(3306,33,354) Design variable to property relation. Name

Word

Type

Description

1

ID

I

Unique identification number

2

TYPE(2)

CHAR4

Name of a property entry

4

PID

I

Property entry identification number

5

FID

I

FID number input. Otherwise, either 0 if property name is input, or frequency (RS) if entry is for frequency dependent property. (See Words 9 and 10)

6

PMIN

RS

Minimum value allowed for this property

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Name

Word

Type

Description

7

PMAX

RS

Maximum value allowed for this property

8

C0

RS

Constant term of relation

9

PNAME1

CHAR4

First word of property name, if any, or blanks if FID number is nonzero in Word 5

10

PNAME2

CHAR4

Second word of property name, if any. Otherwise, either blanks if FID number is nonzero in Word 5, or frequency (RS) if entry is for frequency dependent property. (See Word 5)

11

DVIDi

I

DESVAR entry identification number

12

COEFi

RS

Coefficient of linear relation

Words 11 and 12 repeat until -1 occurs

Record – DVPREL2(3406,34,355) Design variable to property relation based on a user-supplied equation. Name

Word

Type

Description

1

ID

I

Unique identification number

2

TYPE(2)

CHAR4

Name of a property entry

4

PID

I

Property entry identification number

5

FID

I

FID number input. Otherwise, either 0 if property name is input, or frequency (RS) if entry is for frequency dependent property. (See Words 9 and 10)

6

PMIN

RS

Minimum value allowed for this property

7

PMAX

RS

Maximum value allowed for this property

8

EQID

I

DEQATN entry identification number

9

PNAME1

CHAR4

First word of property name, if any, or blanks if FID number is nonzero in Word 5

10

PNAME2

CHAR4

Second word of property name, if any. Otherwise, either blanks if FID number is nonzero in Word 5, or frequency (RS) if entry is for frequency dependent property. (See Word 5)

11

FLAG

I

DESVAR/DTABLE

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Name

Word

Type

FLAG = 1000 12

Description

DESVAR DVIDi

I

A DESVAR entry identification number

Word 12 repeats until -1000 FLAG = 2000 12

DTABLE CHAR4

LABLi(2)

Label for a constant on the DTABLE entry

Words 12 and 13 repeat until -2000 End flag when -1 occurs

Record – DVSHAP(5006,50,470) Design variable to basis vectors. Word

Name

Type

Description

1

DVID

I

Design variable identification number on the DESVAR entry

2

COLi

I

Column number of the displacement matrix

3

SFi

RS

Scaling factor applied to the COL column of the displacement matrix

Words 1 thru 3 repeat until (-1,-1,-1) occurs

Record – MAT1DOM(103,1,9944) If one or more properties from a MAT1 entry are used as design variables, the MAT1DOM record is written to the EDOM data block. This is different than the MAT1 record in the MPT data block. Word

Name

Type

Description

1

MID

I

MAT1 identification number

2

FTE

I

Format code for Young’s modulus

3

FTG

I

Format code for shear modulus

4

FTNU

I

Format code for Poisson’s ratio

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Record – MAT10DOM(2801,28,9945) If one or more properties from a MAT10 entry are used as design variables, the MAT10DOM record is written to the EDOM data block. This is different than the MAT10 record in the MPT data block. Name

Word

Type

Description

1

MID

I

MAT10 identification number

2

FTBULK

I

Format code for bulk modulus

3

FTRHO

I

Format code for mass density

4

FTC

I

Format code for speed of sound

Record – MODTRAK(6006,60,477) Mode tracking parameters. Word

Name

Type

Description

1

SID

I

Set identification number that is selected with a MODTRAK command

2

LOWRNG

I

Lowest mode number in range to search

3

HIGHRNG

I

Highest mode number in range to search

4

MTFILTER

RS

Filtering parameter used in mode cross-orthogonality check

Record – EODB(65535,65535,65535) End of data block.

Record – TRAILER Word 1

Name BIT(6)

Type I

Description Record presence trailer words

3.21 EDT Aero and element deformations.

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Record – HEADER Name

Word 1

Type

Description

CHAR4

NAME(2)

Data block name

Record – ACMODL(5201,52,373) Fluid-structure interface modeling parameters. Name

Word

Type

Description

1

INTER(2)

CHAR4

IDENT or DIFF method specification

3

INFO(2)

CHAR4

Allowable values are ALL, ELEMENTS, PID, SET3, and NONE

5

FSET

I

Fluid set ID

6

SSET

I

Structure set ID

7

NORML

RS

Outward normal search distance to detect fluid-structure interface

8

METHOD(2)

CHAR4

Interface calculation method

10

OVPLANG

RS

Angular tolerance in degrees used to decide whether a fluid free face and a structural face are overlapping

11

SRCHUNIT(2)

CHAR4

Search unit

13

INTOL

RS

Inward normal search distance to detect fluid-structure interface

14

AREAOPT

I

Area option

15

SKNEPS

RS

SKNEPS option. Only used when AREAOPT = 0

16

INTORD

I

Integration order

Record – ADAPT(6301,63,397) Version adaptivity control. Name

Word

Type

Description

1

SID

I

Adapt entry identification number selected by ADAPT case control command

2

ADGEN

I

Identification number of the first PVAL entry generated in the adaptive process

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Word

Name

Type

Description

3

MAXITER

I

Number of analyses performed before adaptive process is stopped

4

PSTRTID

I

Identification number of the PVAL entry describing the starting p-order distribution

5

PMINID

I

Identification number of the PVAL entry describing the minimum p-order distribution

6

PMAXID

I

Identification number of the PVAL entry describing the maximum p-order distribution

7

PART(2)

CHAR4

Part name of the elements defined in ELSET and controlled by TYPE, ERREST, ERRTOL, SIGTOL, and EPSTOL

9

ELSET

I

Identification number of the SET command under the SETS DEFINITION command

10

TYPE

CHAR4

p-order adjustment

11

ERREST

I

Error estimator activation flag

12

ERRTOL

RS

Error tolerance

13

SIGTOL

RS

Stress tolerance

14

EPSTOL

RS

Strain tolerance

15

UNDEF(4)

None

Words 7 thru 18 repeat until -1 occurs

Record – AECOMP(7801,78,582) Component for an integrated load monitor point. Word

Name

Type

Description

1

NAME(2)

CHAR4

Character string identifying the component

3

LISTTYPE(2)

CHAR4

CAERO or AELIST for aerodynamic components and SET1 for structural components

5

LISTID

I

CAERO, AELIST, or SET1 entry identification number

Word 5 repeats until -1 occurs

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Record – AECOMPL(7901,79,583) Component for an integrated load monitor point. Name

Word

Type

Description

1

NAME(2)

CHAR4

Character string identifying the component

3

LABEL(2)

CHAR4

Character string identifying other components defined by AECOMP or AECOMPL entries

Words 3 and 4 repeat until (-1,-1) occurs

Record – AEDW(7301,73,574) Parametric normal wash loading for aerodynamics. Name

Word

Type

Description

1

MACH

RS

Mach number

2

SYMXZ(2)

CHAR4

Character string for identifying symmetry of the force vector. Allowable values are SYMM, ASYMM, and ANTI

4

SYMXY(2)

CHAR4

Character string for identifying symmetry of the force vector. Allowable values are SYMM, ASYMM, and ANTI

6

UXID

I

The identification number of a UXVEC entry

7

DMIJ(2)

CHAR4

The name of a DMI or DMIJ entry that defines the downwash

9

DMIJI(2)

CHAR4

The name of a DMIJI entry that defines the CAERO2 interference element downwashes

Record – AEFACT(4002,40,273) Aerodynamic lists. Name

Word

Type

Description

1

SID

I

Set identification number

2

D

RS

Number

Word 2 repeats until -1 occurs

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Record – AEFORCE(7501,75,576) Parametric force for aerodynamics. Name

Word

Type

Description

1

MACH

RS

Mach number

2

SYMXZ(2)

CHAR4

Character string for identifying symmetry of the force vector. Allowable values are SYMM, ASYMM, and ANTI

4

SYMXY(2)

CHAR4

Character string for identifying symmetry of the force vector. Allowable values are SYMM, ASYMM, and ANTI

6

UXID

I

The identification number of a UXVEC entry

7

MESH(2)

CHAR4

Character string identifying whether the force is defined on the aerodynamic mesh or structural mesh. Allowable values are AERO and STRUCT

9

FORCE

I

The identification number of a FORCE/MOMENT set

10

DMIK(2)

CHAR4

The name of a DMIK entry that defines the aerodynamic force vector

Record – AELINK(2602,26,386) Links aeroelastic variables. Name

Word

Type

Description

1

ID

I

Trim set identification number

2

LABLD(2)

CHAR4

Character string identifying the dependent aerodynamic variable

4

LABL(2)

CHAR4

Character string identifying the aerodynamic variable

6

C

RS

Linking coefficient for the aerodynamic variable

Words 4 thru 6 repeat until (-1,-1,-1) occurs

Record – AELIST(2302,23,341) Aerodynamic element list.

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Name

Word

Type

Description

1

SID

I

Set identification number

2

E

I

List of aerodynamic boxes generated by CAERO1 entries to define a surface

Word 2 repeats until -1 occurs

Record – AEPARM(7001,70,571) General controller for use in trim. Name

Word

Type

Description

1

ID

I

Controller identification number

2

LABEL(2)

CHAR4

Controller name

4

UNIT(2)

CHAR4

Label used to describe the units of the controller values

Record – AEPRESS(7401,74,575) Parametric pressure loading for aerodynamics. Word

Name

Type

Description

1

MACH

RS

Mach number

2

SYMXZ(2)

CHAR4

Character string for identifying symmetry of the force vector. Allowable values are SYMM, ASYMM, and ANTI

4

SYMXY(2)

CHAR4

Character string for identifying symmetry of the force vector. Allowable values are SYMM, ASYMM, and ANTI

6

UXID

I

The identification number of a UXVEC entry

7

DMIJ(2)

CHAR4

The name of a DMI or DMIJ entry that defines the pressure per unit dynamic pressure

9

DMIJI(2)

CHAR4

The name of a DMIJI entry that defines the CAERO2 interference element downwashes

Record – AERO(3202,32,265) Aerodynamic physical data.

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Name

Word

Type

Description

1

ACSID

I

Aerodynamic coordinate system identification number

2

VELOCITY

RS

Velocity for aerodynamic force data recovery and to calculate the BOV parameter

3

REFC

RS

Reference length for reduced frequency

4

RHOREF

RS

Reference density

5

SYMXZ

I

Symmetry key for the aero coordinate xz plane

6

SYMXY

I

Symmetry key for the aero coordinate xy plane that can be used to simulate ground effects

Record – AEROS(2202,22,340) Static aeroelasticity physical data. Name

Word

Type

Description

1

ACSID

I

Aerodynamic coordinate system identification number

2

RCSID

I

Reference coordinate system identification number for rigid body motions

3

REFC

RS

Reference chord length

4

REFB

RS

Reference span

5

REFS

RS

Reference wing area

6

SYMXZ

I

Symmetry key for the aero coordinate xz plane

7

SYMXY

I

Symmetry key for the aero coordinate xy plane that can be used to simulate ground effects

Record – AESTAT(2102,21,339) Static aeroelasticity trim variables. Name

Word

Type

Description

1

ID

I

Identification number of an aerodynamic trim variable dof

2

LABEL(2)

CHAR4

An alphanumeric string identifying the dof

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Record – AESURF(2002,20,338) Aerodynamic control surface. Name

Word

Type

Description

1

ID

I

Controller identification number

2

LABEL(2)

CHAR4

Controller name

4

CID1

I

Identification number of a rectangular coordinate system with a y-axis defining the hinge line of the control surface component

5

ALID1

I

Identification number of an AELIST entry identifying all aerodynamic elements that make up the control surface component

6

CID2

I

Identification number of a rectangular coordinate system with a y-axis defining the hinge line of the control surface component

7

ALID2

I

Identification number of an AELIST entry identifying all aerodynamic elements that make up the control surface component

8

EFF

RS

Control surface effectiveness. Default = 1.0

9

LDW

I

Linear downwash flag

10

CREFC

RS

Reference chord length for the control surface

11

CREFS

RS

Reference surface area for the control surface

12

PLLIM

RS

Lower deflection limit for the control surface in rad

13

PULIM

RS

Upper deflection limit for the control surface in rad

14

HMLLIM

RS

Lower hinge moment limit for the control surface in force-length units

15

HMULIM

RS

Upper hinge moment limit for the control surface in force-length units

16

TQLLIM

RS

Set identification number of TABLED entry providing the lower deflection limit for the control surface as a function of dynamic pressure

17

TQULIM

RS

Set identification number of TABLED entry providing the upper deflection limit for the control surface as a function of dynamic pressure

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Record – AESURFS(7701,77,581) Aerodynamic control surface. Name

Word

Type

Description

1

ID

I

Identification number of an aerodynamic trim variable DOF

2

LABEL(2)

CHAR4

Control surface name

4

LIST1

I

Identification number of a SET1 entry that contains the grid IDs associated with this control surface

5

LIST2

I

Identification number of a SET1 entry that contains the grid IDs associated with this control surface

Record – BOLT(7108,71,251) Bolt definition. Name

Word

Type

1

BID

I

2

FLAG

I

BMID

I

Description Bolt identification number

FLAG = 1 3

Beam identification number

Word 3 repeats until -1 FLAG = 2

Not supported – for future use

3

CID

I

Bolt direction component number

4

G1

I

First grid point defining bolt direction

5

G2

I

Second grid point defining bolt direction

6

EID

I

Solid element identification number

Word 6 repeats until -1

Record – CAERO1(3002,30,263) Aerodynamic panel element connection.

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Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number of a PAERO1 entry

3

CP

I

Coordinate system for locating points 1 and 4

4

NSPAN

I

Number of spanwise boxes

5

NCHORD

I

Number of chordwise boxes

6

LSPAN

I

Identification number of an AEFACT entry containing a list of division points for spanwise boxes

7

LCHORD

I

Identification number of an AEFACT entry containing a list of division points for chordwise boxes

8

IGID

I

Interference group identification number

9

X1

RS

X-coordinate of point 1 in coordinate system CP

10

Y1

RS

Y-coordinate of point 1 in coordinate system CP

11

Z1

RS

Z-coordinate of point 1 in coordinate system CP

12

X12

RS

Edge chord length in aerodynamic coordinate system

13

X4

RS

X-coordinate of point 4 in coordinate system CP

14

Y4

RS

Y-coordinate of point 4 in coordinate system CP

15

Z4

RS

Z-coordinate of point 4 in coordinate system CP

16

X43

RS

Edge chord length in aerodynamic coordinate system

Record – CAERO2(4301,43,167) Aerodynamic body connection. Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number of a PAERO2 entry

3

CP

I

Coordinate system for locating point 1

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Name

Word

Type

Description

4

NSP

I

Number of slender body elements

5

NINT

I

Number of interference elements

6

LSP

I

Identification number of an AEFACT entry for slender body division points

7

LINT

I

Identification number of an AEFACT entry containing a list of division points for interference elements

8

IGID

I

Interference group identification number

9

X1

RS

X-coordinate of point 1 in coordinate system CP

10

Y1

RS

Y-coordinate of point 1 in coordinate system CP

11

Z1

RS

Z-coordinate of point 1 in coordinate system CP

12

X12

RS

Length of body in the x-direction of the aerodynamic coordinate system

13

UNDEF(4)

None

Record – CAERO3(4401,44,168) Aerodynamic panel element configuration. Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number of a PAERO3 entry

3

CP

I

Coordinate system for locating points 1 and 4

4

LISTW

I

Identification number of an AEFACT entry that lists coordinate pairs for structural interpolation of the wing

5

LISTC1

I

Identification number of an AEFACT entry that lists coordinate pairs for control surfaces

6

LISTC2

I

Identification number of an AEFACT entry that lists coordinate pairs for control surfaces

7

UNDEF(2)

None

9

X1

RS

X-coordinate of point 1 in coordinate system CP

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Name

Word

Type

Description

10

Y1

RS

Y-coordinate of point 1 in coordinate system CP

11

Z1

RS

Z-coordinate of point 1 in coordinate system CP

12

X12

RS

Edge chord length in aerodynamic coordinate system

13

X4

RS

X-coordinate of point 4 in coordinate system CP

14

Y4

RS

Y-coordinate of point 4 in coordinate system CP

15

Z4

RS

Z-coordinate of point 4 in coordinate system CP

16

X43

RS

Edge chord length in aerodynamic coordinate system

Record – CAERO4(4501,45,169) Aerodynamic macro-strip element connection. Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number of a PAERO4 entry

3

CP

I

Coordinate system for locating points 1 and 4

4

NSPAN

I

Number of strips

5

LSPAN

I

Identification number of an AEFACT entry containing a list of division points for strips

6

UNDEF(3)

None

9

X1

RS

X-coordinate of point 1 in coordinate system CP

10

Y1

RS

Y-coordinate of point 1 in coordinate system CP

11

Z1

RS

Z-coordinate of point 1 in coordinate system CP

12

X12

RS

Edge chord length in aerodynamic coordinate system

13

X4

RS

X-coordinate of point 4 in coordinate system CP

14

Y4

RS

Y-coordinate of point 4 in coordinate system CP

15

Z4

RS

Z-coordinate of point 4 in coordinate system CP

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Name

Word 16

X43

Type RS

Description Edge chord length in aerodynamic coordinate system

Record – CAERO5(5001,50,175) Aerodynamic panel element configuration. Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number of a PAERO5 entry

3

CP

I

Coordinate system for locating points 1 and 4

4

NSPAN

I

Number of strips

5

LSPAN

I

Identification number of an AEFACT entry containing a list of division points for strips

6

NTHRY

I

Parameter to select Piston or van Dyke’s theory

7

NTHICK

I

Parameter to select thickness integrals input

8

UNDEF

None

9

X1

RS

X-coordinate of point 1 in coordinate system CP

10

Y1

RS

Y-coordinate of point 1 in coordinate system CP

11

Z1

RS

Z-coordinate of point 1 in coordinate system CP

12

X12

RS

Edge chord length in aerodynamic coordinate system

13

X4

RS

X-coordinate of point 4 in coordinate system CP

14

Y4

RS

Y-coordinate of point 4 in coordinate system CP

15

Z4

RS

Z-coordinate of point 4 in coordinate system CP

16

X43

RS

Edge chord length in aerodynamic coordinate system

Record – CLOAD(6201,62,143) Static load combination for superelement loads.

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Name

Word

Type

Description

1

CID

I

Combination identification number

2

S

RS

Scale factor

3

SI

RS

Scale factors

4

IDVI

I

Identification numbers of load vectors

Words 3 and 4 repeat until (-1,-1) occurs

Record – CSSCHD(6401,64,307) Aerodynamic control surface schedule input. Name

Word

Type

Description

1

SID

I

Set identification number

2

AESID

I

Identification number of an AESURF entry to which the schedule is attached

3

LALPHA

I

Identification number of an AEFACT entry containing a list of angles of attack at which schedule information is provided

4

LMACH

I

Identification number of an AEFACT entry containing a list of Mach numbers at which schedule information is provided

5

LSCHD

I

Identification number of an AEFACT entry which contains the scheduling information

Record – DEFORM(104,1,81) Static element deformation. Name

Word

Type

Description

1

SID

I

Deformation set identification number

2

EID

I

Element number

3

D

RS

Deformation

Record – DIVERG(2702,27,387) Divergence analysis data.

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Data Block Descriptions A-E

Name

Word

Type

Description

1

SID

I

Unique set identification number

2

NROOT

I

Number of divergence roots to output

3

M

RS

Mach number

Word 3 repeats until -1 occurs

Record – FLFACT(4102,41,274) Aerodynamic physical data. Name

Word

Type

Description

1

SID

I

Set identification number

2

F

RS

Aerodynamic factor

Word 2 repeats until -1 occurs

Record – FLUTTER(3902,39,272) Aerodynamic flutter data. Word

Name

Type

Description

1

SID

I

Set identification number

2

METHOD(2)

CHAR4

Flutter analysis method

4

DENS

I

Identification number of an FLFACT entry specifying density ratios for flutter analysis

5

MACH

I

Identification number of an FLFACT entry specifying Mach numbers for flutter analysis

6

RFREQ

I

Identification number of an FLFACT entry specifying reduced frequencies for flutter analysis

7

IMETH(2)

CHAR4

Interpolation method for aerodynamic matrix interpolation

9

NEIGN

I

Number of eigenvalues beginning with the first eigenvalue

10

EPS

RS

Convergence parameter

Words 1 thru 10 repeat until -1 occurs

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Data Block Descriptions A-E

Record – ITER(5808,58,220) Iterative solver options. Name

Word

Type

Description

1

SID

I

Set identification number

2

PRECOND

I

Preconditioner option for global and element iterative solution

3

CONV

I

Convergence criterion

4

MSGFLG

I

Message flag

5

ITSEPS

RS

User-given convergence parameter epsilon

6

ITSMAX

I

Maximum number of iterations

7

IPAD

I

Global iterative solution padding value

8

IEXT

I

Global iterative solution extraction level in reduced or block incomplete Cholesky factorization

9

PREFONLY

I

Specifies early termination of the global iterative solver

10

ZPIVOT

RS

Singularity tolerance adjustment during the preconditioner phase of an element iterative solution

Record – MKAERO1(3802,38,271) Mach number and reduced frequency table. Name

Word 1

M(16)

Type RS

Description List of from 1 to 8 Mach numbers and their corresponding 1 to 8 reduced frequencies

Record – MKAERO2(3702,37,270) Mach number and reduced frequency table. Name

Word

Type

Description

1

M1

RS

Mach number

2

K1

RS

Reduced frequency

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Data Block Descriptions A-E

Name

Word

Type

Description

3

M2

RS

Mach number

4

K2

RS

Reduced frequency

5

M3

RS

Mach number

6

K3

RS

Reduced frequency

7

M4

RS

Mach number

8

K4

RS

Reduced frequency

Record – MONPNT1(7601,76,577) Integrated load monitor point. Name

Word

Type

Description

1

NAME(2)

CHAR4

Character string identifying the monitor point

3

LABEL(14)

CHAR4

Character string identifying and labeling the monitor point

17

AXES

I

Component axes about which to sum

18

COMP(2)

CHAR4

The name of an AECOMP or AECOMPL entry that defines the set of grid points over which the monitor point is defined

20

CID

I

Coordinate system identification number

21

X

RS

X-coordinate in the CID coordinate system

22

Y

RS

Y-coordinate in the CID coordinate system

23

Z

RS

Z-coordinate in the CID coordinate system

Record – PAERO1(3102,31,264) Aerodynamic panel property. Name

Word

Type

Description

1

PID

I

Property identification number referenced by a CAERO1 entry

2

B1

I

Identification number of CAERO2 entries for an associated body

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Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

3

B2

I

Identification number of CAERO2 entries for an associated body

4

B3

I

Identification number of CAERO2 entries for an associated body

5

B4

I

Identification number of CAERO2 entries for an associated body

6

B5

I

Identification number of CAERO2 entries for an associated body

7

B6

I

Identification number of CAERO2 entries for an associated body

8

UNDEF

None

Record – PAERO2(4601,46,170) Aerodynamic body properties. Name

Word

Type

Description

1

PID

I

Property identification number

2

ORIENT

CHAR4

Orientation flag

3

UNDEF

None

4

WIDTH

RS

Reference half-width of body and the width of the constant width interference tube

5

AR

RS

Aspect ratio of the interference tube (height/width)

6

LRSB

I

Identification number of an AEFACT entry containing a list of slender body half-widths at the end points of the slender body elements

7

LRIB

I

Identification number of an AEFACT entry containing a list of slender body half-widths at the end points of the interference elements

8

LTH1

I

Identification number of an AEFACT entry defining theta arrays for interference calculations

9

LTH2

I

Identification number of an AEFACT entry defining theta arrays for interference calculations

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Data Block Descriptions A-E

Name

Word

Type

Description

10

THI1

I

The first interference element of a body to use the theta1 array; others use the theta2 array

11

THN1

I

The last interference element of a body to use the theta1 array; others use the theta2 array

12

THI2

I

The first interference element of a body to use the theta1 array; others use the theta2 array

13

THN2

I

The last interference element of a body to use the theta1 array; others use the theta2 array

14

THI3

I

The first interference element of a body to use the theta1 array; others use the theta2 array

15

THN3

I

The last interference element of a body to use the theta1 array; others use the theta2 array

Record – PAERO3(4701,47,171) Aerodynamic panel property. Name

Word

Type

Description

1

PID

I

Property identification number

2

NBOX

I

Number of Mach boxes in the flow direction

3

FLAG

I

4

UNDEF

None

5

X5

RS

X-coordinate of point 5 in the aerodynamic coordinate system defining the cranks and control surface geometry

6

Y5

RS

Y-coordinate of point 5 in the aerodynamic coordinate system defining the cranks and control surface geometry

7

X6

RS

X-coordinate of point 6 in the aerodynamic coordinate system defining the cranks and control surface geometry

8

Y6

RS

Y-coordinate of point 6 in the aerodynamic coordinate system defining the cranks and control surface geometry

FLAG = 0

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Data Block Descriptions A-E

Name

Word

Type

Description

FLAG = 1 4

UNDEF

None

5

X5

RS

X-coordinate of point 5 in the aerodynamic coordinate system defining the cranks and control surface geometry

6

Y5

RS

Y-coordinate of point 5 in the aerodynamic coordinate system defining the cranks and control surface geometry

7

X6

RS

X-coordinate of point 6 in the aerodynamic coordinate system defining the cranks and control surface geometry

8

Y6

RS

Y-coordinate of point 6 in the aerodynamic coordinate system defining the cranks and control surface geometry

9

X7

RS

X-coordinate of point 7 in the aerodynamic coordinate system defining the cranks and control surface geometry

10

Y7

RS

Y-coordinate of point 7 in the aerodynamic coordinate system defining the cranks and control surface geometry

11

X8

RS

X-coordinate of point 8 in the aerodynamic coordinate system defining the cranks and control surface geometry

12

Y8

RS

Y-coordinate of point 8 in the aerodynamic coordinate system defining the cranks and control surface geometry

13

X9

RS

X-coordinate of point 9 in the aerodynamic coordinate system defining the cranks and control surface geometry

14

Y9

RS

Y-coordinate of point 9 in the aerodynamic coordinate system defining the cranks and control surface geometry

15

X10

RS

X-coordinate of point 10 in the aerodynamic coordinate system defining the cranks and control surface geometry

16

Y10

RS

Y-coordinate of point 10 in the aerodynamic coordinate system defining the cranks and control surface geometry

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Data Block Descriptions A-E

Name

Word

Type

Description

FLAG = 2 4

UNDEF

None

5

X5

RS

X-coordinate of point 5 in the aerodynamic coordinate system defining the cranks and control surface geometry

6

Y5

RS

Y-coordinate of point 5 in the aerodynamic coordinate system defining the cranks and control surface geometry

7

X6

RS

X-coordinate of point 6 in the aerodynamic coordinate system defining the cranks and control surface geometry

8

Y6

RS

Y-coordinate of point 6 in the aerodynamic coordinate system defining the cranks and control surface geometry

9

X7

RS

X-coordinate of point 7 in the aerodynamic coordinate system defining the cranks and control surface geometry

10

Y7

RS

Y-coordinate of point 7 in the aerodynamic coordinate system defining the cranks and control surface geometry

11

X8

RS

X-coordinate of point 8 in the aerodynamic coordinate system defining the cranks and control surface geometry

12

Y8

RS

Y-coordinate of point 8 in the aerodynamic coordinate system defining the cranks and control surface geometry

13

X9

RS

X-coordinate of point 9 in the aerodynamic coordinate system defining the cranks and control surface geometry

14

Y9

RS

Y-coordinate of point 9 in the aerodynamic coordinate system defining the cranks and control surface geometry

15

X10

RS

X-coordinate of point 10 in the aerodynamic coordinate system defining the cranks and control surface geometry

16

Y10

RS

Y-coordinate of point 10 in the aerodynamic coordinate system defining the cranks and control surface geometry

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Data Block Descriptions A-E

Name

Word

Type

Description

17

X11

RS

X-coordinate of point 11 in the aerodynamic coordinate system defining the cranks and control surface geometry

18

Y11

RS

Y-coordinate of point 11 in the aerodynamic coordinate system defining the cranks and control surface geometry

19

X12

RS

X-coordinate of point 12 in the aerodynamic coordinate system defining the cranks and control surface geometry

20

Y12

RS

Y-coordinate of point 12 in the aerodynamic coordinate system defining the cranks and control surface geometry

Record – PAERO4(4801,48,172) Aerodynamic strip properties. Word

Name

Type

Description

1

PID

I

Property identification number

2

CLA

I

Select Prandtl-Glauert correction

3

LCLA

I

Identification number of the AEFACT entry that lists the lift curve slope on all strips for each Mach number on the MKAERO entry

4

CIRC

I

Select Theodorsen’s function C(k) or the number of exponential coefficients used to approximate C(k)

5

LCIRC

I

Identification number of the AEFACT entry that lists the b, beta values for each Mach number

6

DOC

RS

Distance of the control surface hinge aft of the quarter-chord divided by the strip chord

7

CAOC

RS

Control surface chord divided by the strip chord

8

GAPOC

RS

Control surface gap divided by the strip chord

Words 6 thru 8 repeat until -1 occurs

Record – PAERO5(5101,51,176) Aerodynamic panel property.

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Data Block Descriptions A-E

Word

Name

Type

Description

1

PID

I

Property identification number

2

NALPHA

I

Number of angle of attack values input for each Mach number on the MKAERO1 or MKAERO2 entry

3

LALPHA

I

Identification number of the AEFACT entry that lists the angle of attack values for the strips at each Mach number in the MKAERO1 or MKAERO2 entry

4

NXIS

I

Number of dimensionless chord coordinates to be input

5

LXIS

I

Identification number of the AEFACT entry that lists the dimensionless chord coordinates for the strip in order indicated by values of NXIS and NTHICK

6

NTAUS

I

Number of thickness ratio values to be input

7

LTAUS

I

Identification number of the AEFACT entry that lists the number of thickness ratio values

8

CAOC

RS

Control surface chord divided by the strip chord

Word 8 repeats until -1 occurs

Record – PANEL(5301,53,378) Panel definition for coupled fluid-structural analysis. Word

Name

Type

Description

1

NAME(2)

CHAR4

Panel label

3

SETID

I

Identification number of a SET1 entry that lists the grid points of the panel

Words 1 thru 3 repeat until -1 occurs

Record – SET1(3502,35,268) Set definition. Word 1

Name SID

Type I

Description Unique identification number

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Data Block Descriptions A-E

Chapter 3

Name

Word 2

Type I

G

Description Structural grid point identification number

Word 2 repeats until -1 occurs

Record – SET2(3602,36,269) Grid point list. Word

Name

Type

Description

1

SID

I

Unique identification number

2

MACRO

I

Identification number of an aerodynamic macro element

3

SP1

RS

Lower span division point defining the prism containing the set

4

SP2

RS

Higher span division point defining the prism containing the set

5

CH1

RS

Lower chord division point defining the prism containing the set

6

CH2

RS

Higher chord division point defining the prism containing the set

7

ZMAX

RS

Z-coordinate of the top of the prism containing the set

8

ZMIN

RS

Z-coordinate of the bottom of the prism containing the set.

Record – SET3(4302,43,607) Set definition. Name

Word

Type

Description

1

SID

I

Set identification number

2

TYPE

I

Set type 1 = grid 2 = element 3 = property

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Data Block Descriptions A-E

Name

Word 3

ID

Type I

Description Identifying number for either structural grids, elements, or physical properties

Word 3 repeats until -1 occurs

Record – SPLINE1(3302,33,266) Surface spline methods. Name

Word

Type

Description

1

EID

I

Element identification number

2

CAERO

I

CAERO entry defining the plane of the spline

3

BOX1

I

First box with motions interpolated using this spline

4

BOX2

I

Last box with motions interpolated using this spline

5

SETG

I

The SETi entry listing the structural grid points to which the spline is attached

6

DZ

RS

Linear attachment flexibility

7

METH(2)

CHAR4

Method for the spline fit: IPS, TPS, or FPS

9

USAGE(2)

CHAR4

Spline usage flag to determine whether this spline applies to force transformation, displacement transformation, or both: FORCE, DISP, or BOTH

11

NELEM

I

Number of elements on x-axis for FPS

12

MELEM

I

Number of elements on y-axis for FPS

Record – SPLINE2(3402,34,267) Linear spline. Name

Word

Type

Description

1

EID

I

Element identification number

2

CAERO

I

CAERO entry that is to be interpolated

3

ID1

I

First box or body element with motions interpolated using this spline

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

ID2

I

Last box or body element with motions interpolated using this spline

5

SETG

I

The SETi entry listing the structural grid points to which the spline is attached

6

DZ

RS

Linear attachment flexibility

7

DTOR

RS

Torsional flexibility ratio

8

CID

I

Rectangular coordinate system for which the y-axis defines the axis of the spline

9

DTHX

RS

Rotational attachment flexibility for rotation about the x-axis of the spline

10

DTHY

RS

Rotational attachment flexibility for rotation about the y-axis of the spline

11

USAGE(2)

CHAR4

Spline usage flag to determine whether this spline applies to force transformation, displacement transformation, or both: FORCE, DISP, or BOTH

Record – SPLINE3(4901,49,173) Aeroelastic constraint equation. Name

Word

Type

Description

1

EID

I

Element identification number

2

CAERO

I

Identification number of the macro-element on which the element to be interpolated lies

3

BOXID

I

Identification number of the aerodynamic element

4

COMP

I

The component of motion to be interpolated

5

USAGE(2)

CHAR4

Spline usage flag to determine whether this spline applies to the force transformation, displacement transformation, or both: FORCE, DISP, or BOTH

7

G

I

Identification number of the independent grid point

8

C

I

Component number in the displacement coordinate system

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Data Block Descriptions A-E

Name

Word 9

A

Type RS

Description Coefficient of the constraint relationship

Words 7 thru 9 repeat until -1 occurs

Record – SPLINE4(6501,65,308) Surface spline methods. Name

Word

Type

Description

1

EID

I

Element identification number

2

CAERO

I

Aero panel identification number defining the interpolation surface

3

AELIST

I

Identification number of an AELIST entry listing boxes with motions that are interpolated using this spline

4

SETG

I

The SETi entry listing the structural grid points to which the spline is attached

5

DZ

RS

Linear attachment flexibility

6

METH(2)

CHAR4

Method for the spline fit: IPS, TPS, or FPS

8

USAGE(2)

CHAR4

Spline usage flag to determine whether this spline applies to force transformation, displacement transformation, or both: FORCE, DISP, or BOTH

10

NELEM

I

Number of elements along the local spline x-axis for FPS

11

MELEM

I

Number of elements along the local spline y-axis for FPS

Record – SPLINE5(6601,66,309) Linear spline. Word

Name

Type

Description

1

EID

I

Element identification number

2

CAERO

I

CAERO entry that is to be interpolated

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

3

AELIST

I

Identification number of an AELIST entry listing aerodynamic boxes with motions that are interpolated using this spline

4

SETG

I

The SETi entry listing the structural grid points to which the spline is attached

5

DZ

RS

Linear attachment flexibility

6

DTORXY

RS

Torsional flexibility ratio in xy-plane

7

CID

I

Rectangular coordinate system that defines the y-axis of the spline and the xy- and yz-planes for bending

8

DTHX

RS

Rotational attachment flexibility for rotation about the x-axis of the spline

9

DTHY

RS

Rotational attachment flexibility for rotation about the y-axis of the spline

10

DTHZ

RS

Set to 0.0

11

USAGE(2)

CHAR4

Spline usage flag to determine whether this spline applies to the force transformation, displacement transformation, or both: FORCE, DISP, or BOTH

13

METHOD(2)

CHAR4

Set to IPS

15

DTORZY

RS

Set to 1.0

Record – TRIM(2402,24,342) Trim variable constraint. Name

Word

Type

Description

1

SID

I

Trim set identification number

2

MACH

RS

Mach number

3

Q

RS

Dynamic pressure

4

AEQR

RS

Flag to request rigid trim analysis

5

LABEL(2)

CHAR4

AESTAT or AESURF entry identifying aerodynamic trim variables

7

UX

RS

Magnitude of aerodynamic extra point dof

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Data Block Descriptions A-E

Word

Name

Type

Description

Words 5 thru 7 repeat until (-1,-1,-1) occurs

Record – UXVEC(7201,72,573) Control parameter state. Word

Name

Type

Description

1

ID

I

Control vector identification number

2

LABEL(2)

CHAR4

Controller name

4

UX

RS

Magnitude of aerodynamic extra point dof

Words 2 thru 4 repeat until (-1,-1) occurs

Record – TRAILER Name

Word 1

UNDEF(6)

Type

Description

None

3.22 EGPSF Table of element to grid point surface interpolation factors Contains surface and volume data and element stress factors for each grid point in that surface or volume.

Record 0 – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data Block Name

Record 1 – IDENT Word 1

Name SRFTYP(C)

Type I

Description Entity Type: 2=surface and 3=volume. See Note 1.

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Data Block Descriptions A-E

Chapter 3

Record 2 – DATA Name

Word

Type

Description

SRFTYP =2

Surface definition

1

SURFID

I

Surface identification number

2

NKEYS(C)

I

Number of keywords in surface data

3

SURFID

I

Surface identification number

4

SETID

I

Set identification number

5

FIBRE

I

Fibre code for surfaces

6

OCID

I

Output coordinated system identification number

7

AXIS

I

Axis code

8

NORMAL

I

Normal code

9

METH

I

Method of calculation

10

TOL

RS

Tolerance

11

MSG

I

Branch message flag

12

BREAK

I

Break flag

13

ECID

I

Element coordinate system usage flag

14

UNDEF(7 )

None

21

UWMREF

I

Reference message flag

22

GPELREC

I

Record number of GPEL

23

NELS(C)

I

Number of elements in surface

24

EID

I

Element identification numbers in surface

Word 24 repeats NELS times 25

NG(C)

I

Number of grid points in surface

26

GRID

I

Grid point identification number (internal)

27

REFID

I

Reference element identification number

28

NE(C)

I

No. of elements contributing to stress at this grid

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DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

29

ELTYPE

I

Element type

30

ELID

I

Element identification number

31

THETA

RS

Angle stress point flag

32

FLAG

I

Angle stress point flag

33

FACTOR

RS

Stress Factor

Words 29 through 33 repeat NE times Words 26 through 33 repeat NG times SRFTYP =3

Volume definition

1

VOLID

I

Volume identification number

2

NKEYS(C)

I

Number of keywords in volume data

3

VOLIDN

I

Negative of volume identification number

4

SETID

I

Set identification number

5

STRESS

I

Stress code

6

UNDEF(7 )

None

13

ECID

I

14

UNDEF(8 )

None

22

GPELREC

I

Record number of GPEL

23

NELS(C)

I

Number of elements in volume

24

EID

I

Element identification numbers in volume

Element coordinate system usage flag

Word 24 repeats NELS times 25

NG(C)

I

Number of grid points in volume

26

GRID

I

Grid point identification number (internal)

27

REFID

I

Reference element identification number

28

NE(C)

I

No. of elements contributing to stress at this grid

29

ELTYPE

I

Element type

30

ELID

I

Element identification number

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Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

31

TOE(9)

RS

Element stress output 3x3 trans. matrix

40

FLAG

I

10*connectivity+identity flag. See Note 2.

41

FACTOR

RS

Factor to apply to stress

Words 29 through 41 repeat NE times Words 26 through 41 repeat NG times SRFTYP =–1

End of Data

End SRFTYP

Record 3 – TRAILER Word

Name

Type

1

NSV

I

2

UNDEF(5 )

None

Description Number of surfaces and volumes

Notes: 1. Records IDENT and DATA are repeated for each surface and volume. 2. In FLAG for volumes, connectivity refers to grid point position on connection entry and identity flag is 1 if TOE is an identity matrix. 3. Possible values for items in RECORD=DATA are: FIBRE

STRESS

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DMAP Programmer’s Guide

Fibre code for surfaces 0

All (Z1,Z2,MID) (default)

1

Z1 only

2

Z2 only

3

Z1 and Z2

4

MID only

5

Z1 and MID

6

Z2 and MID

7

All

Stress code for volumes

Data Block Descriptions A-E

OCID

AXIS

NORMAL

METH

MSG

2

Principal

1

Direct

0

Both

Output coordinate system ID 0

Basic system (default)

>0

User defined coordinate system

Axis code (surfaces only) 0

X axis (default)

1

Y axis

2

Z axis

Normal code (surfaces only) 0

Radius

1

X axis

2

Y axis

3

Z axis

-1

-X axis

-2

-Y axis

-3

-Z axis

10

Radius vector normal

Method of calculation (surfaces only) 0

Topological (default)

1

Geometric

Branch message flag (surfaces only) 0

No message (default)

1

Issue messages

BREAK

Break flag (surfaces only) 0

No break

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Data Block Descriptions A-E

1 ECID

Break

Element coordinate system usage flag 0

Not used

-1

Used

4. GPELREC is nonzero if warning messages concerning the reference normal or reference axis have been issued.

3.23 EGPSTR Element grid point stress table Provides grid point stress data for postprocessing.

Record 0 – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record 1 – Repeat See “EGPSF” for a description of surface and volume definition data. Name

Word

Type

Description

1

SUBVEC

I

Subcase or vector identification number

2

TSEIG

RS

Eigenvalue or time step value

3

TYPE(C)

I

Surface/volume type

4

SVID

I

Surface/volume identification number

5

NE(C)

I

Number of elements

6

EID

I

Element identification numbers

Word 6 repeats NE times 7

NS(C)

I

Number of words of in surface or volume data

8

DATA

I

Surface/volume definition data (See note above)

I

Number of grid points

Word 8 repeats NS times 9

3-166

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DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

10

GRID

I

Grid point identification number

11

ELID

I

Element identification number

TYPE =2

Surface stresses

12

FIBRE

CHAR4

Fibre name

13

SX

RS

Normal x

14

SY

RS

Normal y

15

TXY

RS

Shear xy

16

A

RS

Shear angle

17

SMAJ

RS

Major principal

18

SMIN

RS

Minor principal

19

TMAX

RS

Maximum shear

20

HVM

RS

Hencky/Von Mises

Words 12 through 20 repeat NF times TYPE =3

Volume stresses

12

SX

RS

Normal x

13

SY

RS

Normal y

14

SZ

RS

Normal z

15

TXY

RS

Shear xy

16

TYZ

RS

Shear yz

17

TZX

RS

Shear zx

18

MP

RS

Mean pressure

19

HVM

RS

Hencky-von Mises

20

SA

RS

Principal stresses in a-direction

21

SB

RS

Principal stresses in b-direction

22

SC

RS

Principal stresses in c-direction

23

LXA

RS

x-a direction cosine

DMAP Programmer’s Guide

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Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

24

LXB

RS

x-b direction cosine

25

LXC

RS

x-c direction cosine

26

LYA

RS

y-a direction cosine

27

LYB

RS

y-b direction cosine

28

LYC

RS

y-c direction cosine

29

LZA

RS

z-a direction cosine

30

LZB

RS

z-b direction cosine

31

LZC

RS

z-c direction cosine

End TYPE Words 10 through max repeat NG times

Record 2 – TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

Notes: 1. NF is based on the value of FIBRE and whether strain/curvature or stresses are being processed. If strain/curvature and FIBRE = 4, NF=1 If strain/curvature and FIBRE 4, NF=2 If stress FIBRE=1, 2, or 4, NF=1. If stress FIBRE=0, 3, 5, 6, or, 7, NF=3. 2. SUBVEC and TSEIG can have the following values:

3-168

Linear statics

subcase ID

0.0

Cyclic statics

vector ID

0.0

Nonlinear statics

subcase ID

load factor

Normal Modes

vector ID

eigenvalue

DMAP Programmer’s Guide

Data Block Descriptions A-E

Buckling

vector ID

critical load

Transient

vector ID

time

3. The element identification number is 0 unless more than one grid stress is output for a given grid point. In this case, the element identification number defines the connected element for the given grid point stress.

3.24 ELDCT Element stress discontinuity table Similar in format to “EGPSTR” .

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – Repeat See “EGPSF” for a description of surface and volume definition data Word

Name

Type

Description

1

SUBVEC

I

Subcase or vector identification number

2

TSEIG

RS

Eigenvalue or time step value

3

TYPE(C)

I

Surface/volume type

4

SVID

I

Surface/volume identification number

5

NS(C)

I

Number of words of in surface or volume data

6

DATA

I

Surface/volume definition data (See note above)

Word 6 repeats NS times 7

NE(C)

I

Number of elements

8

EID

I

Element identification number

9

TYPE

I

Element type

TYPE =2 10

Surface stress discontinuities FIBRE

CHAR4

Fibre name

DMAP Programmer’s Guide

3-169

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

11

SX

RS

Normal x

12

SY

RS

Normal y

13

TXY

RS

Shear xy

14

A

RS

Shear angle

15

SMAJ

RS

Major principal

16

SMIN

RS

Minor principal

17

TMAX

RS

Maximum shear

18

HVM

RS

Hencky/Von Mises

19

ERR

RS

Error estimate

Words 10 through 19 repeat NF times TYPE =3

Volume stresse discontinuities

10

SX

RS

Normal x

11

SY

RS

Normal y

12

SZ

RS

Normal z

13

TXY

RS

Shear xy

14

TYZ

RS

Shear yz

15

TZX

RS

Shear zx

16

MP

RS

Mean pressure

17

HVM

RS

Hencky-von Mises

18

SA

RS

Principal stresses in a-direction

19

SB

RS

Principal stresses in b-direction

20

SC

RS

Principal stresses in c-direction

21

ERRN

RS

Error estimate for normal stress

22

ERRP

RS

Error estimate for principal stress

End TYPE Words 8 through max repeat NE times

3-170

DMAP Programmer’s Guide

Data Block Descriptions A-E

Record 2 – TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

Notes: NF is based on the value of FIBRE and whether strain/curvature or stresses are being processed. •

If strain/curvature and FIBRE = 4, NF=1

•

If strain/curvature and FIBRE 4, NF=2

•

If stress FIBRE=1, 2, or 4, NF=1.

•

If stress FIBRE=0, 3, 5, 6, or 7, NF=3.

3.25 EPT Element property table.

RECORD – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

RECORD – BOLTS(7108,71,251) Name

Word 1

Type

Description

BID

I

Bolt identification number

BMID

I

Beam identification number

2

CID

I

Bolt direction component number

3

G1

I

First grid point defining bolt direction

4

G2

I

Second grid point defining bolt direction

5

EID

I

Solid element identification number

ETYPE=1 2 ETYPE=2

DMAP Programmer’s Guide

3-171

Data Block Descriptions A-E

Chapter 3

RECORD – MATCID(17006,170,901) Defines material coordinate system for solid elements. Name

Word

Type

Description

1

CID

I

Material coordinate system identification number

2

SPECOPT

I

Specification option

SPECOPT=1 3

Select individual element identification numbers EID

I

Element identification number

Word 3 repeats until -1 occurs SPECOPT=2 3

Select all element identification numbers ALL(2)

CHAR4

Keyword for selecting ‘ALL’ option

Words 3 repeats until -1 occurs SPECOPT=3

Select element identification numbers using a ‘THRU’ range without the ‘BY’ option

3

EID

I

Element identification number

4

THRU(2)

CHAR4

Keyword for selecting ‘THRU’ option

6

EID

I

Element identification number

Words 3 through 5 repeat until -1 occurs SPECOPT=4

Select element identification numbers using a ‘THRU’ range with the ‘BY’ option

3

EID

I

Element identification number

4

THRU(2)

CHAR4

Keyword for selecting ‘THRU’ option

6

EID

I

Element identification number

7

BY(2)

CHAR4

Keyword for selecting ‘BY’ option

9

N

I

Element selection increment

Words 3 through 9 repeat until -1 occurs

RECORD – NSM(3201,32,991) Defines the properties of a nonstructural mass.

3-172

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

4

ORIGIN

I

Entry origin

5

ID

I

Property or element identification number

6

VALUE

RS

Nonstructural mass value

Words 5 through 6 repeat until End of Record

RECORD – NSM1(3301,33,992) Defines the properties of a nonstructural mass. Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

4

ORIGIN

I

Entry origin

5

VALUE

RS

Nonstructural mass value

6

SPECOPT

I

Specification option

By IDs

SPECOPT=1 7

ID

I

Word 7 repeats until -1 occurs SPECOPT=2 7

All ALL(2)

CHAR4

Words 7 and 8 repeat until -1 occurs SPECOPT=3

Thru range

7

ID

I

8

THRU(2)

CHAR4

10

ID

I

Words 7 through 10 repeat until -1 occurs SPECOPT=4

Thru range with by

DMAP Programmer’s Guide

3-173

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

7

ID

I

8

THRU(2)

CHAR4

10

ID

I

11

BY(2)

CHAR4

13

N

I

Description

Words 7 through 13 repeat until -1 occurs

RECORD – NSMADD(3401,34,993) Combines the nonstructural mass inputs. Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Set of properties or elements

Word 2 repeats until End of Record

RECORD – NSML(3501,35,994) Defines a set of lumped nonstructural mass by ID. Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

4

ID

I

Property of element identification number

5

VALUE

RS

Lumped nonstructural mass value

Words 4 and 5 repeat until -1 occurs

RECORD – NSML1(3701,37,995) Alternate form of NSML entry. Defines lumped nonstructural mass entries by VALUE, ID list. Name

Word 1

3-174

SID

DMAP Programmer’s Guide

Type I

Description Set identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

PROP(2)

CHAR4

Set of properties or elements

4

VALUE

RS

Lumped nonstructural mass value

5

SPECOPT

I

Specification option

By IDs

SPECOPT=1 6

ID

I

Property of element identification number

Word 6 repeats until -1 occurs SPECOPT=2 6

All ALL(2)

CHAR4

Keyword ALL

Words 6 and 7 repeat until -1 occurs SPECOPT=3

Thru range

6

ID1

I

Starting identification number

7

THRU(2)

CHAR4

Keyword THRU

9

ID2

I

Ending identification number

Words 6 through 9 repeat until -1 occurs SPECOPT=4

Thru range with by

6

ID1

I

Starting identification number

7

THRU(2)

CHAR4

Keyword THRU

9

ID2

I

Ending identification number

10

BY(2)

CHAR4

Keyword BY

12

N

I

Increment

Words 6 through 12 repeat until -1 occurs

RECORD – PAABSF(1502,15,36) Defines the properties of a frequency-dependent acoustic absorber Word 1

Name PID

Type I

Description Property identification number

DMAP Programmer’s Guide

3-175

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

2

TZREID

I

TABLEDi entry identification number for resistance

3

TZMID

I

TABLEDi entry identification number for reactance

4

S

RS

Impedance scale factor

5

A

RS

Area factor when only 1 or 2 grid points are specified

6

B

RS

Equivalent structural damping

7

K

RS

Equivalent stiffness

8

RHOC

RS

Constant used for absorption coefficient

RECORD – PACABS(8300,83,382) Defines the properties of the acoustic absorber element Name

Word

Type

Description

1

PID

I

Property identification number

2

SYNTH

I

Request the calculation of B, K, and M

3

TID1

I

TABLEDi entry identification number for resistance

4

TID2

I

TABLEDi entry identification number for reactance

5

TID3

I

TABLEDi entry identification number for weighting function

6

TESTAR

RS

Area of the test specimen

7

CUTFR

RS

Cutoff frequency for tables referenced above

8

B

RS

Equivalent structural damping values

9

K

RS

Equivalent structural stiffness

10

M

RS

Equivalent mass

RECORD – PACBAR(8500,85,384) Acoustic barrier element.

3-176

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

1

PID

I

Property identification number

2

MBACK

RS

Mass per unit area of the backing material

3

MSEPTM

RS

Mass per unit area of the septum material

4

FRESON

RS

Resonant frequency of the sandwich construction

5

KRESON

RS

Resonant stiffness of the sandwich construction

RECORD – PBAR(52,20,181) Simple beam element. Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

I1

RS

Area moment of inertia in plane 1

5

I2

RS

Area moment of inertia in plane 2

6

J

RS

Torsional constant

7

NSM

RS

Nonstructural mass per unit length

8

FE

RS

9

C1

RS

Stress recovery location at point C in element y-axis

10

C2

RS

Stress recovery location at point C in element z-axis

11

D1

RS

Stress recovery location at point D in element y-axis

12

D2

RS

Stress recovery location at point D in element z-axis

13

E1

RS

Stress recovery location at point E in element y-axis

14

E2

RS

Stress recovery location at point E in element z-axis

DMAP Programmer’s Guide

3-177

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

15

F1

RS

Stress recovery location at point F in element y-axis

16

F2

RS

Stress recovery location at point F in element z-axis

17

K1

RS

Area factor for shear in plane 1

18

K2

RS

Area factor for shear in plane 2

19

I12

RS

Area product of inertia for plane 1 and 2

RECORD – PBARL(9102,91,52) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

GROUP(2)

CHAR4

Cross-section group name

5

TYPE(2)

CHAR4

Cross section type

7

VALUE

RS

Cross-section dimensions and NSM

Word 7 repeats until End of Record

RECORD – PBCOMP(5403,55,349) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

I1

RS

Area moment of inertia in plane 1

5

I2

RS

Area moment of inertia in plane 2

6

I12

RS

Area product of inertia for plane 1 and 2

7

J

RS

Torsional constant

8

NSM

RS

Nonstructural mass per unit length

9

K1

RS

Area factor for shear in plane 1

3-178

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

10

K2

RS

Area factor for shear in plane 2

11

M1

RS

Location center of gravity of nonstructural mass along y-axis

12

M2

RS

Location center of gravity of nonstructural mass along y-axis

13

N1

RS

Location neutral axis along element’s y-axis

14

N2

RS

Location neutral axis along element’s y-axis

15

NSECT(C)

I

Number of lumped areas

Name

Word

Type

Description

NSECT =0 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

UNDEF(3 )

None

Words 16 through 20 repeat 4 times Name

Word

Type

Description

NSECT =1 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =2 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

DMAP Programmer’s Guide

3-179

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =3 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =4 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =5 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

3-180

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

19

MID

I

20

UNDEF

None

Description Material identification number

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =6 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =7 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =8 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

DMAP Programmer’s Guide

3-181

Data Block Descriptions A-E

Chapter 3

Name

Word 20

UNDEF

Type

Description

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =9 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =10 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =11 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

3-182

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =12 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =13 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =14 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times

DMAP Programmer’s Guide

3-183

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

NSECT =15 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =16 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =17 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Word

Name

NSECT =18

3-184

DMAP Programmer’s Guide

Type

Description

Data Block Descriptions A-E

Name

Word

Type

Description

16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =19 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =20 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times End NSECT

DMAP Programmer’s Guide

3-185

Data Block Descriptions A-E

Chapter 3

RECORD – PBEAM(5402,54,262) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

NSEGS

I

Number of segments*

4

CCF

I

Constant cross-section flag: 1=yes and 0=no

5

X

RS

6

SO

RS

Stress output request

7

XXB

RS

Distance ratio from end A

8

A

RS

Area

9

I1

RS

Area moment of inertia in plane 1

10

I2

RS

Area moment of inertia in plane 2

11

I12

RS

Area product of inertia for plane 1 and 2

12

J

RS

Torsional constant

13

NSM

RS

Nonstructural mass per unit length

14

C1

RS

Stress recovery location at point C in element y-axis

15

C2

RS

Stress recovery location at point C in element z-axis

16

D1

RS

Stress recovery location at point D in element y-axis

17

D2

RS

Stress recovery location at point D in element z-axis

18

E1

RS

Stress recovery location at point E in element y-axis

19

E2

RS

Stress recovery location at point E in element z-axis

20

F1

RS

Stress recovery location at point F in element y-axis

21

F2

RS

Stress recovery location at point F in element z-axis

3-186

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

Words 6 through 21 repeat 11 times 22

K1

RS

Area factor for shear in plane 1

23

K2

RS

Area factor for shear in plane 2

24

S1

RS

Shear relief coefficient due to taper for plane 1

25

S2

RS

Shear relief coefficient due to taper for plane 1

26

NSIA

RS

Nonstructural mass moment of inertia per unit length at end A

27

NSIB

RS

Nonstructural mass moment of inertia per unit length at end B

28

CWA

RS

Warping coefficient for end A

29

CWB

RS

Warping coefficient for end B

30

M1A

RS

Location of C.G. of nonstructural mass at end A along y-axis

31

M2A

RS

Location of C.G. of nonstructural mass at end A along z-axis

32

M1B

RS

Location of C.G. of nonstructural mass at end B along y-axis

33

M2B

RS

Location of C.G. of nonstructural mass at end B along z-axis

34

N1A

RS

Location of neutral axis at end A along element’s y-axis

35

N2A

RS

Location of neutral axis at end A along element’s z-axis

36

N1B

RS

Location of neutral axis at end B along element’s y-axis

37

N2B

RS

Location of neutral axis at end B along element’s z-axis

RECORD – PBEAML(9202,92,53) Name

Word 1

PID

Type I

Description Property identification number

DMAP Programmer’s Guide

3-187

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

2

MID

I

Material identification number

3

GROUP(2)

CHAR4

Cross-section group name

5

TYPE(2)

CHAR4

Cross section type

7

VALUE

RS

Cross section values for XXB, SO, NSM, and dimensions

Word 7 repeats until (–1) occurs

RECORD – PBEND(2502,25,248) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

I1

RS

Area moment of inertia in plane 1

5

I2

RS

Area moment of inertia in plane 2

6

J

RS

Torsional constant

7

FSI

I

Flexibility and stress intensification factors

8

RM

RS

Mean cross-sectional radius of the curved pipe

9

T

RS

Wall thickness of the curved pipe

10

P

RS

Internal pressure

11

RB

RS

Bend radius of the line of centroids

12

THETAB

RS

Arc angle of element

13

C1

RS

Stress recovery location at point C in element y-axis

14

C2

RS

Stress recovery location at point C in element z-axis

15

D1

RS

Stress recovery location at point D in element y-axis

16

D2

RS

Stress recovery location at point D in element z-axis

3-188

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

17

E1

RS

Stress recovery location at point E in element y-axis

18

E2

RS

Stress recovery location at point E in element z-axis

19

F1

RS

Stress recovery location at point F in element y-axis

20

F2

RS

Stress recovery location at point F in element z-axis

21

K1

RS

Area factor for shear in plane 1

22

K2

RS

Area factor for shear in plane 2

23

NSM

RS

Nonstructural mass per unit length

24

RC

RS

Radial offset of the geometric centroid

25

ZC

RS

Offset of the geometric centroid

26

DELTAN

RS

Radial offset of the neutral axis from the geometric centroid

27

SACL

RS

Miter spacing at center line.

28

ALPHA

RS

One-half angle between the adjacent miter axis (Degrees).

29

FLANGE

I

For FSI=5, defines the number of flanges attached.

30

KX

RS

For FSI=6, the user defined flexibility factor for the torsional moment.

31

KY

RS

For FSI=6, the user defined flexibility factor for the out-of-plane bending moment.

32

KZ

RS

For FSI=6, the user defined flexbility factor for the in-plane bending moment.

33

Not used

34

SY

RS

For FSI=6, the user defined stress intensification factor for the out-of-plane bending.

35

SZ

RS

For FSI=6, the user defined stress intensification factor for the in-plane bending.

DMAP Programmer’s Guide

3-189

Data Block Descriptions A-E

Chapter 3

RECORD – PBUSH(1402,14,37) Name

Word

Type

Description

1

PID

I

Property identification number

2

K(6)

RS

Nominal stiffness values

8

B(6)

RS

Nominal damping coefficient

14

GE(6)

RS

Nominal structural damping constant

20

SA

RS

Stress recovery coefficient in the translational component

21

ST

RS

Stress recovery coefficient in the rotational component

22

EA

RS

Strain recovery coefficient in the translational component

23

ET

RS

Strain recovery coefficient in the rotational component

RECORD – PBUSH1D(3101,31,219) Name

Word

Type

Description

1

PID

I

Property identification number

2

K

RS

Stiffness

3

C

RS

Viscous Damping

4

M

RS

Mass

5

ALPHA

RS

Temperature coefficient

6

SA

RS

Stress recovery coefficient

7

EA

RS

Strain recovery coefficient

8

TYPEA

I

Shock data type: 0=Null, 1=Table, 2=Equation

9

CVT

RS

Coefficient of translation velocity tension

10

CVC

RS

Coefficient of translation velocity compression

11

EXPVT

RS

Exponent of velocity tension

12

EXPVC

RS

Exponent of velocity compression

3-190

DMAP Programmer’s Guide

Data Block Descriptions A-E

Word

Name

Type

Description

13

IDTSU

I

TABLEDi or DEQATN entry identification number for scale factor vs displacement

14

IDTCU

I

DEQATN entry identification number for scale factor vs displacement

15

IDTSUD

I

DEQATN entry identification number for derivative tension

16

IDCSUD

I

DEQATN entry identification number for derivative compression

17

TYPES

I

Spring data type: 0=Null, 1=Table, 2=Equation

18

IDTS

I

TABLEDi or DEQATN entry identification number for tension compression

19

IDCS

I

DEQATN entry identification number for compression

20

IDTDU

I

DEQATN entry identification number for scale factor vs displacement

21

IDCDU

I

DEQATN entry identification number for force vs displacement

22

TYPED

I

Damper data type: 0=Null, 1=Table, 2=Equation

23

IDTD

I

TABLEDi or DEQATN entry identification number for tension compression

24

IDTD

I

DEQATN entry identification number for compression

25

IDTDV

I

DEQATN entry identification number for scale factor versus velocity

26

IDCDV

I

DEQATN entry identification number for force versus velocity

27

TYPEG

I

General data type: 0=Null, 1=Table, 2=Equation

28

IDTG

I

TABLEDi or DEQATN entry identification number for tension compression

29

IDCG

I

DEQATN entry identification number for compression

30

IDTDU

I

DEQATN entry identification number for scale factor versus displacement

DMAP Programmer’s Guide

3-191

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

31

IDCDU

I

DEQATN entry identification number for force versus displacement

32

IDTDV

I

DEQATN entry identification number for scale factor versus velocity

33

IDCDV

I

DEQATN entry identification number for force vs velocity

34

TYPEF

I

Fuse data type: 0=Null, 1=Table

35

IDTF

I

TABLEDi entry identification number for tension

36

IDCF

I

TABLEDi entry identification number for compression

37

UT

RS

Ultimate tension

38

UC

RS

Ultimate compression

RECORD – PBUSHT(702,7,38) Name

Word

Type

Description

1

PID

I

Property identification number

2

TKID(6)

I

TABLEDi entry identification numbers for stiffness

8

TBID(6)

I

TABLEDi entry identification numbers for viscous damping

14

TGEID(6)

I

TABLEDi entry identification number for structural damping

20

TKNID(6)

I

TABLEDi entry IDs for force versus deflection

RECORD – PCOMP(2706,27,287) Name

Word

Type

Description

1

PID

I

Property identification number

2

N(C)

I

Number of plies

3

Z0

RS

Distance from the reference plane to the bottom surface

4

NSM

RS

Nonstructural mass per unit area

3-192

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

5

SB

RS

Allowable shear stress of the bonding material

6

FT

I

Failure theory

7

TREF

RS

Reference temperature

8

GE

RS

Damping coefficient

9

MID

I

Material identification number

10

T

RS

Thicknesses of the ply

11

THETA

RS

Orientation angle of the longitudinal direction of the ply

12

SOUT

I

Stress or strain output request of the ply

Words 9 through 12 repeat N times

RECORD – PCOMPG(15006,150,604) Name

Word

Type

Description

1

PID

I

Property identification number

2

LAMOPT

I

Laminate option

3

Z0

RS

Distance from the reference plane to the bottom surface

4

NSM

RS

Nonstructural mass per unit area

5

SB

RS

Allowable shear stress of the bonding material

6

FT

I

Failure theory

7

TREF

RS

Reference temperature

8

GE

RS

Damping coefficient

9

GPLYIDi

I

Global ply IDs.

10

MID

I

Material identification number

11

T

RS

Thicknesses of the ply

12

THETA

RS

Orientation angle of the longitudinal direction of the ply

13

SOUT

I

Stress or strain output request of the ply

DMAP Programmer’s Guide

3-193

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

Words 9 through 13 repeat N times

RECORD – PCOMPS(16006,160,903) Defines the properties of an n-ply composite material laminate for solid elements. Name

Word

Type

Description

1

PID

I

Property identification number

2

CORDM

I

Material coordinate system identification number

3

PSDIR

I

Stack and ply directions in the material coordinate system

4

SB

RS

Allowable shear stress of the bonding material

5

NB

RS

Allowable normal stress of the bonding material

6

TREF

RS

Reference temperature

7

GE

RS

Damping coefficient

8

UNDEF

None

9

GPLYIDi

I

Global ply identification number

10

MID

I

Material identification number

11

TR

RS

Thicknesses of the ply

12

THETA

RS

Orientation angle of the longitudinal direction of the ply

13

FT

I

Failure theory

14

ILFT

I

Inter-laminar failure theory

15

SOUT

I

Stress or strain output request of the ply

16

TFLAG

I

Flag of ‘ABS’ or ‘REL’

Words 9 through 16 repeat until (-1,-1,-1,-1,-1,-1,-1,-1) occurs

RECORD – PCONEAX(152,19,147) Word

Name

1

PID

3-194

DMAP Programmer’s Guide

Type I

Description Property identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

MID1

I

Material identification number for membrane

3

T1

RS

Membrane thickness

4

MID2

I

Material identification number for bending

5

I

RS

Moment of inertia per unit width

6

MID3

I

Material identification number for transverse shear

7

T2

RS

Transverse shear thickness

8

NSM

RS

Nonstructural mass per unit area

9

Z1

RS

Fiber distance 1 from the middle surface for stress recovery

10

Z2

RS

Fiber distance 2 from the middle surface for stress recovery

11

PHI

RS

Azimuthal angle for stress recovery

Word 11 repeats 14 times

RECORD – PCONV(11001,110,411) Word

Name

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

FORM

I

Type of formula used for free convection

4

EXPF

RS

Free convection exponent

RECORD – PCONVM(2902,29,420) Word

Name

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

FORM

I

Type of formula used for free convection

4

FLAG

I

Flag for mass flow convection

DMAP Programmer’s Guide

3-195

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

5

COEF

RS

Constant coefficient used for forced convection

6

EXPR

RS

Reynolds number convection exponent

7

EXPPI

RS

Prandtl number convection exponent into the working fluid

8

EXPPO

RS

Prandtl number convection exponent out of the working fluid

RECORD – PDAMP(202,2,45) Name

Word

Type

Description

1

PID

I

Property identification number

2

B

RS

Force per unit velocity

RECORD – PDAMPT(1202,12,33) Name

Word

Type

Description

1

PID

I

Property identification number

2

TBID

I

TABLEDi entry identification number for viscous damping

RECORD – PDAMP5(8702,87,412) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

B

RS

Damping multiplier

RECORD – PDUM1(6102,61,116) Word 1

Name UNDEF

Type None

Word 1 repeats until End of Record

3-196

DMAP Programmer’s Guide

Description

Data Block Descriptions A-E

RECORD – PDUM2(6202,62,117) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM3(6302,63,118) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM4(6402,64,159) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM5(6502,65,160) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM6(6602,66,161) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM7(6702,67,163) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

DMAP Programmer’s Guide

3-197

Data Block Descriptions A-E

Chapter 3

RECORD – PDUM8(6802,68,164) Name

Word 1

Type

UNDEF

Description

None

Word 1 repeats until End of Record

RECORD – PDUM9(6902,69,165) Name

Word 1

Type

UNDEF

Description

None

Word 1 repeats until End of Record

RECORD – PELAS(302,3,46) Name

Word

Type

Description

1

PID

I

Property identification number

2

K

RS

Elastic property value

3

GE

RS

Damping coefficient

4

S

RS

Stress coefficient

RECORD – PELAST(1302,13,34) Word

Name

Type

Description

1

PID

I

Property identification number

2

TKID

I

TABLEDi entry identification number for stiffness

3

TGEID

I

TABLEDi entry identification number for structural damping

4

TKNID

I

TABLEDi entry identification number for force vs. deflection

RECORD – PFAST(3601,36,55) Word

Name

1

PID

3-198

DMAP Programmer’s Guide

Type I

Description Property identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

D

RS

Diameter of the spot weld

3

MCID

I

Element stiffness coordinate system

4

MFLAG

I

Defines MCID as absolute or relative

5-7

KT(3)

RS

Translational stiffness

8-10

KR(3)

RS

Rotational stiffness

11

MASS

RS

Lumped mass

12

GE

RS

Structural damping

RECORD – PGAP(2102,21,121) Name

Word

Type

Description

1

PID

I

Property identification number

2

UO

RS

Initial gap opening

3

FO

RS

Preload

4

KA

RS

Axial stiffness for the closed gap

5

KB

RS

Axial stiffness for the open gap

6

KT

RS

Transverse stiffness when the gap is closed

7

MU1

RS

Coefficient of static friction

8

MU2

RS

Coefficient of kinetic friction

9

TMAX

RS

Maximum allowable penetration

10

MAR

RS

Maximum allowable adjustment ratio

11

TRMIN

RS

Fraction of TMAX for the lower bound of penetration

RECORD – PHBDY(2802,28,236) Word

Name

Type

Description

1

PID

I

Property identification number

2

AF

RS

Area factor of the surface

DMAP Programmer’s Guide

3-199

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

3

D1

RS

Diameter 1 associated with the surface

4

D2

RS

Diameter 1 associated with the surface

RECORD – PINTC(12001,120,480) Name

Word

Type

Description

1

PID

I

Property identification number

2

TOL

RS

Tolerance between interface elements and subdomain boundaries

3

DSCALE

RS

Scaling parameter for Lagrange multiplier functions

4

UNDEF(5 )

None

RECORD – PINTS(12101,121,484) Name

Word

Type

Description

1

PID

I

Property identification number

2

TOL

RS

Tolerance between interface elements and subdomain boundaries

3

DSCALE

RS

Scaling parameter for Lagrange multiplier functions

4

UNDEF(5 )

None

RECORD – PLPLANE(4606,46,375) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

CID

I

Coordinate system identification number

4

STR

CHAR4

Location of stress and strain output

5

T

RS

Default membrane thickness for Ti on the connection entry

6

UNDEF(6)

None

3-200

DMAP Programmer’s Guide

Data Block Descriptions A-E

RECORD – PLSOLID(4706,47,376) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

STR

CHAR4

Location of stress and strain output

4

UNDEF(4 )

None

RECORD – PMASS(402,4,44) Name

Word

Type

Description

1

PID

I

Property identification number

2

M

RS

Mass

RECORD – PPLANE(3801,38,979) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

T

RS

Default membrane thickness for Ti on the connection entry

4

NSM

RS

Nonstructural mass per unit area

5

FOROPT

I

Formulation option number

6

UNDEF(3)

None

RECORD – PROD(902,9,29) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

J

RS

Torsional constant

5

C

RS

Coefficient to determine torsional stress

DMAP Programmer’s Guide

3-201

Data Block Descriptions A-E

Chapter 3

Name

Word 6

NSM

Type RS

Description Nonstructural mass per unit length

RECORD – PSHEAR(1002,10,42) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

T

RS

Thickness o

4

NSM

RS

Nonstructural mass per unit area.

5

F1

RS

Effectiveness factor for stiffness along edges 1-2 and 3-4

6

F2

RS

Effectiveness factor for stiffness along edges 2-3 and 1-4

RECORD – PSHELL(2302,23,283) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID1

I

Material identification number for the membrane

3

T

RS

Default membrane thickness for Ti on the connection entry

4

MID2

I

Material identification number for bending

5

BK

RS

Bending moment of inertia ratio

6

MID3

I

Material identification number for transverse shear

7

TS

RS

Transverse shear thickness ratio

8

NSM

RS

Nonstructural mass per unit area

9

Z1

RS

Fiber distance 1 for stress calculation

10

Z2

RS

Fiber distance 1 for stress calculation

11

MID4

I

Material identification number for membrane-bending coupling

3-202

DMAP Programmer’s Guide

Data Block Descriptions A-E

RECORD – PSOLID(2402,24,281) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

CORDM

I

Material coordinate system identification number

4

IN

I

Integration network

5

STRESS

I

Location selection for stress output

6

ISOP

I

Integration scheme

7

FCTN

CHAR4

Fluid element flag

RECORD – PSOLIDL(7602,76,370) Name

Word

Type

1

PID

I

2

FT

I

3

TREF

RS

4

GE

RS

5

NSM

RS

6

NLAY

I

7

MID

I

8

T1

RS

9

THETA

RS

10

SOUT

I

Description Property identification number

Material identification number

Words 7 through 10 repeat 40 times

RECORD – PTRIA6(6202,62,117) Word 1

Name PID

Type I

Description Property identification number

DMAP Programmer’s Guide

3-203

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

2

MID

I

3

REAL(4)

RS

Description Material identification number

RECORD – PTUBE(1602,16,30) This record is slightly unstructured: OD2 is only written out if heat transfer Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

OD

RS

Outside diameter of tube

4

T

RS

Thickness of tube

5

NSM

RS

Nonstructural mass per unit length

6

OD2

RS

Heat transfer only: Outside diameter of tube

RECORD – PSET(10301,103,399) Name

Word

Type

Description

1

ID

I

p-value set identification number

2

POLY1

I

Polynomial order in 1 direction of the CID system

3

POLY2

I

Polynomial order in 2 direction of the CID system

4

POLY3

I

Polynomial order in 2 direction of the CID system

5

CID

I

Coordinate system identification number

6

TYPE

CHAR4

Type of set provided: "SET" or "ELID"

7

TYPEID

I

SET identification number or element identification number with this p-value specification.

Words 1 through 7 repeat until End of Record

RECORD – PVAL(10201,102,400) Name

Word 1

3-204

ID

DMAP Programmer’s Guide

Type I

Description p-value set identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

POLY1

I

Polynomial order in 1 direction of the CID system

3

POLY2

I

Polynomial order in 2 direction of the CID system

4

POLY3

I

Polynomial order in 2 direction of the CID system

5

CID

I

Coordinate system identification number

6

TYPE

CHAR4

Type of set provided: "SET" or "ELID"

7

TYPEID

I

SET identification number or element identification number with this p-value specification.

Words 1 through 7 repeat until End of Record

RECORD – PVISC(1802,18,31) Name

Word

Type

Description

1

PID

I

Property identification number

2

CE

RS

Viscous damping for extension

3

CR

RS

Viscous damping for rotation

RECORD – PWELD(11801,118,560) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material property identification number

3

D

RS

Diameter of the spot weld

4

CONNBEH

I

Connection behavior (0=FF/F, 1=FR, 10=RF/R, 11=RR)

5

CONNTYPE

I

Connection type (0=clamp, 1=hinge, 2=bolt)

6

EXTCON

I

External constraint flag (0=off, 1=on)

7

CONDTYPE

I

Condition type (0=rigid, 1=equivalent)

8

WELDTYPE

I

Weld type (0=spot weld, 1=but seam, 2=T-seam)

9

MINLEN

RS

Minimum length of spot weld

DMAP Programmer’s Guide

3-205

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

10

MAXLEN

RS

Maximum length of spot weld

11

GMCHK

I

Perform geometry check

12

SPCGS

I

SPC the master grid GS

13

CMASS

RS

Concentrated mass

14

UNDEF(1)

None

RECORD – VIEW(2606,26,289) Name

Word

Type

Description

1

IVIEW

I

View identification number

2

ICAVITY

I

Cavity identification number

3

SHADE

I

Shadowing flag for the face of CHBDYi element

4

NB

I

Subelement mesh size in the beta direction

5

NG

I

Subelement mesh size in the gamma direction

6

DISLIN

RS

Displacement of a surface perpendicular to the surface

RECORD – VIEW3D(3002,30,415) Word

Name

Type

Description

1

ICAVITY

I

Radiant cavity identification number

2

GITB

I

Gaussian integration order for third-body shadowing

3

GIPS

I

Gaussian integration order for self-shadowing

4

CIER

I

Discretization level

5

ETOL

RS

Error estimate

6

ZTOL

RS

Zero tolerance

7

WTOL

RS

Warpage tolerance

8

RADCHK

I

Radiation exchange diagnostic output level

3-206

DMAP Programmer’s Guide

Data Block Descriptions A-E

TRAILER Name

Word 1

Type

Description

I

BIT(6)

Record presence trailer words

3.26 EPT705 Element property table (Pre-MSC Nastran 2001). Note See the Note 1 for a listing of the differences between EPT705 and EPT.

RECORD – HEADER Name

Word 1

Type

Description

CHAR4

NAME(2)

Data block name

RECORD – BOLTS(7108,71,251) Name

Word 1

Type

Description

BID

I

Bolt identification number

BMID

I

Beam identification number

2

CID

I

Bolt direction component number

3

G1

I

First grid point defining bolt direction

4

G2

I

Second grid point defining bolt direction

5

EID

I

Solid element identification number

ETYPE=1 2 ETYPE=2

RECORD – NSM(3201,32,991) Defines the properties of a nonstructural mass. Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

DMAP Programmer’s Guide

3-207

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

ORIGIN

I

Entry origin

5

ID

I

Property or element identification number

6

VALUE

RS

Nonstructural mass value

Words 5 through 6 repeat until End of Record

RECORD – NSM1(3301,33,992) Defines the properties of a nonstructural mass. Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

4

ORIGIN

I

Entry origin

5

VALUE

RS

Nonstructural mass value

6

SPECOPT

I

Specification option

By IDs

SPECOPT=1 7

ID

I

Word 7 repeats until End of Record SPECOPT=2 7

All ALL(2)

CHAR4

Words 7 and 8 repeat until End of Record SPECOPT=3

Thru range

7

ID

I

8

THRU(2)

CHAR4

10

ID

I

Words 7 through 10 repeat until End of Record SPECOPT=4

Thru range with by

7

ID

I

8

THRU(2)

CHAR4

3-208

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

10

ID

I

11

BY(2)

CHAR4

13

N

I

Description

Words 7 through 13 repeat until End of Record End SPECOPT

RECORD – NSMADD(3401,34,993) Combines the nonstructural mass inputs. Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Set of properties or elements

Word 2 repeats until End of Record

RECORD – NSML(3501,35,994) Defines a set of lumped nonstructural mass by ID. Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

4

ID

I

Property of element identification number

5

VALUE

RS

Lumped nonstructural mass value

Words 4 and 5 repeat until -1 occurs

RECORD – NSML1(3701,37,995) Alternate form of NSML entry. Defines lumped nonstructural mass entries by VALUE, ID list. Name

Word

Type

Description

1

SID

I

Set identification number

2

PROP(2)

CHAR4

Set of properties or elements

DMAP Programmer’s Guide

3-209

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

4

VALUE

RS

Lumped nonstructural mass value

5

SPECOPT

I

Specification option

By IDs

SPECOPT=1 6

ID

I

Property of element identification number

Word 6 repeats until -1 occurs SPECOPT=2 6

All ALL(2)

CHAR4

Keyword ALL

Words 6 and 7 repeat until -1 occurs SPECOPT=3

Thru range

6

ID1

I

Starting identification number

7

THRU(2)

CHAR4

Keyword THRU

9

ID2

I

Ending identification number

Words 6 through 9 repeat until -1 occurs SPECOPT=4

Thru range with by

6

ID1

I

Starting identification number

7

THRU(2)

CHAR4

Keyword THRU

9

ID2

I

Ending identification number

10

BY(2)

CHAR4

Keyword BY

12

N

I

Increment

Words 6 through 12 repeat until -1 occurs

RECORD – PAABSF(1502,15,36) Defines the properties of a frequency-dependent acoustic absorber Word

Name

Type

Description

1

PID

I

Property identification number

2

TZREID

I

TABLEDi entry identification number for resistance

3-210

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

3

TZMID

I

TABLEDi entry identification number for reactance

4

S

RS

Impedance scale factor

5

A

RS

Area factor when only 1 or 2 grid points are specified

6

B

RS

Equivalent structural damping

7

K

RS

Equivalent stiffness

8

RHOC

RS

Constant used for absorption coefficient

RECORD – PACABS(8300,83,382) Defines the properties of the acoustic absorber element Name

Word

Type

Description

1

PID

I

Property identification number

2

SYNTH

I

Request the calculation of B, K, and M

3

TID1

I

TABLEDi entry identification number for resistance

4

TID2

I

TABLEDi entry identification number for reactance

5

TID3

I

TABLEDi entry identification number for weighting function

6

TESTAR

RS

Area of the test specimen

7

CUTFR

RS

Cutoff frequency for tables referenced above

8

B

RS

Equivalent structural damping values

9

K

RS

Equivalent structural stiffness

10

M

RS

Equivalent mass

RECORD – PACBAR(8500,85,384) Acoustic barrier element. Word 1

Name PID

Type I

Description Property identification number

DMAP Programmer’s Guide

3-211

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

2

MBACK

RS

Mass per unit area of the backing material

3

MSEPTM

RS

Mass per unit area of the septum material

4

FRESON

RS

Resonant frequency of the sandwich construction

5

KRESON

RS

Resonant stiffness of the sandwich construction

RECORD – PBAR(52,20,181) Simple beam element. Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

I1

RS

Area moment of inertia in plane 1

5

I2

RS

Area moment of inertia in plane 2

6

J

RS

Torsional constant

7

NSM

RS

Nonstructural mass per unit length

8

FE

RS

9

C1

RS

Stress recovery location at point C in element y-axis

10

C2

RS

Stress recovery location at point C in element z-axis

11

D1

RS

Stress recovery location at point D in element y-axis

12

D2

RS

Stress recovery location at point D in element z-axis

13

E1

RS

Stress recovery location at point E in element y-axis

14

E2

RS

Stress recovery location at point E in element z-axis

15

F1

RS

Stress recovery location at point F in element y-axis

3-212

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

16

F2

RS

Stress recovery location at point F in element z-axis

17

K1

RS

Area factor for shear in plane 1

18

K2

RS

Area factor for shear in plane 2

19

I12

RS

Area product of inertia for plane 1 and 2

RECORD – PBARL(9102,91,52) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

GROUP(2)

CHAR4

Cross-section group name

5

TYPE(2)

CHAR4

Cross section type

7

VALUE

RS

Cross-section dimensions and NSM

Word 7 repeats until End of Record

RECORD – PBCOMP(5403,55,349) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

I1

RS

Area moment of inertia in plane 1

5

I2

RS

Area moment of inertia in plane 2

6

I12

RS

Area product of inertia for plane 1 and 2

7

J

RS

Torsional constant

8

NSM

RS

Nonstructural mass per unit length

9

K1

RS

Area factor for shear in plane 1

10

K2

RS

Area factor for shear in plane 2

DMAP Programmer’s Guide

3-213

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

11

M1

RS

Location center of gravity of nonstructural mass along y-axis

12

M2

RS

Location center of gravity of nonstructural mass along y-axis

13

N1

RS

Location neutral axis along element’s y-axis

14

N2

RS

Location neutral axis along element’s y-axis

15

NSECT(C)

I

Number of lumped areas

Name

Word

Type

Description

NSECT =0 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

UNDEF(3 )

None

Words 16 through 20 repeat 4 times Name

Word

Type

Description

NSECT =1 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =2 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

3-214

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

19

MID

I

20

UNDEF

None

Description Material identification number

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =3 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =4 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =5 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

DMAP Programmer’s Guide

3-215

Data Block Descriptions A-E

Chapter 3

Name

Word 20

UNDEF

Type

Description

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =6 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =7 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =8 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

3-216

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =9 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =10 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =11 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times

DMAP Programmer’s Guide

3-217

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

NSECT =12 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =13 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =14 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Word

Name

NSECT =15

3-218

DMAP Programmer’s Guide

Type

Description

Data Block Descriptions A-E

Name

Word

Type

Description

16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =16 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =17 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =18 16

Y

RS

Lumped area location along element’s y-axis

DMAP Programmer’s Guide

3-219

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =19 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times Name

Word

Type

Description

NSECT =20 16

Y

RS

Lumped area location along element’s y-axis

17

Z

RS

Lumped area location along element’s z-axis

18

C

RS

Fraction of the total area for the lumped area

19

MID

I

Material identification number

20

UNDEF

None

Words 16 through 20 repeat NSECT times End NSECT

RECORD – PBEAM(5402,54,262) Word

Name

1

PID

3-220

DMAP Programmer’s Guide

Type I

Description Property identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

MID

I

Material identification number

3

NSEGS

I

Number of segments*

4

CCF

I

Constant cross-section flag: 1=yes and 0=no

5

X

RS

6

SO

RS

Stress output request

7

XXB

RS

Distance ratio from end A

8

A

RS

Area

9

I1

RS

Area moment of inertia in plane 1

10

I2

RS

Area moment of inertia in plane 2

11

I12

RS

Area product of inertia for plane 1 and 2

12

J

RS

Torsional constant

13

NSM

RS

Nonstructural mass per unit length

14

C1

RS

Stress recovery location at point C in element y-axis

15

C2

RS

Stress recovery location at point C in element z-axis

16

D1

RS

Stress recovery location at point D in element y-axis

17

D2

RS

Stress recovery location at point D in element z-axis

18

E1

RS

Stress recovery location at point E in element y-axis

19

E2

RS

Stress recovery location at point E in element z-axis

20

F1

RS

Stress recovery location at point F in element y-axis

21

F2

RS

Stress recovery location at point F in element z-axis

Words 6 through 21 repeat 11 times 22

K1

RS

Area factor for shear in plane 1

DMAP Programmer’s Guide

3-221

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

23

K2

RS

Area factor for shear in plane 2

24

S1

RS

Shear relief coefficient due to taper for plane 1

25

S2

RS

Shear relief coefficient due to taper for plane 1

26

NSIA

RS

Nonstructural mass moment of inertia per unit length at end A

27

NSIB

RS

Nonstructural mass moment of inertia per unit length at end B

28

CWA

RS

Warping coefficient for end A

29

CWB

RS

Warping coefficient for end B

30

M1A

RS

Location of C.G. of nonstructural mass at end A along y-axis

31

M2A

RS

Location of C.G. of nonstructural mass at end A along z-axis

32

M1B

RS

Location of C.G. of nonstructural mass at end B along y-axis

33

M2B

RS

Location of C.G. of nonstructural mass at end B along z-axis

34

N1A

RS

Location of neutral axis at end A along element’s y-axis

35

N2A

RS

Location of neutral axis at end A along element’s z-axis

36

N1B

RS

Location of neutral axis at end B along element’s y-axis

37

N2B

RS

Location of neutral axis at end B along element’s z-axis

RECORD – PBEAML(9202,92,53) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

GROUP(2)

CHAR4

Cross-section group name

3-222

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

5

TYPE(2)

CHAR4

Cross section type

7

VALUE

RS

Cross section values for XXB, SO, NSM, and dimensions

Word 7 repeats until (–1) occurs

RECORD – PBEND(2502,25,248) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

I1

RS

Area moment of inertia in plane 1

5

I2

RS

Area moment of inertia in plane 2

6

J

RS

Torsional constant

7

FSI

I

Flexibility and stress intensification factors

8

RM

RS

Mean cross-sectional radius of the curved pipe

9

T

RS

Wall thickness of the curved pipe

10

P

RS

Internal pressure

11

RB

RS

Bend radius of the line of centroids

12

THETAB

RS

Arc angle of element

13

C1

RS

Stress recovery location at point C in element y-axis

14

C2

RS

Stress recovery location at point C in element z-axis

15

D1

RS

Stress recovery location at point D in element y-axis

16

D2

RS

Stress recovery location at point D in element z-axis

17

E1

RS

Stress recovery location at point E in element y-axis

DMAP Programmer’s Guide

3-223

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

18

E2

RS

Stress recovery location at point E in element z-axis

19

F1

RS

Stress recovery location at point F in element y-axis

20

F2

RS

Stress recovery location at point F in element z-axis

21

K1

RS

Area factor for shear in plane 1

22

K2

RS

Area factor for shear in plane 2

23

NSM

RS

Nonstructural mass per unit length

24

RC

RS

Radial offset of the geometric centroid

25

ZC

RS

Offset of the geometric centroid

26

DELTAN

RS

Radial offset of the neutral axis from the geometric centroid

RECORD – PBUSH(1402,14,37) Name

Word

Type

Description

1

PID

I

Property identification number

2

K(6)

RS

Nominal stiffness values

8

B(6)

RS

Nominal damping coefficient

14

GE

RS

Nominal structural damping constant

15

SA

RS

Stress recovery coefficient in the translational component

16

ST

RS

Stress recovery coefficient in the rotational component

17

EA

RS

Strain recovery coefficient in the translational component

18

ET

RS

Strain recovery coefficient in the rotational component

3-224

DMAP Programmer’s Guide

Data Block Descriptions A-E

RECORD – PBUSH1D(3101,31,219) Name

Word

Type

Description

1

PID

I

Property identification number

2

K

RS

Stiffness

3

C

RS

Viscous Damping

4

M

RS

Mass

5

ALPHA

RS

Temperature coefficient

6

SA

RS

Stress recovery coefficient

7

EA

RS

Strain recovery coefficient

8

TYPEA

I

Shock data type: 0=Null, 1=Table, 2=Equation

9

CVT

RS

Coefficient of translation velocity tension

10

CVC

RS

Coefficient of translation velocity compression

11

EXPVT

RS

Exponent of velocity tension

12

EXPVC

RS

Exponent of velocity compression

13

IDTSU

I

TABLEDi or DEQATN entry identification number for scale factor vs displacement

14

IDTCU

I

DEQATN entry identification number for scale factor vs displacement

15

IDTSUD

I

DEQATN entry identification number for derivative tension

16

IDCSUD

I

DEQATN entry identification number for derivative compression

17

TYPES

I

Spring data type: 0=Null, 1=Table, 2=Equation

18

IDTS

I

TABLEDi or DEQATN entry identification number for tension compression

19

IDCS

I

DEQATN entry identification number for compression

20

IDTDU

I

DEQATN entry identification number for scale factor vs displacement

21

IDCDU

I

DEQATN entry identification number for force vs displacement

DMAP Programmer’s Guide

3-225

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

Description

22

TYPED

I

Damper data type: 0=Null, 1=Table, 2=Equation

23

IDTD

I

TABLEDi or DEQATN entry identification number for tension compression

24

IDTD

I

DEQATN entry identification number for compression

25

IDTDV

I

DEQATN entry identification number for scale factor versus velocity

26

IDCDV

I

DEQATN entry identification number for force versus velocity

27

TYPEG

I

General data type: 0=Null, 1=Table, 2=Equation

28

IDTG

I

TABLEDi or DEQATN entry identification number for tension compression

29

IDCG

I

DEQATN entry identification number for compression

30

IDTDU

I

DEQATN entry identification number for scale factor versus displacement

31

IDCDU

I

DEQATN entry identification number for force versus displacement

32

IDTDV

I

DEQATN entry identification number for scale factor versus velocity

33

IDCDV

I

DEQATN entry identification number for force vs velocity

34

TYPEF

I

Fuse data type: 0=Null, 1=Table

35

IDTF

I

TABLEDi entry identification number for tension

36

IDCF

I

TABLEDi entry identification number for compression

37

UT

RS

Ultimate tension

38

UC

RS

Ultimate compression

RECORD – PBUSHT(702,7,38) Name

Word 1

3-226

PID

DMAP Programmer’s Guide

Type I

Description Property identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

TKID(6)

I

TABLEDi entry identification numbers for stiffness

8

TBID(6)

I

TABLEDi entry identification numbers for viscous damping

14

TGEID

I

TABLEDi entry identification number for structural damping

15

TKNID(6)

I

TABLEDi entry IDs for force versus deflection

RECORD – PCOMP(2706,27,287) Name

Word

Type

Description

1

PID

I

Property identification number

2

N(C)

I

Number of plies

3

Z0

RS

Distance from the reference plane to the bottom surface

4

NSM

RS

Nonstructural mass per unit area

5

SB

RS

Allowable shear stress of the bonding material

6

FT

I

Failure theory

7

TREF

RS

Reference temperature

8

GE

RS

Damping coefficient

9

MID

I

Material identification number

10

T

RS

Thicknesses of the ply

11

THETA

RS

Orientation angle of the longitudinal direction of the ply

12

SOUT

I

Stress or strain output request of the ply

Words 9 through 12 repeat N times

RECORD – PCOMPG(15006,150,604) Word 1

Name PID

Type I

Description Property identification number

DMAP Programmer’s Guide

3-227

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

2

LAMOPT

I

Laminate option

3

Z0

RS

Distance from the reference plane to the bottom surface

4

NSM

RS

Nonstructural mass per unit area

5

SB

RS

Allowable shear stress of the bonding material

6

FT

I

Failure theory

7

TREF

RS

Reference temperature

8

GE

RS

Damping coefficient

9

GPLYIDi

I

Global ply IDs.

10

MID

I

Material identification number

11

T

RS

Thicknesses of the ply

12

THETA

RS

Orientation angle of the longitudinal direction of the ply

13

SOUT

I

Stress or strain output request of the ply

Words 9 through 13 repeat N times

RECORD – PCONEAX(152,19,147) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID1

I

Material identification number for membrane

3

T1

RS

Membrane thickness

4

MID2

I

Material identification number for bending

5

I

RS

Moment of inertia per unit width

6

MID3

I

Material identification number for transverse shear

7

T2

RS

Transverse shear thickness

8

NSM

RS

Nonstructural mass per unit area

3-228

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

9

Z1

RS

Fiber distance 1 from the middle surface for stress recovery

10

Z2

RS

Fiber distance 2 from the middle surface for stress recovery

11

PHI

RS

Azimuthal angle for stress recovery

Word 11 repeats 14 times

RECORD – PCONV(11001,110,411) Word

Name

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

FORM

I

Type of formula used for free convection

4

EXPF

RS

Free convection exponent

RECORD – PCONVM(2902,29,420) Word

Name

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

FORM

I

Type of formula used for free convection

4

FLAG

I

Flag for mass flow convection

5

COEF

RS

Constant coefficient used for forced convection

6

EXPR

RS

Reynolds number convection exponent

7

EXPPI

RS

Prandtl number convection exponent into the working fluid

8

EXPPO

RS

Prandtl number convection exponent out of the working fluid

DMAP Programmer’s Guide

3-229

Data Block Descriptions A-E

Chapter 3

RECORD – PDAMP(202,2,45) Name

Word

Type

Description

1

PID

I

Property identification number

2

B

RS

Force per unit velocity

RECORD – PDAMPT(1202,12,33) Name

Word

Type

Description

1

PID

I

Property identification number

2

TBID

I

TABLEDi entry identification number for viscous damping

RECORD – PDAMP5(8702,87,412) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

B

RS

Damping multiplier

RECORD – PDUM1(6102,61,116) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM2(6202,62,117) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM3(6302,63,118) Word 1

3-230

Name UNDEF

DMAP Programmer’s Guide

Type None

Description

Data Block Descriptions A-E

Word

Name

Type

Description

Word 1 repeats until End of Record

RECORD – PDUM4(6402,64,159) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM5(6502,65,160) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM6(6602,66,161) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM7(6702,67,163) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – PDUM8(6802,68,164) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

DMAP Programmer’s Guide

3-231

Data Block Descriptions A-E

Chapter 3

RECORD – PDUM9(6902,69,165) Name

Word 1

Type

UNDEF

Description

None

Word 1 repeats until End of Record

RECORD – PELAS(302,3,46) Name

Word

Type

Description

1

PID

I

Property identification number

2

K

RS

Elastic property value

3

GE

RS

Damping coefficient

4

S

RS

Stress coefficient

RECORD – PELAST(1302,13,34) Name

Word

Type

Description

1

PID

I

Property identification number

2

TKID

I

TABLEDi entry identification number for stiffness

3

TGEID

I

TABLEDi entry identification number for structural damping

4

TKNID

I

TABLEDi entry identification number for force vs. deflection

RECORD – PFAST(3601,36,55) Name

Word

Type

Description

1

PID

I

Property identification number

2

D

RS

Diameter of the spot weld

3

MCID

I

Element stiffness coordinate system

4

MFLAG

I

Defines MCID as absolute or relative

5-7

KT(3)

RS

Translational stiffness

8-10

KR(3)

RS

Rotational stiffness

3-232

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

11

MASS

RS

Lumped mass

12

GE

RS

Structural damping

RECORD – PGAP(2102,21,121) Name

Word

Type

Description

1

PID

I

Property identification number

2

UO

RS

Initial gap opening

3

FO

RS

Preload

4

KA

RS

Axial stiffness for the closed gap

5

KB

RS

Axial stiffness for the open gap

6

KT

RS

Transverse stiffness when the gap is closed

7

MU1

RS

Coefficient of static friction

8

MU2

RS

Coefficient of kinetic friction

9

TMAX

RS

Maximum allowable penetration

10

MAR

RS

Maximum allowable adjustment ratio

11

TRMIN

RS

Fraction of TMAX for the lower bound of penetration

RECORD – PHBDY(2802,28,236) Word

Name

Type

Description

1

PID

I

Property identification number

2

AF

RS

Area factor of the surface

3

D1

RS

Diameter 1 associated with the surface

4

D2

RS

Diameter 1 associated with the surface

RECORD – PINTC(12001,120,480) Word 1

Name PID

Type I

Description Property identification number

DMAP Programmer’s Guide

3-233

Data Block Descriptions A-E

Chapter 3

Name

Word

Type

Description

2

TOL

RS

Tolerance between interface elements and subdomain boundaries

3

DSCALE

RS

Scaling parameter for Lagrange multiplier functions

4

UNDEF(5 )

None

RECORD – PINTS(12101,121,484) Name

Word

Type

Description

1

PID

I

Property identification number

2

TOL

RS

Tolerance between interface elements and subdomain boundaries

3

DSCALE

RS

Scaling parameter for Lagrange multiplier functions

4

UNDEF(5 )

None

RECORD – PLPLANE(4606,46,375) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

CID

I

Coordinate system identification number

4

STR

CHAR4

Location of stress and strain output

5

T

RS

Default membrane thickness for Ti on the connection entry

6

UNDEF(6)

None

RECORD – PLSOLID(4706,47,376) Word

Name

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

STR

CHAR4

Location of stress and strain output

3-234

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word 4

Type

Description

None

UNDEF(4 )

RECORD – PMASS(402,4,44) Name

Word

Type

Description

1

PID

I

Property identification number

2

M

RS

Mass

RECORD – PPLANE(3801,38,979) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

T

RS

Default membrane thickness for Ti on the connection entry

4

NSM

RS

Nonstructural mass per unit area

5

FOROPT

I

Formulation option number

6

UNDEF(3)

None

RECORD – PROD(902,9,29) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

A

RS

Area

4

J

RS

Torsional constant

5

C

RS

Coefficient to determine torsional stress

6

NSM

RS

Nonstructural mass per unit length

DMAP Programmer’s Guide

3-235

Data Block Descriptions A-E

Chapter 3

RECORD – PSHEAR(1002,10,42) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

T

RS

Thickness o

4

NSM

RS

Nonstructural mass per unit area.

5

F1

RS

Effectiveness factor for stiffness along edges 1-2 and 3-4

6

F2

RS

Effectiveness factor for stiffness along edges 2-3 and 1-4

RECORD – PSHELL(2302,23,283) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID1

I

Material identification number for the membrane

3

T

RS

Default membrane thickness for Ti on the connection entry

4

MID2

I

Material identification number for bending

5

BK

RS

Bending moment of inertia ratio

6

MID3

I

Material identification number for transverse shear

7

TS

RS

Transverse shear thickness ratio

8

NSM

RS

Nonstructural mass per unit area

9

Z1

RS

Fiber distance 1 for stress calculation

10

Z2

RS

Fiber distance 1 for stress calculation

11

MID4

I

Material identification number for membrane-bending coupling

RECORD – PSOLID(2402,24,281) Word 1

3-236

Name PID

DMAP Programmer’s Guide

Type I

Description Property identification number

Data Block Descriptions A-E

Name

Word

Type

Description

2

MID

I

Material identification number

3

CORDM

I

Material coordinate system identification number

4

IN

I

Integration network

5

STRESS

I

Location selection for stress output

6

ISOP

I

Integration scheme

7

FCTN

CHAR4

Fluid element flag

RECORD – PSOLIDL(7602,76,370) Name

Word

Type

1

PID

I

2

FT

I

3

TREF

RS

4

GE

RS

5

NSM

RS

6

NLAY

I

7

MID

I

8

T1

RS

9

THETA

RS

10

SOUT

I

Description Property identification number

Material identification number

Words 7 through 10 repeat 40 times

RECORD – PTRIA6(6202,62,117) Word

Name

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

REAL(4)

RS

DMAP Programmer’s Guide

3-237

Data Block Descriptions A-E

Chapter 3

RECORD – PTUBE(1602,16,30) This record is slightly unstructured: OD2 is only written out if heat transfer Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material identification number

3

OD

RS

Outside diameter of tube

4

T

RS

Thickness of tube

5

NSM

RS

Nonstructural mass per unit length

6

OD2

RS

Heat transfer only: Outside diameter of tube

RECORD – PSET(10301,103,399) Name

Word

Type

Description

1

ID

I

p-value set identification number

2

POLY1

I

Polynomial order in 1 direction of the CID system

3

POLY2

I

Polynomial order in 2 direction of the CID system

4

POLY3

I

Polynomial order in 2 direction of the CID system

5

CID

I

Coordinate system identification number

6

TYPE

CHAR4

Type of set provided: "SET" or "ELID"

7

TYPEID

I

SET identification number or element identification number with this p-value specification.

Words 1 through 7 repeat until End of Record

RECORD – PVAL(10201,102,400) Name

Word

Type

Description

1

ID

I

p-value set identification number

2

POLY1

I

Polynomial order in 1 direction of the CID system

3

POLY2

I

Polynomial order in 2 direction of the CID system

4

POLY3

I

Polynomial order in 2 direction of the CID system

3-238

DMAP Programmer’s Guide

Data Block Descriptions A-E

Name

Word

Type

Description

5

CID

I

Coordinate system identification number

6

TYPE

CHAR4

Type of set provided: "SET" or "ELID"

7

TYPEID

I

SET identification number or element identification number with this p-value specification.

Words 1 through 7 repeat until End of Record

RECORD – PVISC(1802,18,31) Name

Word

Type

Description

1

PID

I

Property identification number

2

CE

RS

Viscous damping for extension

3

CR

RS

Viscous damping for rotation

RECORD – PWELD(11801,118,560) Name

Word

Type

Description

1

PID

I

Property identification number

2

MID

I

Material property identification number

3

D

RS

Diameter of the spot weld

4

CONNBEH

I

Connection behavior (0=FF/F, 1=FR, 10=RF/R, 11=RR)

5

CONNTYPE

I

Connection type (0=clamp, 1=hinge, 2=bolt)

6

EXTCON

I

External constraint flag (0=off, 1=on)

7

CONDTYPE

I

Condition type (0=rigid, 1=equivalent)

8

WELDTYPE

I

Weld type (0=spot weld, 1=but seam, 2=T-seam)

9

MINLEN

RS

Minimum length of spot weld

10

MAXLEN

RS

Maximum length of spot weld

11

GMCHK

I

Perform geometry check

12

SPCGS

I

SPC the master grid GS

DMAP Programmer’s Guide

3-239

Chapter 3

Data Block Descriptions A-E

Name

Word

Type

13

CMASS

RS

14

UNDEF(1)

None

Description Concentrated mass

RECORD – VIEW(2606,26,289) Name

Word

Type

Description

1

IVIEW

I

View identification number

2

ICAVITY

I

Cavity identification number

3

SHADE

I

Shadowing flag for the face of CHBDYi element

4

NB

I

Subelement mesh size in the beta direction

5

NG

I

Subelement mesh size in the gamma direction

6

DISLIN

RS

Displacement of a surface perpendicular to the surface

RECORD – VIEW3D(3002,30,415) Word

Name

Type

Description

1

ICAVITY

I

Radiant cavity identification number

2

GITB

I

Gaussian integration order for third-body shadowing

3

GIPS

I

Gaussian integration order for self-shadowing

4

CIER

I

Discretization level

5

ETOL

RS

Error estimate

6

ZTOL

RS

Zero tolerance

7

WTOL

RS

Warpage tolerance

8

RADCHK

I

Radiation exchange diagnostic output level

TRAILER Word 1

3-240

Name BIT(6)

DMAP Programmer’s Guide

Type I

Description Record presence trailer words

Data Block Descriptions A-E

Notes: 1. EPT705 is the same as EPT except that: •

SACL, ALPHA, FLANGE, KX, KY, KZ, undefined word 33, SY, and SZ are stripped from RECORD - PBEND. The record size is reduced from 35 words to 26 words.

•

Five GE entries are stripped from RECORD - PBUSH. The record size is reduced from 23 words to 18 words.

•

Five TGEID entries are stripped from RECORD - PBUSHT. The record size is reduced from 20 words to 15 words.

RECORD – PCOMPS(16006,160,903) Defines the properties of an n-ply composite material laminate for solid elements. Name

Word

Type

Description

1

PID

I

Property identification number

2

CORDM

I

Material coordinate system identification number

3

PSDIR

I

Stack and ply directions in the material coordinate system

4

SB

RS

Allowable shear stress of the bonding material

5

NB

RS

Allowable normal stress of the bonding material

6

TREF

RS

Reference temperature

7

GE

RS

Damping coefficient

8

UNDEF

None

9

GPLYIDi

I

Global ply identification number

10

MID

I

Material identification number

11

TR

RS

Thicknesses of the ply

12

THETA

RS

Orientation angle of the longitudinal direction of the ply

13

FT

I

Failure theory

14

ILFT

I

Inter-laminar failure theory

15

SOUT

I

Stress or strain output request of the ply

16

TFLAG

I

Flag of ‘ABS’ or ‘REL’

Words 9 through 16 repeat until (-1,-1,-1,-1,-1,-1,-1,-1) occurs

DMAP Programmer’s Guide

3-241

Data Block Descriptions A-E

Chapter 3

RECORD – MATCID(17006,170,901) Defines material coordinate system for solid elements. Name

Word

Type

Description

1

CID

I

Material coordinate system identification number

2

SPECOPT

I

Specification option

SPECOPT=1 3

Select individual element identification numbers EID

I

Element identification number

Word 3 repeats until -1 occurs SPECOPT=2 3

Select all element identification numbers ALL(2)

CHAR4

Keyword for selecting ‘ALL’ option

Words 3 repeats until -1 occurs SPECOPT=3

Select element identification numbers using a ‘THRU’ range without the ‘BY’ option

3

EID

I

Element identification number

4

THRU(2)

CHAR4

Keyword for selecting ‘THRU’ option

6

EID

I

Element identification number

Words 3 through 5 repeat until -1 occurs SPECOPT=4

Select element identification numbers using a ‘THRU’ range with the ‘BY’ option

3

EID

I

Element identification number

4

THRU(2)

CHAR4

Keyword for selecting ‘THRU’ option

6

EID

I

Element identification number

7

BY(2)

CHAR4

Keyword for selecting ‘BY’ option

9

N

I

Element selection increment

Words 3 through 9 repeat until -1 occurs

3.27 EQEXIN Equivalence between external and internal grid/scalar numbers

3-242

DMAP Programmer’s Guide

Data Block Descriptions A-E

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – EXT2INT Contains pairs of external grid and scalar identification numbers and internal numbers in external sort. Name

Word

Type

Description

1

GRIDID

I

External grid or scalar identification number

2

INTID

I

Internal identification number

Record 2 – EXT2SIL Contains pairs of external grid and scalar numbers and coded SIL numbers in external sort. Name

Word

Type

Description

1

GRIDID

I

External grid or scalar identification number

2

TENXSIL

I

10*SIL number + code (See Note)

Record 3 – TRAILER Name

Word

Type

1

NGS

I

2

UNDEF(5 )

None

Description Total number of grid scalar points

Notes: In TENXSIL, the SIL number (scalar index value) is the degree-of-freedom counter and in this context represents the first degree-of-freedom of the grid or scalar point. Code represents the type of point: 1

for grid point

2

for scalar point

3

for extra point

For example, if there are three grid points in the model, the three SIL numbers are 1, 7, and 13 and the TENXSIL numbers are 11, 71, and 131.

DMAP Programmer’s Guide

3-243

Chapter 3

Data Block Descriptions A-E

3.28 ERROR Table of p-element error tolerances

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data Block Name

Record 1 – ERROR Name

Word

Type

Description

1

EID

I

Element identification number

2

ERRMAX

RS

Accumulated Maximum error for all subcases

3

P(3)

I

Polynomial order in x,y,z directions

6

ERRCAS

RS

Calculated error for current subcase

7

WHYCAS

I

Why an element is excluded from error analysis

8

WHYALL

I

Accumulation over all subcases of previous item

Words 1 through 8 repeat until End of Record

Record 2 – TRAILER Word

Name

Type

Description

1

NWERRN

I

Used by OFPVUI subroutine

2

ERRPRN

I

Accumulates error print requests

3

PVALDV

I

Accumulates PVAL card print/punch requests.

4

ILOOP

I

To check with current ILOOP for new adaptivity loop

5

PVALID

I

To be used as old PVAL identification number. Updated only when SEID=0

6

UNDEF

None

Notes: WHYCAS is composed of bits for internal use only. Bits include values for ERRTOL,SIGTOL,EPSTOL,ERRGRD,ERRELM

3-244

DMAP Programmer’s Guide

Data Block Descriptions A-E

3.29 EST Element Summary Table EST is a collection of data from other data blocks for all elements. The format of EST is not included in this manual, but the format of the EPT data block which contributes to EST is included. The format of EST can be viewed by opening est.ddl in a text editor: install_path\nxnr\nast\del\est.ddl.

DMAP Programmer’s Guide

3-245

Chapter

4

Data Block Descriptions F-M

•

FOL

•

GPDT

•

GEOM1

•

GPDT68

•

GEOM168

•

GPL

•

GEOM2

•

HIS

•

GEOM3

•

KDICT

•

GEOM4

•

LAMA

•

GEOM4705

•

MPT

4.1 FOL Frequency response frequency output list

Record 0 – HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

FREQ

RS

Frequency

Word 3 repeats until End of Record

Record 1 – TRAILER Word

Name

Type

Description

1

WORD1

I

Number of frequencies

2

WORD2

I

Frequency set record number

3

WORD3

I

Number of loads

4

UNDEF(3 )

None

DMAP Programmer’s Guide

4-1

Chapter 4

Data Block Descriptions F-M

4.2 GEOM1 Table of Bulk Data entry images related to geometry.

Record – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record – CORD1C(1701,17,6) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

TWO

I

Constant 2

3

ONE

I

Constant 1

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

6

G3

I

Grid point 3 identification number

Record – CORD1R(1801,18,5) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

ONE1

I

Constant 1

3

ONE2

I

Constant 1

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

6

G3

I

Grid point 3 identification number

Record – CORD1S(1901,19,7) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

THREE

I

Constant 3

4-2

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

3

ONE

I

Constant 1

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

6

G3

I

Grid point 3 identification number

Record – CORD2C(2001,20,9) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

TWO1

I

Constant 2

3

TWO2

I

Constant 2

4

RID

I

Reference coordinate system identification number

5

A1

RX

Location of A in coordinate 1 of RID

6

A2

RX

Location of A in coordinate 2 of RID

7

A3

RX

Location of A in coordinate 3 of RID

8

B1

RX

Location of B in coordinate 1 of RID

9

B2

RX

Location of B in coordinate 2 of RID

10

B3

RX

Location of B in coordinate 3 of RID

11

C1

RX

Location of C in coordinate 1 of RID

12

C2

RX

Location of C in coordinate 2 of RID

13

C3

RX

Location of C in coordinate 3 of RID

Record – CORD2R(2101,21,8) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

ONE

I

Constant 1

3

TWO

I

Constant 2

DMAP Programmer’s Guide

4-3

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

4

RID

I

Reference coordinate system identification number

5

A1

RX

Location of A in coordinate 1 of RID

6

A2

RX

Location of A in coordinate 2 of RID

7

A3

RX

Location of A in coordinate 3 of RID

8

B1

RX

Location of B in coordinate 1 of RID

9

B2

RX

Location of B in coordinate 2 of RID

10

B3

RX

Location of B in coordinate 3 of RID

11

C1

RX

Location of C in coordinate 1 of RID

12

C2

RX

Location of C in coordinate 2 of RID

13

C3

RX

Location of C in coordinate 3 of RID

Record – CORD2S(2201,22,10) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

SIXTY5

I

Constant 65 or 3?

3

EIGHT

I

Constant 8 or 2?

4

RID

I

Reference coordinate system identification number

5

A1

RX

Location of A in coordinate 1 of RID

6

A2

RX

Location of A in coordinate 2 of RID

7

A3

RX

Location of A in coordinate 3 of RID

8

B1

RX

Location of B in coordinate 1 of RID

9

B2

RX

Location of B in coordinate 2 of RID

10

B3

RX

Location of B in coordinate 3 of RID

11

C1

RX

Location of C in coordinate 1 of RID

12

C2

RX

Location of C in coordinate 2 of RID

13

C3

RX

Location of C in coordinate 3 of RID

4-4

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – CORD3G(501,5,43) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

METHOD(2)

CHAR4

Methods

4

FORM(2)

CHAR4

Forms

6

THETAID(3)

I

Identification number for DEQATN or TABLE

9

CIDREF

I

Coordinate system identification number

Record – CORD3R(14301,143,651) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

6

G3

I

Grid point 3 identification number

Record – CSUPER(2301,23,304) Name

Word

Type

Description

1

SSID

I

Coded identification number for secondary superelement

2

PSID

I

Primary superelement identification number

3

G

I

Exterior grid or scalar point identificaiton numbers

Word 3 repeats until End of Record

Record – CSUPER1(5701,57,323) This record is obsolete. Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

PSID

I

Primary superelement identification number

DMAP Programmer’s Guide

4-5

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

3

TYPE

I

,{

4

VIEW

I

,{

5

DIROPT

I

,{

6

DIRTOL

RS

,{

7

GEOMTOL

RS

,{

8

CARDID

I

,{

9

MODEL

I

,{

10

SOLID

I

,{

11

DBSET

I

,{

12

COPY

I

,{

13

DELETE

I

,{

14

GRIDLIST

I

,{

15

XX

I

xx

xx

XX =0 16

G

I

,{

17

C

I

,{

Words 16 through 17 repeat until (-1,-1,-1) occurs yy

XX =–1 End XX

Record – CSUPEXT(5501,55,297) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

G

I

Grid or scalar point IDs in the downstream superelement

Word 2 repeats until End of Record

4-6

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – CSUPUP(5801,58,324) This record is obsolete. Name

Word

Type

Description

1

SEUP1

I

,{

2

PSID

I

Primary superelement identification number

3

SEDOWN1

I

,{

4

SEUP2

I

,{

5

PSID

I

Primary superelement identification number

6

SEDOWN2

I

,{

Record – EXTRN(1627,16,463) Name

Word

Type

Description

1

GID

I

Grid point identification numbers to connect external SE

2

C

I

Component numbers

Words 1 through 2 repeat until (-1,-1) occurs

Record – FEEDGE(6101,61,388) Name

Word

Type

Description

1

EDGEID

I

Edge identification number

2

GRID1

I

Identification number of end GRID 1

3

GRID2

I

Identification number of end GRID 2

4

CID

I

Coordinate system identification number

5

GEOMIN

CHAR4

Type of referencing entry: "GMCURV" or "POINT"

6

GEOMID1

I

Identification number of a POINT or GMCURV entry

7

GEOMID2

I

Identification number of a POINT or GMCURV entry

DMAP Programmer’s Guide

4-7

Chapter 4

Data Block Descriptions F-M

Record – FEFACE(6201,62,389) Name

Word

Type

Description

1

FACEID

I

Face identification number

2

GRID1

I

Identification number of end GRID 1

3

GRID2

I

Identification number of end GRID 2

4

GRID3

I

Identification number of end GRID 3

5

GRID4

I

Identification number of end GRID 4

6

CIDBC

I

Coordinate system identification number for the constraints

7

SURFID(2)

I

Alternate method used to specify the geometry

Record – GMCORD(6401,64,402) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

ENTITY

CHAR4

Bulk Data entry used to define the coordinate system

3

ID1

I

Entity identification number 1

4

ID2

I

Entity identification number 2

Record – GMCURV(6601,66,392) Word

Name

Type

Description

1

CURVID

I

Curve identification number

2

GROUP(2)

CHAR4

Group of curves/surfaces to which this curve belongs

4

CIDIN

I

Coordinate system identification number for the geometry

5

CIDBC

I

Coordinate system identification number for the constraints

6

DATA

CHAR4

Geometry evaluator specific data

Word 6 repeats until End of Record

4-8

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – GMSURF(10101,101,394) Name

Word

Type

Description

1

ID

I

Surface Identification number

2

GROUP(2)

CHAR4

Group of curves/surfaces to which this curve belongs

4

CIDIN

I

Coordinate system identification number for the geometry

5

CIDBC

I

Coordinate system identification number for the constraints

6

DATA

CHAR4

Geometry evaluator specific data

Word 6 repeats until End of Record

Record – GRID(4501,45,1) Name

Word

Type

Description

1

ID

I

Grid point identification number

2

CP

I

Location coordinate system identification number

3

X1

RX

Location of the point in coordinate 1 of CP

4

X2

RX

Location of the point in coordinate 2 of CP

5

X3

RX

Location of the point in coordinate 3 of CP

6

CD

I

Degree-of-freedom coordinate system identification number

7

PS

I

Permanent single-point constraints

8

SEID

I

Superelement identification number

Record – POINT(6001,60,377) Name

Word

Type

Description

1

ID

I

Point identification number

2

CID

I

Coordinate system identification number

3

X1

RX

Location of the point in coordinate 1 of CID

4

X2

RX

Location of the point in coordinate 2 of CID

DMAP Programmer’s Guide

4-9

Data Block Descriptions F-M

Chapter 4

Name

Word 5

Type

X3

RX

Description Location of the point in coordinate 3 of CID

Record – SEBNDRY(1527,15,466) Name

Word

Type

Description

1

SEIDA

I

Superelement A identification number

2

SEIDB

I

Superelement B identification number

3

G

I

Boundary grid point identification number in SEIDA

Word 3 repeats until End of Record

Record – SEBULK(1427,14,465) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

TYPE

I

Superelement type

3

RSEID

I

Reference superelement identification number

4

METHOD

I

Boundary point search method: 1=automatic or 2=manual

5

TOL

RS

Location tolerance

6

LOC

I

Coincident location check option: yes=1 or no=2

7

MEDIA

I

Media format of boundary data of external SE

8

UNIT

I

FORTRAN unit number of OP2 and OP4 input of external SE

Record – SECONCT(427,4,453) Word

Name

Type

Description

1

SEIDA

I

Superelement A identification number

2

SEIDB

I

Superelement B identification number

3

TOL

RS

Location tolerance

4

LOC

I

Coincident location check option: yes=1 or no=2

4-10

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

5

UNDEF(4 )

None

9

GA

I

Grid point identification number in SEIDA

10

GB

I

Grid point identification number in SEIDB

Words 9 through 10 repeat until (-1,-1) occurs

Record – SEELT(7902,79,302) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

EID

I

Element identification number

Word 2 repeats until End of Record

Record – SEEXCLD(527,72,454) Name

Word

Type

Description

1

SEIDA

I

Superelement A identification number

2

SEIDB

I

Superelement B identification number or -1 for all

3

GA

I

Grid point identification number in SEIDA

Word 3 repeats until End of Record

Record – SELABEL(1027,10,459) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

LABEL(14)

CHAR4

Label associated with superelement SEID

Record – SELOAD(1127,11,461) Word 1

Name LID0

Type I

Description New mapped load set identification number to be used in the residual structure

DMAP Programmer’s Guide

4-11

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

SEID

I

Superelement identification number of the external superelement

3

LIDSE

I

Load set identification number in the external superelement

Record – SELOC(827,8,457) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

GA1

I

Grid point 1 identification number in SEID

3

GA2

I

Grid point 2 identification number in SEID

4

GA3

I

Grid point 3 identification number in SEID

5

GB1

I

Grid point 1 identification number in the main Bulk Data

6

GB2

I

Grid point 2 identification number in the main Bulk Data

7

GB3

I

Grid point 3 identification number in the main Bulk Data

Record – SEMPLN(927,9,458) Type

Name

Word

Description

1

SEID

I

Superelement identification number

2

MIRRTYPE

I

Mirror type

MIRRTYPE=1

Plane

3

G1

I

Grid point 1 identification number in the main Bulk Data

4

G2

I

Grid point 2 identification number in the main Bulk Data

5

G3

I

Grid point 3 identification number in the main Bulk Data

6

UNDEF(2 )

None

Not Defined

MIRRTYPE=2

4-12

DMAP Programmer’s Guide

Normal

Data Block Descriptions F-M

Type

Name

Word

Description

3

G

I

Grid point identification number in the main Bulk Data

4

CID

I

Coordinate system identification number

5

N1

RS

Normal component in direction 1 of CID

6

N2

RS

Normal component in direction 2 of CID

7

N3

RS

Normal component in direction 3 of CID

End MIRRTYPE

Record – SENQSET(1327,13,464) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

NQSET

I

Number of internally generated scalar points

Record – SEQGP(5301,53,4) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

SEQID

I

Sequenced identification number

Record – SEQSEP(5401,54,305) Name

Word

Type

Description

1

SSID

I

Secondary superelement identification number

2

PSID

I

Primary superelement identification number

3

G

I

Exterior grid or scalar point identificaiton numbers

Word 3 repeats until End of Record

Record – SESET(5601,56,296) Word 1

Name SEID

Type I

Description Superelement identification number

DMAP Programmer’s Guide

4-13

Data Block Descriptions F-M

Chapter 4

Name

Word 2

Type I

G

Description Grid or scalar point identification number

Word 2 repeats until End of Record

Record – SETREE(1227,12,462) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

SEUPI

I

Upstream superelement identification number

Word 2 repeats until End of Record

Record – SNORM(5678,71,475) Word

Name

Type

Description

1

GID

I

Grid point identification number

2

CID

I

Coordinate system identification number

3

N1

RS

Normal component in direction 1 of CID

4

N2

RS

Normal component in direction 2 of CID

5

N3

RS

Normal component in direction 3 of CID

Record – TRAILER Word 1

Name BIT(6)

Type I

Description Record presence trailer words

Notes: 1. CSUPER1 and CSUPUP records are recognized only by IFP module and are removed eventually. 2. ADUMi records are not written. Rather, the contents are coded and stored in words 45 thru 54 of the system cell common block. 3. There is no record for the GRDSET entry. Rather, the GRID record is modified accordingly. 4. When GEOM1 is an alias for GEOM1VU, view grids are appended to the GRID record. The starting view grid id is controlled by system cell 180. On the SEBULK entry, the allowable values for superelement type are:

4-14

DMAP Programmer’s Guide

Data Block Descriptions F-M

•

1=PRIMARY

•

2=COLLECTOR

•

3=IDENTICAL

•

4=REPEATED

•

5=EXTERNAL

•

6=MIRROR

4.3 GEOM2 Table of Bulk Data entries related to element connectivity. GEOM2 also contains information on scalar points. ECT is identical in format to GEOM2 except all grid and scalar point external identification numbers are replaced by internal numbers. Also, ECT does not contain SPOINT records.

RECORD – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data Block Name

RECORD – BEAMAERO(2601,26,0) Name

Word

Type

Description

1

EID

I

Box identification number

2

COMPID

I

Component number in AECOMP

3

COMPTYPE(2)

CHAR4

Component type: SLBD (slender body)

5

G(2)

I

Grid identification numbers in AEGRID defining perimeter

RECORD – CAABSF(2708,27,59) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

DMAP Programmer’s Guide

4-15

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

5

G3

I

Grid point 3 identification number

6

G4

I

Grid point 4 identification number

RECORD – CAXIF2(2108,21,224) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

GRIDF point 1 identification number

3

IDF2

I

GRIDF point 2 identification number

4

RHO

RS

Fluid density in mass units

5

B

RS

Fluid bulk modulus

6

UNDEF

None

RECORD – CAXIF3(2208,22,225) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

GRIDF point 1 identification number

3

IDF2

I

GRIDF point 2 identification number

4

IFD3

I

GRIDF point 2 identification number

5

RHO

RS

Fluid density in mass units

6

B

RS

Fluid bulk modulus

7

UNDEF

None

RECORD – CAXIF4(2308,23,226) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

GRIDF point 1 identification number

3

IDF2

I

GRIDF point 2 identification number

4-16

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

4

IFD3

I

GRIDF point 2 identification number

5

IDF4

I

GRIDF point 4 identification number

6

RHO

RS

Fluid density in mass units

7

B

RS

Fluid bulk modulus

8

UNDEF

None

RECORD – CBAR(2408,24,180) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GA

I

Grid point End A identification number

4

GB

I

Grid point End B identification number

F =0

Z

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 1

F =1

XYZ option - global cooridnate system

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 1

F =2

Grid option

5

GO

I

6

UNDEF(2 )

None

8

F

I

Grid point ID at end of orientation vector

Orientation vector flag = 2

End F

DMAP Programmer’s Guide

4-17

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

9

PA

I

Pin flags for end A

10

PB

I

Pin flags for end B

11

W1A

RS

T1 component of offset vector from GA

12

W2A

RS

T2 component of offset vector from GA

13

W3A

RS

T3 component of offset vector from GA

14

W1B

RS

T1 component of offset vector from GB

15

W2B

RS

T2 component of offset vector from GB

16

W3B

RS

T3 component of offset vector from GB

RECORD – CBARAO(4001,40,275) Name

Word

Type

Description

1

EID

I

Element identification number

2

SCALE

I

Scale of Xi values

3

X1

RS

1st intermediate station for data recovery

4

X2

RS

2nd intermediate station for data recovery

5

X3

RS

3rd intermediate station for data recovery

6

X4

RS

4th intermediate station for data recovery

7

X5

RS

5th intermediate station for data recovery

8

X6

RS

6th intermediate station for data recovery

9

UNDEF

None

RECORD – CBEAM(5408,54,261) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GA

I

Grid point End A identification number

4

GB

I

Grid point End B identification number

4-18

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

5

SA

I

Scalar or grid point End A identification number for warping

6

SB

I

Scalar or grid point End B identification number for warping

F =0

Y

7

X1

RS

T1 component of orientation vector from GA

8

X2

RS

T2 component of orientation vector from GA

9

X3

RS

T3 component of orientation vector from GA

10

F

I

Orientation vector flag = 0

F =1

XYZ option - global coordinate system

7

X1

RS

T1 component of orientation vector from GA

8

X2

RS

T2 component of orientation vector from GA

9

X3

RS

T3 component of orientation vector from GA

10

F

I

Orientation vector flag =1

F =2

Grid option

7

GO

I

8

UNDEF(2 )

None

10

F

I

Orientation vector flag = 2

11

PA

I

Pin flags for end A

12

PB

I

Pin flags for end B

13

W1A

RS

T1 component of offset vector from GA

14

W2A

RS

T2 component of offset vector from GA

15

W3A

RS

T3 component of offset vector from GA

16

W1B

RS

T1 component of offset vector from GB

17

W2B

RS

T2 component of offset vector from GB

18

W3B

RS

T3 component of offset vector from GB

Grid point ID at end of orientation vector

End F

DMAP Programmer’s Guide

4-19

Data Block Descriptions F-M

Chapter 4

RECORD – CBEAMP(11401,114,9016) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Internal indices of grid points

7

SA

I

Scalar or grid point End A identification number for warping

8

SB

I

Scalar or grid point End B identification number for warping

F =0

Z

9

X1

RS

T1 component of orientation vector from GA

10

X2

RS

T2 component of orientation vector from GA

11

X3

RS

T3 component of orientation vector from GA

12

F

I

Orientation vector flag

F =1

XYZ option - global cooridnate system

9

X1

RS

T1 component of orientation vector from GA

10

X2

RS

T2 component of orientation vector from GA

11

X3

RS

T3 component of orientation vector from GA

12

F

I

Orientation vector flag = 1

F =2

Grid option

9

GO

I

10

UNDEF(2 )

None

12

F

I

Orientation vector flag = 2

13

BIT

RS

Built In Twist

14

PA

I

Pin flags for end A

15

PB

I

Pin flags for end B

16

W1A

RS

T1 component of offset vector from GA

Grid point ID at end of orientation vector

End F

4-20

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

17

W2A

RS

T2 component of offset vector from GA

18

W3A

RS

T3 component of offset vector from GA

19

W1B

RS

T1 component of offset vector from GB

20

W2B

RS

T2 component of offset vector from GB

21

W3B

RS

T3 component of offset vector from GB

22

UNDEF(2 )

None

RECORD – CBEND(4601,46,298) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GA

I

Grid point End A identification number

4

GB

I

Grid point End B identification number

F =0

Z

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 0

F =1

XYZ option - global cooridnate system

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 1

F =2

Grid option

5

GO

I

6

UNDEF(2 )

None

8

F

I

Grid point ID at end of orientation vector

Orientation vector flag = 2

DMAP Programmer’s Guide

4-21

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

End F 9

UNDEF(4 )

None

13

GEOM

I

Element geometry option

RECORD – CBUSH(2608,26,60) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GA

I

Grid point End A identification number

4

GB

I

Grid point End B identification number

F =-1

Use Element CID below for orientation

5

UNDEF(3 )

None

8

F

I

F =0

Orientation vector flag = -1

XYZ option - Basic coordinate system - SECONVRT module

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 0

F =1

XYZ option

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 1

F =2

Grid option

5

GO

I

6

UNDEF(2 )

None

4-22

DMAP Programmer’s Guide

Grid point identification number at end of orientation vector

Data Block Descriptions F-M

Name

Word 8

Type

Description

F

I

Orientation vector flag = 2

9

CID

I

Element coordinate system identification

10

S

RS

Location of spring damper

11

OCID

I

Coordinate system for spring offset

12

S1

RS

T1 component of spring-damper offset in the OCID system

13

S2

RS

T2 component of spring-damper offset in the OCID system

14

S3

RS

T3 component of spring-damper offset in the OCID system

End F

RECORD – CBUSH1D(5608,56,218) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(2)

I

Grid point identification numbers

5

CID

I

Coordinate system identification number

6

UNDEF(3 )

None

RECORD – CCONE(2315,23,0) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

RINGA

I

Ringa + 1000000 * n

4

RINGB

I

Ringb + 100000 * n

DMAP Programmer’s Guide

4-23

Data Block Descriptions F-M

Chapter 4

RECORD – CDAMP1(201,2,69) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

5

C1

I

Component number at grid point 1

6

C2

I

Component number at grid point 2

RECORD – CDAMP2(301,3,70) Name

Word

Type

Description

1

EID

I

Element identification number

2

B

RS

Value of the scalar damper

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

5

C1

I

Component number at grid point 1

6

C2

I

Component number at grid point 2

RECORD – CDAMP3(401,4,71) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CDAMP4(501,5,72) Name

Word 1

4-24

EID

DMAP Programmer’s Guide

Type I

Description Element identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

B

RS

Value of the scalar damper

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CDAMP5(10608,106,404) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CDUM2(6208,62,108) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – CDUM3(6308,63,109) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – CDUM4(6408,64,110) Word 1

Name UNDEF

Type

Description

None

Word 1 repeats until End of Record

DMAP Programmer’s Guide

4-25

Chapter 4

Data Block Descriptions F-M

RECORD – CDUM5(6508,65,111) Name

Word 1

Type

UNDEF

Description

None

Word 1 repeats until End of Record

RECORD – CDUM6(6608,66,112) Name

Word 1

Type

UNDEF

Description

None

Word 1 repeats until End of Record

RECORD – CDUM7(6708,67,113) Name

Word 1

Type

UNDEF

Description

None

Word 1 repeats until End of Record

RECORD – CDUM8(6808,68,114) Name

Word 1

UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – CDUM9(6908,69,115) Name

Word 1

UNDEF

Type

Description

None

Word 1 repeats until End of Record

RECORD – CELAS1(601,6,73) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

4-26

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

5

C1

I

Component number at grid point 1

6

C2

I

Component number at grid point 2

RECORD – CELAS2(701,7,74) Name

Word

Type

Description

1

EID

I

Element identification number

2

K

RS

Stiffness of the scalar spring

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

5

C1

I

Component number at grid point 1

6

C2

I

Component number at grid point 2

7

GE

RS

Damping coefficient

8

S

RS

Stress coefficient

RECORD – CELAS3(801,8,75) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CELAS4(901,9,76) Name

Word

Type

Description

1

EID

I

Element identification number

2

K

RS

Stiffness of the scalar spring

DMAP Programmer’s Guide

4-27

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CFAST(13801,138,566) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GS

I

Spot weld master node identification number GS

4

FORMAT(C)

I

Connection format (9=elpat, 10=partpat)

5

GA

I

Identification number of GA

6

GB

I

Identification number of GB

7–8

UNDEF(2)

9

GUPPER(8)

I

Grid identification numbers of the upper shell

17

GLOWER(8)

I

Grid identification numbers of the lower shell

25

GUACT(32)

I

Unique set of grid IDs of the active shells in upper patch

57

GLACT(32)

I

Unique set of grid IDs of the active shells in lower patch

89

NUG

I

Number of active grids in upper patch

90

NLG

I

Number of active grids in lower patch

91

GUELE(32)

I

Grid IDs of the active shells in upper patch

123

GLELE(32)

I

Grid IDs of the active shells in lower patch

155

GHA(12)

RS

Coordinates of 4 GHA points

167

GHB(12)

RS

Coordinates of 4 GHB points

179

TAVG

RS

Average shell thickness

FORMAT=9 180

4-28

ELPAT EIDUP

DMAP Programmer’s Guide

I

Element ID of upper shell

Data Block Descriptions F-M

Name

Word 181

EIDLOW

Type I

Description Element ID of lower shell

FORMAT=PARTPAT

PARTPAT

180

PIDUP

I

Property ID of upper shell

181

PIDLOW

I

Property ID of lower shell

END FORMAT 182

TMIN

RS

Minimum shell thickness

183

XS

RS

X coordinate of spot weld location

184

YS

RS

Y coordinate of spot weld location

185

ZS

RS

Z coordinate of spot weld location

186

XGA

RS

X coordinate of point ga

187

YGA

RS

Y coordinate of point ga

188

ZGA

RS

Z coordinate of point ga

189

XGB

RS

X coordinate of point gb

190

YGB

RS

Y coordinate of point gb

191

ZGB

RS

Z coordinate of point gb

RECORD – CFLUID2(8515,85,0) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL point 1 identification number

3

IDF2

I

RINGFL point 2 identification number

4

RHO

RS

Mass density

5

B

RS

Bulk modulus

6

HARMINDX

I

Harmonic index

DMAP Programmer’s Guide

4-29

Data Block Descriptions F-M

Chapter 4

RECORD – CFLUID3(8615,86,0) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL point 1 identification number

3

IDF2

I

RINGFL point 2 identification number

4

IDF3

I

RINGFL point 3 identification number

5

RHO

RS

Mass density

6

B

RS

Bulk modulus

7

HARMINDX

I

Harmonic index

RECORD – CFLUID4(8715,87,0) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDF1

I

RINGFL point 1 identification number

3

IDF2

I

RINGFL point 2 identification number

4

IDF3

I

RINGFL point 3 identification number

5

IDF4

I

RINGFL point 4 identification number

6

RHO

RS

Mass density

7

B

RS

Bulk modulus

8

HARMINDX

I

Harmonic index

RECORD – CGAP(1908,19,104) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GA

I

Grid point End A identification number

4

GB

I

Grid point End B identification number

F =0

4-30

Z

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 0

F =1

XYZ option - global cooridnate system

5

X1

RS

T1 component of orientation vector from GA

6

X2

RS

T2 component of orientation vector from GA

7

X3

RS

T3 component of orientation vector from GA

8

F

I

Orientation vector flag = 1

F =2

Grid option

5

GO

I

6

UNDEF(2 )

None

8

F

I

Orientation vector flag = 2

CID

I

Element coordinate system identification number

Grid point ID at end of orientation vector

End F 9

RECORD – CHACAB(8100,81,381) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(20)

I

Grid point identification numbers of connection points

RECORD – CHACBR(8200,82,383) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

DMAP Programmer’s Guide

4-31

Chapter 4

Data Block Descriptions F-M

Name

Word 3

G(20)

Type I

Description Grid point identification numbers of connection points

RECORD – CHBDYE(8308,83,405) Name

Word

Type

Description

1

EID

I

Element identification number

2

EID2

I

Heat conduction element identification number

3

SIDE

I

Consistent element side identification number

4

IVIEWF

I

VIEW entry identification number for the front face

5

IVIEWB

I

VIEW entry identification number for the back face

6

RADMIDF

I

RADM entry identification number for front face

7

RADMIDB

I

RADM entry identification number for back face

RECORD – CHBDYG(10808,108,406) Name

Word

Type

Description

1

EID

I

2

UNDEF

None

3

TYPE

I

Surface type

4

IVIEWF

I

VIEW entry identification number for the front face

5

IVIEWB

I

VIEW entry identification number for the back face

6

RADMIDF

I

RADM entry identification number for front face

7

RADMIDB

I

RADM entry identification number for back face

8

UNDEF

None

4-32

DMAP Programmer’s Guide

Element identification number

Data Block Descriptions F-M

Name

Word 9

Type I

G(8)

Description Grid point identification numbers of connection points

RECORD – CHBDYP(10908,109,407) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

TYPE

I

Surface type

4

IVIEWF

I

VIEW entry identification number for the front face

5

IVIEWB

I

VIEW entry identification number for the back face

6

G1

I

Grid point 1 identification number

7

G2

I

Grid point 2 identification number

8

GO

I

Grid point ID at end of orientation vector

9

RADMIDF

I

RADM entry identification number for front face

10

RADMIDB

I

RADM entry identification number for back face

11

DISLIN

I

12

CE

I

Coordinate system for defining orientation vector

13

E1

RS

T1 components of the orientation vector in the CE system

14

E2

RS

T2 components of the orientation vector in the CE system

15

E3

RS

T3 components of the orientation vector in the CE system

RECORD – CHEXA(7308,73,253) Name

Word 1

EID

Type I

Description Element identification number

DMAP Programmer’s Guide

4-33

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

PID

I

Property identification number

3

G(20)

I

Grid point identification numbers of connection points

RECORD – CHEXA20F(16300,163,9989) Same as record CHEXA description.

RECORD – CHEXAFD(14000,140,9990) Same as record CHEXA description.

RECORD – CHEXAL(7708,77,9944) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

UNDEF

None

4

G(20)

I

Grid point identification numbers of connection points

RECORD – CHEXP(12001,120,9011) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

11

E1(24)

I

35

F(6)

I

41

B1

I

42

E2(24)

I

RECORD – CHEXPR(7409,74,9991) Same as record CHEXA description.

4-34

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CMASS1(1001,10,65) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

5

C1

I

Component number at grid point 1

6

C2

I

Component number at grid point 2

RECORD – CMASS2(1101,11,66) Type

Name

Word

Description

1

EID

I

Element identification number

2

M

RS

Scalar mass value

3

G1

I

Grid point 1 identification number

4

G2

I

Grid point 2 identification number

5

C1

I

Component number at grid point 1

6

C2

I

Component number at grid point 2

RECORD – CMASS3(1201,12,67) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CMASS4(1301,13,68) Name

Word 1

EID

Type I

Description Element identification number

DMAP Programmer’s Guide

4-35

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

M

RS

Scalar mass value

3

S1

I

Scalar point 1 identification number

4

S2

I

Scalar point 2 identification number

RECORD – CMFREE(2508,25,0) Name

Word

Type

1

EID

I

2

S

I

3

S2

I

4

Y

RS

5

N

I

Description Element identification number

RECORD – CONM1(1401,14,63) Name

Word

Type

Description

1

EID

I

Element identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

M1(1)

RS

Mass matrix term M11

5

M2(2)

RS

Mass matrix terms M21 through M22

7

M3(3)

RS

Mass matrix terms M31 through M33

10

M4(4)

RS

Mass matrix terms M41 through M44

14

M5(5)

RS

Mass matrix terms M51 through M55

19

M6(6)

RS

Mass matrix terms M61 through M66

RECORD – CONM2(1501,15,64) Name

Word 1

4-36

EID

DMAP Programmer’s Guide

Type I

Description Element identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

M

RS

Mass

5

X1

RS

T1 offset from the grid point to the center of gravity

6

X2

RS

T2 offset from the grid point to the center of gravity

7

X3

RS

T3 offset from the grid point to the center of gravity

8

I1(1)

RS

Mass moments of inertia term I11

9

I2(2)

RS

Mass moments of inertia term I21 through I22

11

I3(3)

RS

Mass moments of inertia term I31 through I33

RECORD – CONROD(1601,16,47) Name

Word

Type

Description

1

EID

I

Element identification number

2

G1

I

Grid point 1 identification number

3

G2

I

Grid point 2 identification number

4

MID

I

Material identification number

5

A

RS

Area

6

J

RS

Torsional constant

7

C

RS

Coefficient for torsional stress

8

NSM

RS

Nonstructural mass per unit length

RECORD – CONV(12701,127,408) Name

Word

Type

Description

1

EID

I

Element identification number

2

PCONID

I

Convection property identification number

DMAP Programmer’s Guide

4-37

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

3

FLMND

I

Point for film convection fluid property temperature

4

CNTRLND

I

Control point for free convection boundary condition

5

TA

I

Ambient points used for convection

Word 5 repeats 8 times

RECORD – CONVM(8908,89,422) Name

Word

Type

Description

1

EID

I

Element identification number

2

PCONID

I

Convection property identification number

3

FLMND

I

Point for film convection fluid property temperature

4

CNTMDOT

I

Control point used for controlling mass flow.

5

TA

I

Ambient points used for convection

Word 5 repeats 2 times

RECORD – CPENP(12101,121,9012) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

9

E1(18)

I

27

F(5)

I

32

B1

I

33

E2(14)

I

4-38

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CPENTA(4108,41,280) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(15)

I

Grid point identification numbers of connection points

RECORD – CPENTAL(7108,71,9943) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

UNDEF

None

4

G(15)

I

Grid point identification numbers of connection points

RECORD – CPENPR(7509,75,9992) Same as record CPENTA description.

RECORD – CPENT15F(16500,165,9987) Same as record CPENTA description.

RECORD – CPENT6FD(16000,160,9988) Same as record CPENTA description.

RECORD – CPLSTN3(1701,17,980) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

6

THETA

RS

Material property orientation angle or coordinate system ID

7

UNDEF(10)

None

DMAP Programmer’s Guide

4-39

Chapter 4

Data Block Descriptions F-M

RECORD – CPLSTN4(5701,57,981) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

7

THETA

RS

Material property orientation angle or coordinate system ID

8

UNDEF(9)

None

RECORD – CPLSTN6(5801,58,982) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

9

THETA

RS

Material property orientation angle or coordinate system ID

10

UNDEF(7)

None

RECORD – CPLSTN8(7201,72,983) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

11

THETA

RS

Material property orientation angle or coordinate system ID

12

UNDEF(5)

None

4-40

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CPLSTS3(8801,88,984) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

6

UNDEF

None

7

THETA

RS

8

UNDEF(4)

None

12

TFLAG

I

Flag signifying meaning of T(3) values

13

T(3)

RS

Membrane thickness of element at grid points

16

UNDEF

None

Material property orientation angle or coordinate system ID

RECORD – CPLSTS4(8401,84,985) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

7

THETA

RS

Material property orientation angle or coordinate system ID

8

UNDEF(4)

None

12

TFLAG

I

Flag signifying meaning of T(4) values

13

T(4)

RS

Membrane thickness of element at grid points

RECORD – CPLSTS6(1801,18,986) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

DMAP Programmer’s Guide

4-41

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

3

G(6)

I

9

UNDEF(2)

None

11

THETA

RS

Material property orientation angle or coordinate system ID

12

TFLAG

I

Flag signifying meaning of T(3) values

13

T(3)

RS

Membrane thickness of element at grid points

16

UNDEF

None

Grid point identification numbers of connection points

RECORD – CPLSTS8(3601,36,987) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

11

THETA

RS

Material property orientation angle or coordinate system ID

12

TFLAG

I

Flag signifying meaning of T(4) values

13

T(4)

RS

Membrane thickness of element at grid points

17

UNDEF(8)

None

RECORD – CPYRAM(17200,172,1000) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(13)

I

Grid point identification numbers of connection points

16

UNDEF

None

4-42

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CPYRA5FD(25700,257,9948) Same as record CPYRAM description.

RECORD – CPYRA13F(25800,258,9947) Same as record CPYRAM description.

RECORD – CPYRAMPR(7909,79,9946) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(13)

I

Grid point identification numbers of connection points

16

UNDEF

None

RECORD – CQDX4FD(17000,170,9980) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(9)

I

Grid point identification numbers of connection points

RECORD – CQDX9FD(17100,171,9979) Same as record CQDX4FD description.

RECORD – CQDX4FDN(25110,170,9951) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

4

UNDEF

DMAP Programmer’s Guide

4-43

Chapter 4

Data Block Descriptions F-M

RECORD – CQDX8FDN(25310,171,9949) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

4

UNDEF

RECORD – CQUAD(9108,91,507) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(9)

I

Grid point identification numbers of connection points

RECORD – CQUAD4(2958,51,177) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

7

THETA

RS

Material property orientation angle or coordinate system ID

8

ZOFFS

RS

Offset from the surface of grid points reference plane

9

UNDEF

None

10

TFLAG

I

Alternate thickness flag

11

T(4)

RS

Membrane thickness of element at grid points

RECORD – CQUAD4FD(13900,139,9984) Same as record CQUAD description.

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DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CQUAD8(4701,47,326) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

11

T(4)

RS

Membrane thickness of element at grid points

15

THETA

RS

Material property orientation angle or coordinate system ID

16

ZOFFS

RS

Offset from the surface of grid points reference plane

17

TFLAG

I

Alternate thickness flag

RECORD – CQUAD9FD(16400,164,9983) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(9)

I

Grid point identification numbers of connection points

RECORD – CQUADP(11101,111,9014) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(17)

I

Internal indices of connection points

20

UNDEF(7 )

None

27

INORM

I

Flag for normals

28

THETA

RS

Material property orientation angle or coordinate system ID

29

ZOFFS

RS

Offset from the surface of grid points reference plane

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4-45

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

30

UNDEF(2 )

None

32

T(4)

RS

Description

Membrane thickness of element at grid points

RECORD – CQUADR(8009,80,367) Same as record CQUAD4 description.

RECORD – CQUADX(9008,90,508) Same as record CQUAD description.

RECORD – CQUADX4(6112,61,997) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

4

THETA

RS

Material property orientation angle

RECORD – CQUADX8(6114,61,999) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

4

THETA

RS

Material property orientation angle

RECORD – CROD(3001,30,48) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(2)

I

Grid point identification numbers of connection points

4-46

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CSHEAR(3101,31,61) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

RECORD – CSLOT3(4408,44,227) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDS(3)

I

GRIDS identification numbers

5

RHO

RS

Fluid density in mass units

6

B

RS

Fluid bulk modulus

7

M

I

Number of slots in circumferential direction

8

HARMINDX

I

Harmonic index

RECORD – CSLOT4(4508,45,228) Name

Word

Type

Description

1

EID

I

Element identification number

2

IDS(4)

I

GRIDS identification numbers

6

RHO

RS

Fluid density in mass units

7

B

RS

Fluid bulk modulus

8

M

I

Number of slots in circumferential direction

9

HARMINDX

I

Harmonic index

RECORD – CTETP(12201,122,9013) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

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4-47

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

3

G(4)

I

7

E1(12)

I

19

F(4)

I

23

B1

I

24

E2(4)

I

Description Grid point identification numbers of connection points

RECORD – CTETRA(5508,55,217) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(10)

I

Grid point identification numbers of connection points

RECORD – CTETPR(7609,76,9993) Same as record CTETRA description.

RECORD – CTETR10F(16600,166,9985) Same as record CTETRA description.

RECORD – CTETR4FD(16100,161,9986) Same as record CTETRA description.

RECORD – CTRAX3FDN(25010,168,9952) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

4

UNDEF

4-48

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – CTRAX6FDN(25210,169,9950) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

4

UNDEF

RECORD – CTRIA3(5959,59,282) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

6

THETA

RS

Material property orientation angle or coordinate system identification number

7

ZOFFS

RS

Offset from the surface of grid points reference plane

8

UNDEF(2)

None

10

TFLAG

I

Alternate thickness flag

11

T(3)

RS

Membrane thickness of element at grid points

RECORD – CTRIA3FD(16200,162,9982) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

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Chapter 4

Data Block Descriptions F-M

RECORD – CTRIA6(4801,48,327) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

9

THETA

RS

Material property orientation angle or coordinate system identification number

10

ZOFFS

RS

Offset from the surface of grid points reference plane

11

T(3)

RS

Membrane thickness of element at grid points

14

TFLAG

I

Alternate thickness flag

RECORD – CTRIA6FD(16700,167,9981) Same as record CTRIA3FD description.

RECORD – CTRIAP(11301,113,9015) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(11)

I

Internal indices of grid points

14

UNDEF(3 )

None

17

THETA

RS

18

UNDEF

None

19

ZOFFS

RS

20

UNDEF(2 )

None

22

T(3)

RS

RECORD – CTRIAR(9200,92,385) Same as record CTRIA3 description.

4-50

DMAP Programmer’s Guide

Material property orientation angle or coordinate system identification number

Offset from the surface of grid points reference plane

Membrane thickness of element at grid points

Data Block Descriptions F-M

RECORD – CTRIAX(10108,101,512) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

9

UNDEF

None

RECORD – CTRIAX6(6108,61,107) Name

Word

Type

Description

1

EID

I

Element identification number

2

MID

I

Material identification number

3

G(6)

I

Grid point identification numbers of connection points

9

THETA

RS

Material property orientation angle

10

UNDEF(2 )

None

RECORD – CTRAX3(6111,61,996) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

4

THETA

RS

Material property orientation angle

RECORD – CTRAX6(6113,61,998) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

DMAP Programmer’s Guide

4-51

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

3

G(6)

I

Grid point identification numbers of connection points

4

THETA

RS

Material property orientation angle

RECORD – CTRIX3FD(16800,168,9978) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

6

UNDEF(3 )

None

RECORD – CTRIX6FD(16900,169,9977) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(6)

I

Grid point identification numbers of connection points

RECORD – CTUBE(3701,37,49) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(2)

I

Grid point identification numbers of connection points

RECORD – CVISC(3901,39,50) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

4-52

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word 3

Type I

G(2)

Description Grid point identification numbers of connection points

RECORD – CWELD(11701,117,559) Name

Word

Type

Description

1

EID

I

Element ID for FORM="ALIGN", "ELEMID" or "GRIDID"

2

PID

I

Property ID

3

GS

I

Spot weld master node ID GS

4

FORMAT(C)

I

Connection format (0 GRIDID, 1 ALIGN, 2 elemid

5

GA

I

ID of GA

6

GB

I

ID of GB

7

TYPE

I

Types of upper and lower elements for FORM="GRIDID"

8

UNDEF

None

FORMAT =0

GRIDID

9

GUPPER(8)

I

Grid identification numbers of the upper shell

17

GLOWER(8)

I

Grid identification numbers of the lower shell

FORMAT =1 9

ALIGN UNDEF(16 )

None ELEMID

FORMAT =2 9

EIDUP

I

Element identification number of the upper shell

10

EIDLOW

I

Element identification number of the lower shell

11

UNDEF(14 )

None

End FORMAT 25

TAVG

RS

Average shell thickness

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4-53

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

26

RID1

I

RBE2 ID for the rigid connection between the spot weld and the upper shell

27

RID2

I

RBE2 ID for the rigid connection between the spot weld and the lower shell

28

TMIN

RS

Minimum shell thickness

29

XS

RS

X coordinate of spot weld location

30

YS

RS

Y coordinate of spot weld location

31

ZS

RS

Z coordinate of spot weld location

RECORD – CWELDC(13501,135,564) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GS

I

Spot weld master node identification number GS

4

FORMAT(C)

I

Connection format (0=GRIDID, 1=ALIGN, 2=ELEMID, 9=ELPAT, 10=PARTPAT)

5

GA

I

Identification number of GA

6

GB

I

Identification number of GB

7

UNDEF(2)

None

9

GUPPER(8)

I

Grid identification numbers of the upper shell

17

GLOWER(8)

I

Grid identification numbers of the lower shell

25

TAVG

RS

Average shell thickness

26

RID1

I

RBE2 ID for the rigid connection between the spot weld and the upper shell

27

RID2

I

RBE2 ID for the rigid connection between the spot weld and the lower shell

28

TMIN

RS

Minimum shell thickness

29

XS

RS

X coordinate of spot weld location

30

YS

RS

Y coordinate of spot weld location

4-54

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word 31

ZS

Type RS

Description Z coordinate of spot weld location

RECORD – CWELDP(13701,137,565) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

GS

I

Spot weld master node identification number GS

4

FORMAT(C)

I

Connection format (9=elpat, 10=partpat)

5

GA

I

Identification number of GA

6

GB

I

Identification number of GB

7–8

UNDEF(2)

9

GUPPER(8)

I

Grid identification numbers of the upper shell

17

GLOWER(8)

I

Grid identification numbers of the lower shell

25

GUACT(32)

I

Unique set of grid IDs of the active shells in upper patch

57

GLACT(32)

I

Unique set of grid IDs of the active shells in lower patch

89

NUG

I

Number of active grids in upper patch

90

NLG

I

Number of active grids in lower patch

91

GUELE(32)

I

Grid IDs of the active shells in upper patch

123

GLELE(32)

I

Grid IDs of the active shells in lower patch

155

GHA(12)

RS

Coordinates of 4 GHA points

167

GHB(12)

RS

Coordinates of 4 GHB points

179

TAVG

RS

Average shell thickness

FORMAT=9

ELPAT

180

EIDUP

I

Element ID of upper shell

181

EIDLOW

I

Element ID of lower shell

DMAP Programmer’s Guide

4-55

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

FORMAT=PARTPAT

PARTPAT

180

PIDUP

I

Property ID of upper shell

181

PIDLOW

I

Property ID of lower shell

END FORMAT 182

TMIN

RS

Minimum shell thickness

183

XS

RS

X coordinate of spot weld location

184

YS

RS

Y coordinate of spot weld location

185

ZS

RS

Z coordinate of spot weld location

186

XGA

RS

X coordinate of point ga

187

YGA

RS

Y coordinate of point ga

188

ZGA

RS

Z coordinate of point ga

189

XGB

RS

X coordinate of point gb

190

YGB

RS

Y coordinate of point gb

191

ZGB

RS

Z coordinate of point gb

RECORD – This record is no longer used– CWELDG(13601,136,562) Name

Word

Type

Description

1

EID

I

Shell element identification number

2

PID

I

Property identification number

3

GS

I

Spot weld master node identification number GS

4

FORMAT(C)

I

Connection format (3=TRIA3, 4=QUAD4, 6=TRIA6, 8=QUAD8)

5

GA

I

Identification number of GA

6

GB

I

Identification number of GB

7

TYPE

I

Types of upper and lower elements for FORM="GRIDID"

8

CID

I

C

4-56

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word FORMAT =3

Type

Description

TRIA3

9

EIDSH

I

Element identification number

10

PIDSH

I

Property identification number of PSHELL

11

GIDSH(3)

I

Grid Iidentification numbers of element

14

TH

RS

MCID or THETA

15

ZOFFS

RS

ZOFFS

16

UNDEF(3 )

None

19

T(3)

RS

22

UNDEF(3 )

None

FORMAT =4

Membrane thickness

QUAD4

9

EIDSH

I

Element identification number

10

PIDSH

I

Property identification number of PSHELL

11

GIDSH(4)

I

Grid identification numbers of element

15

TH

RS

MCID or THETA

16

ZOFFS

RS

ZOFFS

17

UNDEF(2 )

None

19

T(4)

RS

23

UNDEF(2 )

None

FORMAT =6

Membrane thickness

TRIA6

9

EIDSH

I

Element identification number

10

PIDSH

I

Property identification number of PSHELL

11

GIDSH(6)

I

Grid identification numbers of element

17

TH

RS

MCID or THETA

18

ZOFFS

RS

ZOFFS

19

T(3)

RS

Membrane thickness

22

UNDEF(3 )

None

DMAP Programmer’s Guide

4-57

Data Block Descriptions F-M

Chapter 4

Name

Word FORMAT =8

Type

Description

QUAD8

9

EIDSH

I

Element identification number

10

PIDSH

I

Property identification number of PSHELL

11

GIDSH(8)

I

Grid identification numbers of element

19

T(4)

RS

Membrane thickness

23

TH

RS

MCID or THETA

24

ZOFFS

RS

ZOFFS

End FORMAT 25

EID2

I

CWELD or RBAR element identification number

26

RID1

I

R

27

RID2

I

R

RECORD – GENEL(4301,43,28) Name

Word

Type

Description

1

EID

I

Element identification number

2

UI

I

Independent grid point identification number

3

CI

I

Component number

Words 2 through 3 repeat until End of Record 4

M(C)

I

Number of rows and columns in K or Z and rows in S

5

UD

I

Dependent grid point identification number

6

CD

I

Component number

Words 5 through 6 repeat until End of Record 7

N(C)

I

Number of columns in S

8

F

I

1 => Z 2=> K

9

KZIJ

RS

Lower triangular terms of the K or Z matrix. See Notes.

4-58

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

Word 9 repeats MM times 10

NZERO(C)

NZERO =1 11

I Actually " 0"

SIJ

RS

Terms of the S matrix

Word 11 repeats M times Word 11 repeats N times NZERO =0 End NZERO 12

UNDEF

None

Word 12 repeats until End of Record

RECORD – GMBNDC(3201,32,478) Name

Word

Type

Description

1

BID

I

Boundary identification number

2

GRIDI

I

Initial grid identification number for boundary

3

GRIDF

I

Final grid identification number for boundary

4

ENTITY(2)

CHAR4

Entity type for defining boundary

6

EID

I

Entity identification numbers for boundary of subdomain

Word 6 repeats until End of Record

RECORD – GMBNDS(12901,129,482) Name

Word

Type

Description

1

BID

I

Boundary identification number

2

GRIDC(4)

I

Corner grid 1

6

ENTITY(2)

CHAR4

Entity type for defining boundary

8

EID

I

Entity identification numbers for boundary of subdomain

DMAP Programmer’s Guide

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Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

Word 8 repeats until End of Record

RECORD – GMINTC(3301,33,479) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

IBOUND(6)

I

Boundary identification number

9

UNDEF(42 )

None

RECORD – GMINTS(13001,130,483) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

IBOUND(4)

I

Boundary identification number

7

UNDEF(44 )

None

RECORD – PLOTEL(5201,52,11) Name

Word

Type

Description

1

EID

I

Element identification number

2

G(2)

I

Grid point identification numbers of connection points

RECORD – Q4AERO(3002,46,0) Name

Word

Type

Description

1

EID

I

Box identification number

2

COMPID

I

Component number in AECOMP

3

COMPTYPE(2)

CHAR4

Component type: SLBD (slender body)

5

G(4)

I

Grid identification numbers in AEGRID defining perimeter

4-60

DMAP Programmer’s Guide

Data Block Descriptions F-M

RECORD – RADBC(12801,128,417) Name

Word

Type

Description

1

EID

I

Element identification number

2

FAMB

RS

Radiation view factor between the face and the ambient point

3

CNTRLND

I

Control point for radiation boundary condition

4

NODAMB

I

RECORD – SINT(7801,78,8883) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

PTELE

I

Pointer to element identification number

4

NSEG

I

Number of segments

5

STSC

I

Stride for segment displacement data

6

PTSC

I

Pointer to segment displacements

7

NBOUND

I

Number of boundaries

8

BID

I

Boundary identification number

9

NFACE

I

Number of faces

10

STBC

I

Stride for boundary displacement data

11

NSEG

I

Number of segments

12

STLC1

I

Stride for Boundary Lagrange Multiplier data

13

PTBND

I

Pointer to boundary identification number

14

PTBC

I

Pointer to boundary displacements

15

PTLC

I

Pointer to boundary Lagrange Multipliers

Words 8 through 15 repeat 5 times 16

UNDEF(3 )

None

DMAP Programmer’s Guide

4-61

Data Block Descriptions F-M

Chapter 4

RECORD – SPOINT(5551,49,105) Word 1

Name ID

Type

Description

I

Scalar point identification number

RECORD – T3AERO(2701,27,0) Name

Word

Type

Description

1

EID

I

Box identification number

2

COMPID

I

Component number in AECOMP

3

COMPTYPE(2)

CHAR4

Component type: SLBD (slender body)

5

G(3)

I

Grid identification numbers in AEGRID defining perimeter

RECORD – VUBEAM(11601,116,9942) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(2)

I

Grid point identification numbers of connection points

RECORD – VUHEXA(12301,123,145) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(8)

I

Grid point identification numbers of connection points

RECORD – VUPENTA(12401,124,146) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

4-62

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word 3

Type I

G(6)

Description Grid point identification numbers of connection points

RECORD – VUQUAD4(11201,112,9940) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

RECORD – VUTETRA(12501,125,147) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(4)

I

Grid point identification numbers of connection points

RECORD – VUTRIA3(11501,115,9941) Name

Word

Type

Description

1

EID

I

Element identification number

2

PID

I

Property identification number

3

G(3)

I

Grid point identification numbers of connection points

RECORD – TRAILER Word 1

Name BIT(6)

Type I

Description Record presence trailer words

Notes: 1. Records appear in ascending internal element ID.

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Chapter 4

Data Block Descriptions F-M

2. When the ECT is an alias for the GEOM2VU block, the third word of the header record in: •

VUHEXA becomes 9921

•

VUPENTA becomes 9922

•

VUTETRA becomes 9923

For each of the above, the grid id is then a VIEW grid id. The beginning value of the VIEW grids is controlled by system cell 182. 3. Internal indices are: •

CQUADP: (NGRIDS + 2*NEDGES +4*NFACES + 1 Bubble Point)

•

CTRIAP: (NGRIDS+2*NEDGES+NFACES + 1BODY(for bubble)

•

CBEAMP: (NGRIDS+2*NEDGES)

4. For the BEAMAERO, Q4AERO, and T3AERO records, the component types are general labels for components: •

SLBD are Slender Body Types and are "BEAM-LIKE" Elements appearing only in the BEAMAERO Record.

•

The remaining Components Types can be QUAD or TRIA connections denoting various element types.

•

INBD are Interference Body Panels.

•

LS are Lifting Surface Panels.

•

WAKE are Wake Boxes.

•

MFLO are Flow-Thru Surfaces like Inlets (Mass-Flow).

5. In GENEL record, MM=((M*(M+1)/2)-1).

4.4 GEOM3 Table of Bulk Data entry images related to static and thermal loads

Record – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record – ACCEL(7401,74,601) Word 1

4-64

Name SID

DMAP Programmer’s Guide

Type I

Description Load set identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

CID

I

Coordinate system identification number

3

N(3)

RS

Components of a vector coordinate system defined by CID

6

DIR

CHAR1

Component direction of acceleration variation

7

LOCi

RS

Location along direction DIR in coordinate system

8

VALi

RS

The load scale factor associated with location LOCi

Words 7 through 8 repeat until (-1,-1) occurs.

Record – ACCEL1(7501,75,602) Name

Word

Type

Description

1

SID

I

Load set identification number

2

CID

I

Coordinate system identification number

3

A

RS

Acceleration vector scale factor

4

N(3)

RS

Components of a vector coordinate system defined by CID

7

GRIDID

I

Grid ID or THRU or BY code

Words 7 repeats until (-1) occurs.

Record – BOLTFOR(7002,70,254) Name

Word

Type

Description

1

SID

I

Bolt force set identification number

2

FORCE

RS

Bolt Force

3

BOLTID

I

Bolt identification number

Record – BOLTLD(7601,76,608) Name

Word

Type

Description

1

SID

I

Set identification number of BOLTLD bulk entry

2

S

RS

Overall scale factor

DMAP Programmer’s Guide

4-65

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

3

Si

RS

Scale factor on Li

4

Li

I

Set identification number of BOLTFOR bulk entries

Word 4 repeats until (-1,-1) occurs

Record – FORCE(4201,42,18) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

F

RS

Scale factor

5

N(3)

RS

Components of a vector coordinate system defined by CID

Record – FORCE1(4001,40,20) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

F

RS

Scale factor

4

G(2)

I

Grid point identification numbers

Record – FORCE2(4101,41,22) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

F

RS

Scale factor

4

G(4)

I

Grid point identification numbers

4-66

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – GMLOAD(6309,63,391) Name

Word

Type

Description

1

SID

I

Load set identification number

2

CID

I

Coordinate system identification number

3

N1

RS

Component 1 of a vector coordinate system defined by CID

4

N2

RS

Component 2 of a vector coordinate system defined by CID

5

N3

RS

Component 3 of a vector coordinate system defined by CID

6

ENTITY

CHAR4

Entity type that is being loaded

7

ENTID

I

Entity identification number

8

METHTYP

I

Method

METHTYP =1

TABLE3D

9

TABLID

I

10

UNDEF(8 )

None

METHTYP =2

DEQATN

9

EQTNID

I

10

UNDEF(8 )

None

METHTYP =3

CONSTANT

9

RS

FIELD(9)

METHTYP =4

LINEAR

9

RS

FIELD(9)

METHTYP =5

QUAD

9

RS

FIELD(9)

METHTYP =6

CUBIC

9

RS

FIELD(9)

TABLE3D identification number

DEQATN identification number

Load magnitude data

Load magnitude data

Load magnitude data

Load magnitude data

METHTYP=11 9

MTABLID

I

DMAP Programmer’s Guide

4-67

Data Block Descriptions F-M

Chapter 4

Name

Word 10

Type

Description

None

UNDEF(8)

METHTYP=12 9

MEQTNID

I

10

UNDEF(8)

None

METHTYP=13 9

RS

MCONST(9)

METHTYP=14 9

RS

MLINEAR(9)

METHTYP=15 9

RS

MQUAD(9)

METHTYP=16 9

RS

MCUBIC(9)

End METHTYP

Record – GRAV(4401,44,26) Name

Word

Type

Description

1

SID

I

Load set identification number

2

CID

I

Coordinate system identification number

3

A

RS

Acceleration vector scale factor

4

N(3)

RS

Components of a vector coordinate system defined by CID

7

MB

I

Bulk Data Section with CID definition: -1=main, 0=partitioned

Record – LOAD(4551,61,84) Name

Word

Type

Description

1

SID

I

Load set identification number

2

S

RS

Overall scale factor

4-68

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

3

SI

RS

Scale factor on LI

4

LI

I

Load set identification number

Words 3 through 4 repeat until (-1,-1) occurs

Record – LOADCYH(3709,37,331) Name

Word

Type

Description

1

SID

I

Load set identification number

2

S

RS

Scale factor

3

HID

I

Harmonic index

4

HTYPE

I

Harmonic type

5

SI

RS

Scale factor on LI

6

LI

I

Load set identification number

Words 5 through 6 repeat 2 times

Record – LOADCYN(3809,38,332) Name

Word

Type

Description

1

SID

I

Load set identification number

2

S

RS

Scale factor

3

SEGID

I

Segment identification number

4

SEGTYPE

I

Segment type

5

SI

RS

Scale factor on LI

6

LI

I

Load set identification number

Words 5 through 6 repeat 2 times

Record – LOADCYT(3909,39,333) Name

Word 1

SID

Type I

Description Load set identification number

DMAP Programmer’s Guide

4-69

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

TABLEID

I

TABLEDi identification number

3

LOADSET

I

Load set identification number

4

METHOD

I

Method of interpolation

Words 2 through 4 repeat 2 times

Record – LSEQ(3609,36,188) Name

Word

Type

Description

1

SID

I

Load set identification number

2

DAREA

I

DAREA set identification number

3

LID

I

Load set identification number

4

TID

I

Temperature set identification number

5

UNDEF

None

Record – MOMENT(4801,48,19) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

M

RS

Moment scale factor

5

N(3)

RS

Components of a vector coordinate system defined by CID

Record – MOMENT1(4601,46,21) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

M

RS

Moment scale factor

4

G(2)

I

Grid point identification numbers

4-70

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – MOMENT2(4701,47,23) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

M

RS

Moment scale factor

4

G(4)

I

Grid point identification numbers

Record – PLOAD(5101,51,24) Name

Word

Type

Description

1

SID

I

Load set identification number

2

P

RS

Pressure

3

G(4)

I

Grid point identification numbers

Record – PLOAD1(6909,69,198) Name

Word

Type

Description

1

SID

I

Load set identification number

2

EID

I

Element identification number

3

TYPE

I

Load type

4

SCALE

I

Scale factor for X1 and X2

5

X1

RS

Distance to position 1 along the element axis from end A

6

P1

RS

Pressure at position 1

7

X2

RS

Distance to position 2 along the element axis from end A

8

P2

RS

Pressure at position 2

Record – PLOAD2(6802,68,199) Word 1

Name SID

Type I

Description Load set identification number

DMAP Programmer’s Guide

4-71

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

P

RS

Pressure

3

EID

I

Element identification number

Record – PLOAD3(7109,71,255) Name

Word

Type

Description

1

SID

I

Load set identification number

2

P

RS

Pressure

3

EID

I

Element identification number

4

G(2)

I

Grid point identification numbers

Record – PLOAD4(7209,72,299) Name

Word

Type

Description

1

SID

I

Load set identification number

2

EID

I

Element identification number

3

P(4)

RS

Pressures

7

G1

I

Grid point identification number at a corner of the face

8

G34

I

Grid point ID at a diagonal from G1 or CTETRA corner

9

CID

I

Coordinate system identification number

10

N(3)

RS

Components of a vector coordinate system defined by CID

Record – PLOADE1(6701,67,978) Name

Word

Type

Description

1

SID

I

Load set identification number

2

EID

I

Element identification number

3

PA

RS

Surface traction at grid point GA

4

PB

RS

Surface traction at grid point GB

4-72

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

5

G(2)

I

Corner grid point identification numbers

7

THETA

RS

Angle between surface traction and inward normal

Record – PLOADX(7001,70,278) This record is obsolete Name

Word

Type

Description

1

SID

I

Load set identification number

2

P(2)

RS

Pressure

4

G(3)

I

Grid point identification numbers

Record – PLOADX1(7309,73,351) Name

Word

Type

Description

1

SID

I

Load set identification number

2

EID

I

Element identification number

3

PA

RS

Surface traction at grid point GA

4

PB

RS

Surface traction at grid point GB

5

G(2)

I

Corner grid point identification numbers

7

THETA

RS

Angle between surface traction and inward normal

Record – PRESAX(5215,52,154) Name

Word

Type

Description

1

SID

I

Load set identification number

2

P

RS

Pressure

3

RID(2)

I

Ring identification numbers

5

PHI1

RS

Azimuthal angles in degrees

6

UNDEF

None

DMAP Programmer’s Guide

4-73

Chapter 4

Data Block Descriptions F-M

Record – QBDY1(4509,45,239) Name

Word

Type

Description

1

SID

I

Load set identification number

2

Q0

RS

Heat flux into element

3

EID

I

Element identification number

Record – QBDY2(4909,49,240) Name

Word

Type

Description

1

SID

I

Load set identification number

2

EID

I

Element identification number

3

Q0(8)

RS

Heat flux at the i-th grid point on the referenced CHBDYj

Record – QBDY3(2109,21,414) Name

Word

Type

Description

1

SID

I

Load set identification number

2

Q0

RS

Thermal heat flux load, or load multiplier

3

CNTRLND

I

Control point for thermal flux load

4

EID

I

Element identification number

Record – QHBDY(4309,43,233) Name

Word

Type

Description

1

SID

I

Load set identification number

2

FLAG

I

Face type

3

Q0

RS

Magnitude of thermal flux into face

4

AF

RS

Area factor

5

G(8)

I

Grid point identification numbers

4-74

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – QVECT(2209,22,241) Name

Word

Type

Description

1

SID

I

Load set identification number

2

Q0

RS

Magnitude of thermal flux vector into face

3

TSOUR

RS

Temperature of the radiant source

4

CE

I

Coordinate system identification number for thermal vector flux

5

FLAG

I

6

E

RS

Vector component of flux in coordinate system CE

Words 5 through 6 repeat 3 times 7

CNTRLND

I

Control point

8

EID

I

Element identification number

Record – QVOL(2309,23,416) Name

Word

Type

Description

1

SID

I

Load set identification number

2

QVOL

RS

Power input per unit volume produced by a conduction element

3

CNTRLND

I

Control point used for controlling heat generation

4

EID

I

Element identification number

Record – RFORCE(5509,55,190) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Grid point identification number

3

CID

I

Coordinate system identification number

4

A

RS

Scale factor of the angular velocity

5

R(3)

RS

Rectangular components of rotation vector

DMAP Programmer’s Guide

4-75

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

8

METHOD

I

Method used to compute centrifugal forces

9

RACC

RS

Scale factor of the angular acceleration

10

MB

I

Bulk Data Section with CID definition: -1=main, 0=partitioned

Record – SLOAD(5401,54,25) Name

Word

Type

Description

1

SID

I

Load set identification number

2

G

I

Scalar or grid point identification number

3

F

RS

Scale factor

Record – TEMP(5701,57,27) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

G

I

Grid point identification number

3

T

RS

Temperature

Record – TEMPD(5641,65,98) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

T

RS

Temperature

Record – TEMPEST(11109,111,424) Word

Name

Type

Description

1

SID

I

Temperature set identification number

2

TEMP

RS

Temperature

3

EID

I

Element identification number

4-76

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – TEMPF(6209,62,390) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

EID

I

Element identification number

3

FTEMP

I

DEQATN identification number

4

FTABID

I

TABLE3D identification number

Record – TEMPIC(11209,112,425) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

TEMP

RS

Temperature

3

EID

I

Element identification number

Record – TEMPP1(8109,81,201) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

EID

I

Element identification number

3

T

RS

Temperature at the element’s reference plane

4

TPRIME

RS

Effective linear thermal gradient

5

TS(2)

RS

Temperatures for stress calculation

Record – TEMPP2(8209,82,202) This record is obsolete Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

EID

I

Element identification number

3

T

RS

S,{

4

MX

RS

S,{

DMAP Programmer’s Guide

4-77

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

5

MY

RS

S,{

6

MXY

RS

S,{

7

T(2)

RS

S,{

Record – TEMPP3(8309,83,203) This record is obsolete Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

EID

I

Element identification number

3

Z

RS

S,{

4

T

RS

S,{

Words 3 through 4 repeat 11 times

Record – TEMPRB(8409,84,204) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

EID

I

Element identification number

3

TA

RS

Temperature at end A on the neutral axis

4

TB

RS

Temperature at end B on the neutral axis

5

TP1A

RS

Effective linear gradient in direction 1 on end A

6

TP1B

RS

Effective linear gradient in direction 1 on end B

7

TP2A

RS

Effective linear gradient in direction 2 on end A

8

TP2B

RS

Effective linear gradient in direction 2 on end B

9

TS(8)

RS

Temperatures for stress calculation

Record – PFACE(6409,64,9032) This record is created by the GP0 module; not by the user.

4-78

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

1

SID

I

Load set identification number

2

FACEID

I

Face identification number

3

CID

I

Coordinate system identification number

4

N(3)

RS

Components of a vector coordinate system defined by CID

7

EQTNID

I

DEQATN identification number

8

TABLID

I

TABLE3D identification number

9

FIELD(9)

RS

See GMLOAD record

18

G(4)

I

Grid point identification numbers

22

GNIDA

I

Side i grid-n A identification number

23

GNIDB

I

Side i grid-n B identification number

24

PSEL

I

Computed p value

25

MAXNDF

I

Maximum number of degrees-of-freedom or stride

Words 22 through 25 repeat 4 times 26

FACFID

I

Grid-n identification number for the face

27

NDOF

I

Number of degrees-of-freedom for the face

28

LDISTFG

I

Load distribution flag

29

UNDEF(2 )

None

31

CIDF

I

Coordinate system ID of the face

32

NDOFF(4)

I

NDOF flags

Record – PEDGE(6609,66,9031) This record is created by the GP0 module; not by the user. Word

Name

Type

Description

1

SID

I

Load set identification number

2

EDGEID

I

Edge identification number

3

CID

I

Coordinate system identification number

DMAP Programmer’s Guide

4-79

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

4

N(3)

RS

Components of a vector coordinate system defined by CID

7

EQTNID

I

DEQATN identification number

8

TABLID

I

TABLE3D identification number

9

FIELD(4)

RS

See GMLOAD record

13

G(2)

I

Grid point identification numbers

15

F1ID

I

Grid-n 1 identification number

16

F2ID

I

Grid-n 2 identification number

17

PSEL

I

Computed p value

18

MAXNDF

I

Maximum number of degrees-of-freedom or stride

19

INTFL

I

1 or 2

20

UNDEF(13 )

None

33

CIDE

I

Coordinate system identification number of the edge

Record – TRAILER Name

Word 1

BIT(6)

Type I

Description Record presence trailer words

4.5 GEOM4 Table of Bulk Data entry images related to constraints. Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity.

Record – HEADER Word 1

4-80

Name NAME(2)

DMAP Programmer’s Guide

Type CHAR4

Description Data block name

Data Block Descriptions F-M

Record – ASET(5561,76,215) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – ASET1(5571,77,216) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – BNDFIX(110,1,584) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – BNDFIX1(210,2,585) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

DMAP Programmer’s Guide

4-81

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – BNDFREE(310,3,586) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – BNDFREE1(410,4,587) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – BNDGRID(10200,102,473) Word 1

4-82

Name GPI

DMAP Programmer’s Guide

Type I

Description Shape boundary grid point identification number

Data Block Descriptions F-M

Record – BSET(110,1,311) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – BSET1(210,2,312) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – CSET(310,3,313) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – CSET1(410,4,314) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

DMAP Programmer’s Guide

4-83

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – CYAX(1510,15,328) Name

Word 1

Type I

G

Description Grid point identification number on the axis of symmetry

Word 1 repeats until End of Record

Record – CYJOIN(5210,52,257) Name

Word

Type

Description

1

SIDE

I

Side identification number: 1 or 2

2

C(2)

CHAR4

Coordinate system type on symetry booundary

4

ID

I

Grid or scalar point identification number

Word 4 repeats until End of Record

Record – CYSUP(1610,16,329) Name

Word

Type

Description

1

GID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – CYSYM(1710,17,330) Word

Name

Type

Description

1

NSEG

I

Number of segments

2

STYPE(2)

CHAR4

Symmetry type

4-84

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – EGENDT(8801,88,9022) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

SPCID

I

SPC set identification number

3

EDGEID

I

Edge identification number

4

C

I

Component numbers

5

DISTFLG

I

Distribution flag

6

DISFUN

I

Distribution function (DEQATN)

7

DISTAB

I

Distribution table (TABLE3D)

8

FIELD(4)

RS

See GMBC record

Words 4 through 11 repeat 6 times 12

ELTYPE

I

Element type

13

EID

I

Element identification number

14

EORD

I

Edge order

15

EDGEID

I

Edge identification number

16

FACEID

I

Face identification number

17

CURVID

I

Curve identification number

18

SURFID

I

Surface identification number

19

G(2)

I

Grid point identification numbers

21

MIDG

I

22

POINT(2)

I

Point identification numbers

24

F1ID

I

Grid-n 1 identification number

25

F2ID

I

Grid-n 2 identification number

26

NDOF

I

I,{

27

CIDE

I

Coordinate system identification number for the edge

28

MAXNDFE

I

Maximum number of degrees-of-freedom, or stride, for the edge

DMAP Programmer’s Guide

4-85

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

29

MAXNDFB

I

Maximum number of degrees-of-freedom, or stride, for the body

30

PUSER

I

p-level specified by user

31

PSEL

I

p-level selected by program

32

BODYFID

I

Grid-n identification number for the body

33

NDOFB

I

Number of degrees-of-freedom for the body

34

F1ID

I

Grid-n 1 identification number

35

CID

I

Coordinate system identification number

36

X

RS

S,{

37

Y

RS

S,{

38

Z

RS

S,{

Words 34 through 38 repeat 7 times

Record – FCENDT(9001,90,9024) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

SID

I

Set identification number

3

FACEID

I

Face identification number

4

C

I

Component numbers

5

DISTFLG

I

Distribution flag

6

DISFUN

I

Distribution function (DEQATN)

7

DISTAB

I

Distribution table (TABLE3D)

8

FIELD(9)

RS

See GMBC record

Words 4 through 16 repeat 6 times 17

F1ID

I

Grid-n 1 identification number

18

F2ID

I

Grid-n 2 identification number

19

NDOF

I

Number of degrees-of-freedom for the face

4-86

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

20

MAXNDF

I

Maximum number of degrees-of-freedom or stride

21

CIDE

I

Coordinate system identification number of the edge

Words 17 through 21 repeat 4 times 22

FACFID

I

Grid-n identification number for the face

23

NDOF

I

Number of degrees-of-freedom for the face

24

MAXNDFF

I

Maximum number of degrees-of-freedom for the face

25

CIDF

I

Coordinate system identification number for the face

26

ELTYPE

I

Element type

27

EID

I

Element identification number

28

EORD

I

Edge order

29

FACEID

I

Face identification number

30

SURFID

I

Surface identification number

31

G(4)

I

Grid point identification numbers

35

CIDF

I

Coordinate system identification number for the face

36

MAXNDIF

I

37

UNDEF

None

38

PUSER(4)

I

p-level specified by user

42

PSEL(4)

I

p-level selected by program

46

FACFID

I

Grid-n identification number for the face

47

NDOF

I

Number of degrees-of-freedom for the face

48

F1ID

I

Grid-n 1 identification number

49

CID

I

Coordinate system identification number

50

X

RS

51

Y

RS

DMAP Programmer’s Guide

4-87

Data Block Descriptions F-M

Chapter 4

Name

Word 52

Z

Type

Description

RS

Words 48 through 52 repeat 13 times

Record – GMBC(8001,80,395) Name

Word

Type

Description

1

LID

I

Load set identification number

2

SPCID

I

SPC set identification number

3

C

I

Component number

4

ENTITY

CHAR4

Entity type that is being loaded

5

ENTID

I

Entity identification number

6

METHOD

I

Method of data specification

METHOD =1

TABLE3D

7

TABLID

I

8

UNDEF(8 )

None

METHOD =2

DEQATN

7

EQTNID

I

8

UNDEF(8 )

None

METHOD =3 7 METHOD =4

METHOD =5 FIELD(9)

RS

Enforced displacement data

RS

Enforced displacement data

CUBIC FIELD(9)

End METHOD

4-88

Enforced displacement data

QUAD

METHOD =6 7

RS LINEAR

FIELD(9)

7

DEQATN identification number

CONSTANT FIELD(9)

7

TABLE3D identification number

DMAP Programmer’s Guide

RS

Enforced displacement data

Data Block Descriptions F-M

Record – GMSPC(7801,78,393) Name

Word

Type

Description

1

ID

I

Set identification number

2

C

I

Component number

3

ENTITY

CHAR4

Entity type that is being loaded

4

ENTID

I

Entity identification number

Record – MPC(4901,49,17) Name

Word

Type

Description

1

SID

I

Set identification number

2

G

I

Grid point identification number

3

C

I

Component number

4

A

RX

Coefficient

5

GI

I

Grid point identification number

6

CI

I

Component number

7

AI

RX

Coefficient

Words 5 through 7 repeat until (-1,-1,-1) occurs

Record – MPCADD(4891,60,83) Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Set identification number

Word 2 repeats until End of Record

Record – OMIT(5001,50,15) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

DMAP Programmer’s Guide

4-89

Data Block Descriptions F-M

Chapter 4

Record – OMIT1(4951,63,92) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – QSET(510,5,315) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – QSET1(610,6,316) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

4-90

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

End THRUFLAG

Record – RBAR(6601,66,292) Word

Name

Type

Description

1

EID

I

Element identification number

2

GA

I

Grid point A identification number

3

GB

I

Grid point B identification number

4

CNA

I

Component numbers of independent degrees-of-freedom at end A

5

CNB

I

Component numbers of independent degrees-of-freedom at end B

6

CMA

I

Component numbers of dependent degrees-of-freedom at end A

7

CMB

I

Component numbers of dependent degrees-of-freedom at end B

8

ALF

RS

Coefficient of thermal expansion

Record – RBE1(6801,68,294) Word

Name

Type

Description

1

EID

I

Element identification number

2

GN

I

Grid point identification number for independent degrees-of-freedom

3

CN

I

Component numbers of independent degrees-of-freedom

Words 2 through 3 repeat until (-2,-2) occurs 4

GM

I

Grid point identification number for dependent degrees-of-freedom

5

CM

I

Component numbers of dependent degrees-of-freedom

Words 4 through 5 repeat until (-1,-1) occurs 6

ALF

RS

Coefficient of thermal expansion

DMAP Programmer’s Guide

4-91

Data Block Descriptions F-M

Chapter 4

Name

Word 7

UNDEF

Type

Description

None

Record – RBE2(6901,69,295) Name

Word

Type

Description

1

EID

I

Element identification number

2

GN

I

Grid point identification number for independent degrees-of-freedom

3

CM

I

Component numbers of dependent degrees-of-freedom

4

GM

I

Grid point identification number for dependent degrees-of-freedom

Word 4 repeats until -1 occurs 5

ALF

RS

Coefficient of thermal expansion

Record – RBE3(7101,71,187) Name

Word

Type

Description

1

EID

I

Element identification number

2

REFG

I

Reference grid point identification number

3

REFC

I

Component numbers at the reference grid point

4

WT1

RS

Weighting factor for components of motion at G

5

C

I

Component numbers

6

G

I

Grid point identification number

Word 6 repeats until -1 occurs Words 4 through 6 repeat until -2 occurs 7

GM

I

Grid point identification number for dependent degrees-of-freedom

8

CM

I

Component numbers of dependent degrees-of-freedom

Words 7 through 8 repeat until -3 occurs 9

4-92

ALF

DMAP Programmer’s Guide

RS

Coefficient of thermal expansion

Data Block Descriptions F-M

Record – RELEASE(1310,13,247) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – RROD(6501,65,291) Word

Name

Type

Description

1

EID

I

Element identification number

2

GA

I

Grid point A identification number

3

GB

I

Grid point B identification number

4

CMA

I

Component numbers of dependent degrees-of-freedom at end A

5

CMB

I

Component numbers of dependent degrees-of-freedom at end B

6

ALF

RS

Coefficient of thermal expansion

Record – RSPLINE(7001,70,186) Word

Name

Type

Description

1

EID

I

Element identification number

2

DBYL

RS

Ratio of the diameter to the sum of the segments lengths

DMAP Programmer’s Guide

4-93

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

3

G1

I

Grid point identification number

4

G2

I

Grid point identification number

5

C2

I

Components to be constrained

Words 4 through 5 repeat until (-1,-1) occurs

Record – RSSCON(7201,72,398) Name

Word

Type

Description

1

EID

I

Element identification number

2

TYPE(C)

I

Type of connectivity

TYPE =0

GRID style 1

3

GRID1

I

Grid identification number 1

4

GRID2

I

Grid identification number 2

5

GRID3

I

Grid identification number 3

6

UNDEF(3 )

None

TYPE =01

GRID style 2

3

GRID1

I

Grid identification number 1

4

GRID2

I

Grid identification number 2

5

GRID3

I

Grid identification number 3

6

GRID4

I

Grid identification number 4

7

GRID5

I

Grid identification number 5

8

GRID6

I

Grid identification number 6

TYPE =02

Edge style

3

EDGE1

I

Edge identification number 1

4

EDGE2

I

Edge identification number 2

5

EDGE3

I

Edge identification number 3

6

UNDEF(3 )

None

TYPE =03

4-94

DMAP Programmer’s Guide

Element style

Data Block Descriptions F-M

Name

Word

Type

Description

3

ELID1

I

Element identification number 1

4

ELID2

I

Element identification number 2

5

UNDEF(4 )

None

TYPE =04

CINTERF

3

CBID

I

4

SBID

I

5

CBPID

I

6

UNDEF(3)

None

End TYPE

Record – RTRPLT(6701,67,293) Name

Word

Type

Description

1

EID

I

Element identification number

2

GA

I

Grid point A identification number

3

GB

I

Grid point B identification number

4

GC

I

Grid point C identification number

5

CNA

I

Component numbers for independent degrees-of-freedom at vertex A

6

CNB

I

Component numbers for independent degrees-of-freedom at vertex B

7

CNC

I

Component numbers for independent degrees-of-freedom at vertex C

8

UNDEF

None

9

CMA

I

Component numbers for dependent degrees-of-freedom at vertex A

10

CMB

I

Component numbers for dependent degrees-of-freedom at vertex B

11

CMC

I

Component numbers for dependent degrees-of-freedom at vertex C

12

ALF

RS

Coefficient of thermal expansion

DMAP Programmer’s Guide

4-95

Data Block Descriptions F-M

Chapter 4

Record – RVDOF(9801,98,609) DOF specification for residual vector computations. Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – RVDOF1(9901,99,610) DOF specification for residual vector computations. Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru flag range

THRUFLAG = 0

No

3

I

ID

Grid or scalar point identification number

THRUFLAG = 1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – RWELD(11901,119,561) Name

Word

Type

Description

1

EID

I

Element ID

2

GA

I

Grid ID of GA

3

TYPE

I

Type of shell element

4

GI(8)

I

Grid IDs of shell element

12

GS

I

Grid ID of GS

4-96

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – SEBSET(710,7,317) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record – SEBSET1(810,8,318) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – SECSET(910,9,319) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record – SECSET1(1010,10,320) Word 1

Name SEID

Type I

Description Superelement identification number

DMAP Programmer’s Guide

4-97

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – SEQSET(1110,11,321) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record – SEQSET1(1210,12,322) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

I

4-98

ID1

DMAP Programmer’s Guide

First grid or scalar point identification number

Data Block Descriptions F-M

Name

Word 5

Type

ID2

I

Description Second grid or scalar point identification number

End THRUFLAG

Record – SESUP(1410,14,325) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record – SEUSET(1810,18,334) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

SNAME

I

Set name

3

ID

I

Grid or scalar point identification number

4

C

I

Component numbers

Record – SEUSET1(1910,19,335) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

SNAME

I

Set name

3

C

I

Component numbers

4

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

5

I

ID

Grid or scalar point identification number

Word 5 repeats until End of Record THRUFLAG=1

Yes

5

I

ID1

First grid or scalar point identification number

DMAP Programmer’s Guide

4-99

Data Block Descriptions F-M

Chapter 4

Name

Word 6

Type

ID2

I

Description Second grid or scalar point identification number

End THRUFLAG

Record – SPC(5501,55,16) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

Record – SPC1(5481,58,12) Name

Word

Type

Description

1

SID

I

Set identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – SPCADD(5491,59,13) Word

Name

1

SID

4-100

DMAP Programmer’s Guide

Type I

Description Set identification number

Data Block Descriptions F-M

Name

Word 2

Type I

S

Description Set identification number

Word 2 repeats until End of Record

Record – SPCD(5110,51,256) Name

Word

Type

Description

1

SID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

Record – SPCDE(8701,87,9021) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

EDGEID

I

Edge identification number

6

SID

I

Set identification number

Record – SPCDF(8901,89,9023) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

FACEID

I

Face identification number

6

SID

I

Set identification number

DMAP Programmer’s Guide

4-101

Data Block Descriptions F-M

Chapter 4

Record – SPCDG(9701,97,9030) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

METHOD

I

Method

5

D

RS

Enforced displacement

6

SID

I

Set identification number

Record – SPCE(9301,93,9027) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

EDGID

I

Grid or scalar point identification number

Record – SPCEB(9101,91,9025) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

EDGEID

I

Edge identification number

Record – SPCF(9401,94,9028) Name

Word 1

4-102

SID

DMAP Programmer’s Guide

Type I

Description Set identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

FACEID

I

Face identification number

Record – SPCFB(9201,92,9026) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

LOADID

I

Load set identification number

Record – SPCGB(9601,96,9029) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

METHOD

I

I,{

5

D

RS

Enforced displacement

6

SID

I

Set identification number

Record – SPCGRID(8601,86,9031) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

UNDEF(2 )

None

DMAP Programmer’s Guide

4-103

Data Block Descriptions F-M

Chapter 4

Record – SPCOFF(6110,61,343) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – SPCOFF1(6210,62,344) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record – SUPORT(5601,56,14) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record – SUPORT1(10100,101,472) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid point identification number

3

C

I

Component numbers

Words 2 through 3 repeat until (-1,-1) occurs

4-104

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – TEMPBC(11309,113,426) Name

Word

Type

Description

1

SID

I

Temperature set identification number

2

TYPE

I

Type of temperature boundary condition: STAT or TRAN

3

TEMP

RS

Temperature

4

GID

I

Grid or scalar point identification number

Record – USET(2010,20,193) Name

Word

Type

Description

1

SNAME

I

Set name

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record – USET1(2110,21,194) Name

Word

Type

Description

1

SNAME

I

Set name

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

DMAP Programmer’s Guide

4-105

Chapter 4

Data Block Descriptions F-M

Record – TRAILER Name

Word 1

BIT(6)

Type I

Description Record presence trailer words

4.6 GEOM168 Table of Bulk Data entry images related to geometry (Pre-MSC Nastran Version 69). Note See Note 6 for a listing of the differences between GEOM168 and GEOM1.

Record – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record – CORD1C(1701,17,6) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

TWO

I

Constant 2

3

ONE

I

Constant 1

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

6

G3

I

Grid point 3 identification number

Record – CORD1R(1801,18,5) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

ONE1

I

Constant 1

3

ONE2

I

Constant 1

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

4-106

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word 6

Type I

G3

Description Grid point 3 identification number

Record – CORD1S(1901,19,7) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

THREE

I

Constant 3

3

ONE

I

Constant 1

4

G1

I

Grid point 1 identification number

5

G2

I

Grid point 2 identification number

6

G3

I

Grid point 3 identification number

Record – CORD2C(2001,20,9) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

TWO1

I

Constant 2

3

TWO2

I

Constant 2

4

RID

I

Reference coordinate system identification number

5

A1

RS

Location of A in coordinate 1 of RID

6

A2

RS

Location of A in coordinate 2 of RID

7

A3

RS

Location of A in coordinate 3 of RID

8

B1

RS

Location of B in coordinate 1 of RID

9

B2

RS

Location of B in coordinate 2 of RID

10

B3

RS

Location of B in coordinate 3 of RID

11

C1

RS

Location of C in coordinate 1 of RID

12

C2

RS

Location of C in coordinate 2 of RID

13

C3

RS

Location of C in coordinate 3 of RID

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Record – CORD2R(2101,21,8) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

ONE

I

Constant 1

3

TWO

I

Constant 2

4

RID

I

Reference coordinate system identification number

5

A1

RS

Location of A in coordinate 1 of RID

6

A2

RS

Location of A in coordinate 2 of RID

7

A3

RS

Location of A in coordinate 3 of RID

8

B1

RS

Location of B in coordinate 1 of RID

9

B2

RS

Location of B in coordinate 2 of RID

10

B3

RS

Location of B in coordinate 3 of RID

11

C1

RS

Location of C in coordinate 1 of RID

12

C2

RS

Location of C in coordinate 2 of RID

13

C3

RS

Location of C in coordinate 3 of RID

Record – CORD2S(2201,22,10) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

SIXTY5

I

Constant 65 or 3?

3

EIGHT

I

Constant 8 or 2?

4

RID

I

Reference coordinate system identification number

5

A1

RS

Location of A in coordinate 1 of RID

6

A2

RS

Location of A in coordinate 2 of RID

7

A3

RS

Location of A in coordinate 3 of RID

8

B1

RS

Location of B in coordinate 1 of RID

9

B2

RS

Location of B in coordinate 2 of RID

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Name

Word

Type

Description

10

B3

RS

Location of B in coordinate 3 of RID

11

C1

RS

Location of C in coordinate 1 of RID

12

C2

RS

Location of C in coordinate 2 of RID

13

C3

RS

Location of C in coordinate 3 of RID

Record – CORD3G(501,5,43) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

METHOD(2)

CHAR4

Methods

4

FORM(2)

CHAR4

Forms

6

THETAID(3)

I

Identification number for DEQATN or TABLE

9

CIDREF

I

Coordinate system identification number

Record – CSUPER(2301,23,304) Name

Word

Type

Description

1

SSID

I

Coded identification number for secondary superelement

2

PSID

I

Primary superelement identification number

3

G

I

Exterior grid or scalar point identificaiton numbers

Word 3 repeats until End of Record

Record – CSUPEXT(5501,55,297) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

G

I

Grid or scalar point IDs in the downstream superelement

Word 2 repeats until End of Record

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Chapter 4

Record – EXTRN(1627,16,463) Name

Word

Type

Description

1

GID

I

Grid point identification numbers to connect external SE

2

C

I

Component numbers

Words 1 through 2 repeat until (-1,-1) occurs

Record – FEEDGE(6101,61,388) Name

Word

Type

Description

1

EDGEID

I

Edge identification number

2

GRID1

I

Identification number of end GRID 1

3

GRID2

I

Identification number of end GRID 2

4

CID

I

Coordinate system identification number

5

GEOMIN

CHAR4

Type of referencing entry: "GMCURV" or "POINT"

6

GEOMID1

I

Identification number of a POINT or GMCURV entry

7

GEOMID2

I

Identification number of a POINT or GMCURV entry

Record – GMCURV(6601,66,392) Word

Name

Type

Description

1

CURVID

I

Curve identification number

2

GROUP(2)

CHAR4

Group of curves/surfaces to which this curve belongs

4

CIDIN

I

Coordinate system identification number for the geometry

5

CIDBC

I

Coordinate system identification number for the constraints

6

DATA

CHAR4

Geometry evaluator specific data

Word 6 repeats until End of Record

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Record – FEFACE(6201,62,389) Name

Word

Type

Description

1

FACEID

I

Face identification number

2

GRID1

I

Identification number of end GRID 1

3

GRID2

I

Identification number of end GRID 2

4

GRID3

I

Identification number of end GRID 3

5

GRID4

I

Identification number of end GRID 4

6

CIDBC

I

Coordinate system identification number for the constraints

7

SURFID(2)

I

Alternate method used to specify the geometry

Record – POINT(6001,60,377) Name

Word

Type

Description

1

ID

I

Point identification number

2

CID

I

Coordinate system identification number

3

X1

RS

Location of the point in coordinate 1 of CID

4

X2

RS

Location of the point in coordinate 2 of CID

5

X3

RS

Location of the point in coordinate 3 of CID

Record – GMSURF(10101,101,394) Name

Word

Type

Description

1

ID

I

Surface Identification number

2

GROUP(2)

CHAR4

Group of curves/surfaces to which this curve belongs

4

CIDIN

I

Coordinate system identification number for the geometry

5

CIDBC

I

Coordinate system identification number for the constraints

6

DATA

CHAR4

Geometry evaluator specific data

Word 6 repeats until End of Record

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Chapter 4

Record – GMCORD(6401,64,402) Name

Word

Type

Description

1

CID

I

Coordinate system identification number

2

ENTITY

CHAR4

Bulk Data entry used to define the coordinate system

3

ID1

I

Entity identification number 1

4

ID2

I

Entity identification number 2

Record – GRID(4501,45,1) Name

Word

Type

Description

1

ID

I

Grid point identification number

2

CP

I

Location coordinate system identification number

3

X1

RS

Location of the point in coordinate 1 of CP

4

X2

RS

Location of the point in coordinate 2 of CP

5

X3

RS

Location of the point in coordinate 3 of CP

6

CD

I

Degree-of-freedom coordinate system identification number

7

PS

I

Permanent single-point constraints

8

SEID

I

Superelement identification number

Record – SEBNDRY(1527,15,466) Name

Word

Type

Description

1

SEIDA

I

Superelement A identification number

2

SEIDB

I

Superelement B identification number

3

G

I

Boundary grid point identification number in SEIDA

Word 3 repeats until End of Record

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Data Block Descriptions F-M

Record – SEBULK(1427,14,465) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

TYPE

I

Superelement type

3

RSEID

I

Reference superelement identification number

4

METHOD

I

Boundary point search method: 1=automatic or 2=manual

5

TOL

RS

Location tolerance

6

LOC

I

Coincident location check option: yes=1 or no=2

7

MEDIA

I

Media format of boundary data of external SE

8

UNIT

I

FORTRAN unit number of OP2 and OP4 input of external SE

Record – SECONCT(427,4,453) Name

Word

Type

Description

1

SEIDA

I

Superelement A identification number

2

SEIDB

I

Superelement B identification number

3

TOL

RS

Location tolerance

4

LOC

I

Coincident location check option: yes=1 or no=2

5

UNDEF(4 )

None

9

GA

I

Grid point identification number in SEIDA

10

GB

I

Grid point identification number in SEIDB

Words 9 through 10 repeat until (-1,-1) occurs

Record – SEELT(7902,79,302) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

EID

I

Element identification number

Word 2 repeats until End of Record

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Record – SEEXCLD(527,72,454) Name

Word

Type

Description

1

SEIDA

I

Superelement A identification number

2

SEIDB

I

Superelement B identification number or –1 for all

3

GA

I

Grid point identification number in SEIDA

Word 3 repeats until End of Record

Record – SELABEL(1027,10,459) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

LABEL(14)

CHAR4

Label associated with superelement SEID

Record – SELOC(827,8,457) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

GA1

I

Grid point 1 identification number in SEID

3

GA2

I

Grid point 2 identification number in SEID

4

GA3

I

Grid point 3 identification number in SEID

5

GB1

I

Grid point 1 identification number in the main Bulk Data

6

GB2

I

Grid point 2 identification number in the main Bulk Data

7

GB3

I

Grid point 3 identification number in the main Bulk Data

Record – SEMPLN(927,9,458) Word

Name

Type

Description

1

SEID

I

Superelement identification number

2

MIRRTYPE

I

Mirror type

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Name

Word

Type

MIRRTYPE=1

Description

Plane

3

G1

I

Grid point 1 identification number in the main Bulk Data

4

G2

I

Grid point 2 identification number in the main Bulk Data

5

G3

I

Grid point 3 identification number in the main Bulk Data

6

UNDEF(2 )

None

Not Defined

MIRRTYPE=2

Normal

3

G

I

Grid point identification number in the main Bulk Data

4

CID

I

Coordinate system identification number

5

N1

RS

Normal component in direction 1 of CID

6

N2

RS

Normal component in direction 2 of CID

7

N3

RS

Normal component in direction 3 of CID

End MIRRTYPE

Record – SENQSET(1327,13,464) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

NQSET

I

Number of internally generated scalar points

Record – SEQGP(5301,53,4) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

SEQID

I

Sequenced identification number

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Chapter 4

Record – SEQSEP(5401,54,305) Name

Word

Type

Description

1

SSID

I

Secondary superelement identification number

2

PSID

I

Primary superelement identification number

3

G

I

Exterior grid or scalar point identification numbers

Word 3 repeats until End of Record

Record – SESET(5601,56,296) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

G

I

Grid or scalar point identification number

Word 2 repeats until End of Record

Record – SETREE(1227,12,462) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

SEUPI

I

Upstream superelement identification number

Word 2 repeats until End of Record

Record – SNORM(5678,71,475) Word

Name

Type

Description

1

GID

I

Grid point identification number

2

CID

I

Coordinate system identification number

3

N1

RS

Normal component in direction 1 of CID

4

N2

RS

Normal component in direction 2 of CID

5

N3

RS

Normal component in direction 3 of CID

Record – CSUPER1(5701,57,323) This record is obsolete and is removed eventually.

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Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

PSID

I

Primary superelement identification number

3

TYPE

I

,{

4

VIEW

I

,{

5

DIROPT

I

,{

6

DIRTOL

RS

,{

7

GEOMTOL

RS

,{

8

CARDID

I

,{

9

MODEL

I

,{

10

SOLID

I

,{

11

DBSET

I

,{

12

COPY

I

,{

13

DELETE

I

,{

14

GRIDLIST

I

,{

15

XX

I

xx

xx

XX =0 16

G

I

,{

17

C

I

,{

Words 16 through 17 repeat until (-1,-1,-1) occurs yy

XX =-1 End XX

Record – CSUPUP(5801,58,324) This record is obsolete and is removed eventually. Word

Name

Type

Description

1

SEUP1

I

,{

2

PSID

I

Primary superelement identification number

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Word

Data Block Descriptions F-M

Name

Type

Description

3

SEDOWN1

I

,{

4

SEUP2

I

,{

5

PSID

I

Primary superelement identification number

6

SEDOWN2

I

,{

Record - TRAILER Name

Word 1

BIT(6)

Type I

Description Record presence trailer words

Notes: 1. CSUPER1 and CSUPUP records are recognized only by the IFP module and are removed eventually. 2. ADUMi records are not written. Rather, the contents are coded and stored in words 45 thru 54 of the system cell common block. 3. There is no record for the GRDSET entry. Rather, the GRID record is modified accordingly. 4. When GEOM1 is an alias for GEOM1VU, view grids are appended to the GRID record. The starting view grid id is controlled by system cell 180. 5. On the SEBULK entry, the allowable values for superelement type are: •

1=PRIMARY

•

2=COLLECTOR

•

3=IDENTICAL

•

4=REPEATED

•

5=EXTERNAL

•

6=MIRROR

6. GEOM168 is the same as GEOM1 except that: •

In Record - CORD2C, the locations of A, B, and C in coordinates 1, 2, and 3 of RID are converted from RX to RS.

•

In Record - CORD2R, the locations of A, B, and C in coordinates 1, 2, and 3 of RID are converted from RX to RS.

•

In Record - CORD2S, the locations of A, B, and C in coordinates 1, 2, and 3 of RID are converted from RX to RS.

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•

In Record - POINT, the location of the point in coordinate 1, 2, or 3 of CID are converted from RX to RS.

•

In Record - GRID, the location of the point in coordinate 1, 2, and 3 of CP are converted from RX to RS.

4.7 GEOM4705 Table of Bulk Data entry images related to constraints (Pre-MSC Nastran 2001). Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity. Note See the Note 1 for a listing of the differences between GEOM4705 and GEOM4.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – ASET(5561,76,215) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 2 – ASET1(5571,77,216) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

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Name

Word

Type

Description

End THRUFLAG

Record 3 – BNDFIX(110,1,584) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 4 – BNDFIX1(210,2,585) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 5 – BNDFREE(310,3,586) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 6 – BNDFREE1(410,4,587) Name

Word 1

4-120

C

DMAP Programmer’s Guide

Type I

Description Component numbers

Data Block Descriptions F-M

Name

Word 2

Type

Description

I

THRUFLAG

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 7 – BNDGRID(10200,102,473) Name

Word 1

Type I

GPI

Description Shape boundary grid point identification number

Record 8 – BSET(110,1,311) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 9 – BSET1(210,2,312) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

I

ID1

First grid or scalar point identification number

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Chapter 4

Name

Word 4

Type

ID2

I

Description Second grid or scalar point identification number

End THRUFLAG

Record 10 – CSET(310,3,313) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 11 – CSET1(410,4,314) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 12 – CYAX(1510,15,328) Name

Word 1

G

Type I

Word 1 repeats until End of Record

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Description Grid point identification number on the axis of symmetry

Data Block Descriptions F-M

Record 13 – CYJOIN(5210,52,257) Name

Word

Type

Description

1

SIDE

I

Side identification number: 1 or 2

2

C(2)

CHAR4

Coordinate system type on symetry booundary

4

ID

I

Grid or scalar point identification number

Word 4 repeats until End of Record

Record 14 – CYSUP(1610,16,329) Name

Word

Type

Description

1

GID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 15 – CYSYM(1710,17,330) Name

Word

Type

Description

1

NSEG

I

Number of segments

2

STYPE(2)

CHAR4

Symmetry type

Record 16 – EGENDT(8801,88,9022) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

SPCID

I

SPC set identification number

3

EDGEID

I

Edge identification number

4

C

I

Component numbers

5

DISTFLG

I

Distribution flag

6

DISFUN

I

Distribution function (DEQATN)

7

DISTAB

I

Distribution table (TABLE3D)

8

FIELD(4)

RS

See GMBC record

Words 4 through 11 repeat 6 times

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Chapter 4

Name

Word

Type

Description

12

ELTYPE

I

Element type

13

EID

I

Element identification number

14

EORD

I

Edge order

15

EDGEID

I

Edge identification number

16

FACEID

I

Face identification number

17

CURVID

I

Curve identification number

18

SURFID

I

Surface identification number

19

G(2)

I

Grid point identification numbers

21

MIDG

I

22

POINT(2)

I

Point identification numbers

24

F1ID

I

Grid-n 1 identification number

25

F2ID

I

Grid-n 2 identification number

26

NDOF

I

I,{

27

CIDE

I

Coordinate system identification number for the edge

28

MAXNDFE

I

Maximum number of degrees-of-freedom, or stride, for the edge

29

MAXNDFB

I

Maximum number of degrees-of-freedom, or stride, for the body

30

PUSER

I

p-level specified by user

31

PSEL

I

p-level selected by program

32

BODYFID

I

Grid-n identification number for the body

33

NDOFB

I

Number of degrees-of-freedom for the body

34

F1ID

I

Grid-n 1 identification number

35

CID

I

Coordinate system identification number

36

X

RS

S,{

37

Y

RS

S,{

38

Z

RS

S,{

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Data Block Descriptions F-M

Name

Word

Type

Description

Words 34 through 38 repeat 7 times

Record 17 – FCENDT(9001,90,9024) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

SID

I

Set identification number

3

FACEID

I

Face identification number

4

C

I

Component numbers

5

DISTFLG

I

Distribution flag

6

DISFUN

I

Distribution function (DEQATN)

7

DISTAB

I

Distribution table (TABLE3D)

8

FIELD(9)

RS

See GMBC record

Words 4 through 16 repeat 6 times 17

F1ID

I

Grid-n 1 identification number

18

F2ID

I

Grid-n 2 identification number

19

NDOF

I

Number of degrees-of-freedom for the face

20

MAXNDF

I

Maximum number of degrees-of-freedom or stride

21

CIDE

I

Coordinate system identification number of the edge

Words 17 through 21 repeat 4 times 22

FACFID

I

Grid-n identification number for the face

23

NDOF

I

Number of degrees-of-freedom for the face

24

MAXNDFF

I

Maximum number of degrees-of-freedom for the face

25

CIDF

I

Coordinate system identification number for the face

26

ELTYPE

I

Element type

27

EID

I

Element identification number

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Chapter 4

Name

Word

Type

Description

28

EORD

I

Edge order

29

FACEID

I

Face identification number

30

SURFID

I

Surface identification number

31

G(4)

I

Grid point identification numbers

35

CIDF

I

Coordinate system identification number for the face

36

MAXNDIF

I

37

UNDEF

None

38

PUSER(4)

I

p-level specified by user

42

PSEL(4)

I

p-level selected by program

46

FACFID

I

Grid-n identification number for the face

47

NDOF

I

Number of degrees-of-freedom for the face

48

F1ID

I

Grid-n 1 identification number

49

CID

I

Coordinate system identification number

50

X

RS

51

Y

RS

52

Z

RS

Words 48 through 52 repeat 13 times

Record 18 – GMBC(8001,80,395) Name

Word

Type

Description

1

LID

I

Load set identification number

2

SPCID

I

SPC set identification number

3

C

I

Component number

4

ENTITY

CHAR4

Entity type that is being loaded

5

ENTID

I

Entity identification number

6

METHOD

I

Method of data specification

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Data Block Descriptions F-M

Name

Word

Type

METHOD =1

TABLE3D

7

TABLID

I

8

UNDEF(8 )

None

METHOD =2

TABLE3D identification number

DEQATN

7

EQTNID

I

8

UNDEF(8 )

None

METHOD =3 7

RS

METHOD =4

RS

METHOD =5

Enforced displacement data

QUAD RS

FIELD(9)

METHOD =6 7

Enforced displacement data

LINEAR FIELD(9)

7

DEQATN identification number

CONSTANT FIELD(9)

7

Description

Enforced displacement data

CUBIC RS

FIELD(9)

Enforced displacement data

End METHOD

Record 19 – GMSPC(7801,78,393) Name

Word

Type

Description

1

ID

I

Set identification number

2

C

I

Component number

3

ENTITY

CHAR4

Entity type that is being loaded

4

ENTID

I

Entity identification number

Record 20 – MPC(4901,49,17) Name

Word

Type

Description

1

SID

I

Set identification number

2

G

I

Grid point identification number

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Chapter 4

Name

Word

Type

Description

3

C

I

Component number

4

A

RS

Coefficient

5

GI

I

Grid point identification number

6

CI

I

Component number

7

AI

RS

Coefficient

Words 5 through 7 repeat until (-1,-1,-1) occurs

Record 21 – MPCADD(4891,60,83) Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Set identification number

Word 2 repeats until End of Record

Record 22 – OMIT(5001,50,15) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 23 – OMIT1(4951,63,92) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

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First grid or scalar point identification number

Data Block Descriptions F-M

Name

Word 4

Type

ID2

I

Description Second grid or scalar point identification number

End THRUFLAG

Record 24 – QSET(510,5,315) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 25 – QSET1(610,6,316) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 26 – RBAR(6601,66,292) Word

Name

Type

Description

1

EID

I

Element identification number

2

GA

I

Grid point A identification number

3

GB

I

Grid point B identification number

4

CNA

I

Component numbers of independent degrees-of-freedom at end A

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Word

Data Block Descriptions F-M

Name

Type

Description

5

CNB

I

Component numbers of independent degrees-of-freedom at end B

6

CMA

I

Component numbers of dependent degrees-of-freedom at end A

7

CMB

I

Component numbers of dependent degrees-of-freedom at end B

Record 27 – RBE1(6801,68,294) Word

Name

Type

Description

1

EID

I

Element identification number

2

GN

I

Grid point identification number for independent degrees-of-freedom

3

CN

I

Component numbers of independent degrees-of-freedom

Words 2 through 3 repeat until (-2,-2) occurs 4

GM

I

Grid point identification number for dependent degrees-of-freedom

5

CM

I

Component numbers of dependent degrees-of-freedom

Words 4 through 5 repeat until (-1,-1) occurs

Record 28 – RBE2(6901,69,295) Word

Name

Type

Description

1

EID

I

Element identification number

2

GN

I

Grid point identification number for independent degrees-of-freedom

3

CM

I

Component numbers of dependent degrees-of-freedom

4

GM

I

Grid point identification number for dependent degrees-of-freedom

Word 4 repeats until -1 occurs

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Data Block Descriptions F-M

Record 29 – RBE3(7101,71,187) Name

Word

Type

Description

1

EID

I

Element identification number

2

REFG

I

Reference grid point identification number

3

REFC

I

Component numbers at the reference grid point

4

WT1

RS

Weighting factor for components of motion at G

5

C

I

Component numbers

6

G

I

Grid point identification number

Word 6 repeats until -1 occurs Words 4 through 6 repeat until -2 occurs 7

GM

I

Grid point identification number for dependent degrees-of-freedom

8

CM

I

Component numbers of dependent degrees-of-freedom

Words 7 through 8 repeat until -3 occurs

Record 30 – RELEASE(1310,13,247) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

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Data Block Descriptions F-M

Record 31– RROD(6501,65,291) Word

Name

Type

Description

1

EID

I

Element identification number

2

GA

I

Grid point A identification number

3

GB

I

Grid point B identification number

4

CMA

I

Component numbers of dependent degrees-of-freedom at end A

5

CMB

I

Component numbers of dependent degrees-of-freedom at end B

Record 32– RSPLINE(7001,70,186) Name

Word

Type

Description

1

EID

I

Element identification number

2

DBYL

RS

Ratio of the diameter to the sum of the segments lengths

3

G1

I

Grid point identification number

4

G2

I

Grid point identification number

5

C2

I

Components to be constrained

Words 4 through 5 repeat until (-1,-1) occurs

Record 33– RSSCON(7201,72,398) Name

Word

Type

Description

1

EID

I

Element identification number

2

TYPE(C)

I

Type of connectivity

TYPE =0

GRID style 1

3

GRID1

I

Grid identification number 1

4

GRID2

I

Grid identification number 2

5

GRID3

I

Grid identification number 3

6

UNDEF(3 )

None

TYPE =01

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DMAP Programmer’s Guide

GRID style 2

Data Block Descriptions F-M

Name

Word

Type

Description

3

GRID1

I

Grid identification number 1

4

GRID2

I

Grid identification number 2

5

GRID3

I

Grid identification number 3

6

GRID4

I

Grid identification number 4

7

GRID5

I

Grid identification number 5

8

GRID6

I

Grid identification number 6

TYPE =02

Edge style

3

EDGE1

I

Edge identification number 1

4

EDGE2

I

Edge identification number 2

5

EDGE3

I

Edge identification number 3

6

UNDEF(3 )

None

TYPE =03

Element style

3

ELID1

I

Element identification number 1

4

ELID2

I

Element identification number 2

5

UNDEF(4 )

None

TYPE =04

CINTERF

3

CBID

I

4

SBID

I

5

CBPID

I

6

UNDEF(3)

None

End TYPE

Record 34 – RTRPLT(6701,67,293) Name

Word

Type

Description

1

EID

I

Element identification number

2

GA

I

Grid point A identification number

3

GB

I

Grid point B identification number

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Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

4

GC

I

Grid point C identification number

5

CNA

I

Component numbers for independent degrees-of-freedom at vertex A

6

CNB

I

Component numbers for independent degrees-of-freedom at vertex B

7

CNC

I

Component numbers for independent degrees-of-freedom at vertex C

8

UNDEF

None

9

CMA

I

Component numbers for dependent degrees-of-freedom at vertex A

10

CMB

I

Component numbers for dependent degrees-of-freedom at vertex B

11

CMC

I

Component numbers for dependent degrees-of-freedom at vertex C

Record 35 – RWELD(11901,119,561) Name

Word

Type

Description

1

EID

I

Element ID

2

GA

I

Grid ID of GA

3

TYPE

I

Type of shell element

4

GI(8)

I

Grid IDs of shell element

12

GS

I

Grid ID of GS

Record 36 – SEBSET(710,7,317) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

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Data Block Descriptions F-M

Record 37 – SEBSET1(810,8,318) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 38 – SECSET(910,9,319) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record 39 – SECSET1(1010,10,320) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

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Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 40 – SEQSET(1110,11,321) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record 41 – SEQSET1(1210,12,322) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 42 – SESUP(1410,14,325) Word 1

4-136

Name SEID

DMAP Programmer’s Guide

Type I

Description Superelement identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record 43 – SEUSET(1810,18,334) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

SNAME

I

Set name

3

ID

I

Grid or scalar point identification number

4

C

I

Component numbers

Record 44 – SEUSET1(1910,19,335) Name

Word

Type

Description

1

SEID

I

Superelement identification number

2

SNAME

I

Set name

3

C

I

Component numbers

4

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

5

I

ID

Grid or scalar point identification number

Word 5 repeats until End of Record THRUFLAG=1

Yes

5

ID1

I

First grid or scalar point identification number

6

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 45 – SPC(5501,55,16) Word 1

Name SID

Type I

Description Set identification number

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Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

Record 46 – SPC1(5481,58,12) Name

Word

Type

Description

1

SID

I

Set identification number

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 47 – SPCADD(5491,59,13) Name

Word

Type

Description

1

SID

I

Set identification number

2

S

I

Set identification number

Word 2 repeats until End of Record

Record 48 – SPCD(5110,51,256) Word

Name

Type

Description

1

SID

I

Superelement identification number

2

ID

I

Grid or scalar point identification number

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Data Block Descriptions F-M

Name

Word

Type

Description

3

C

I

Component numbers

4

D

RS

Enforced displacement

Record 49 – SPCDE(8701,87,9021) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

EDGEID

I

Edge identification number

6

SID

I

Set identification number

Record 50 – SPCDF(8901,89,9023) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

FACEID

I

Face identification number

6

SID

I

Set identification number

Record 51 – SPCDG(9701,97,9030) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

METHOD

I

Method

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Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

5

D

RS

Enforced displacement

6

SID

I

Set identification number

Record 52 – SPCE(9301,93,9027) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

EDGID

I

Grid or scalar point identification number

Record 53 – SPCEB(9101,91,9025) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

EDGEID

I

Edge identification number

Record 54 – SPCF(9401,94,9028) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

FACEID

I

Face identification number

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Data Block Descriptions F-M

Record 55 – SPCFB(9201,92,9026) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

D

RS

Enforced displacement

5

LOADID

I

Load set identification number

Record 56 – SPCGB(9601,96,9029) Name

Word

Type

Description

1

LOADID

I

Load set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

METHOD

I

I,{

5

D

RS

Enforced displacement

6

SID

I

Set identification number

Record 57 – SPCGRID(8601,86,9031) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

4

UNDEF(2 )

None

Record 58 – SPCOFF(6110,61,343) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

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Data Block Descriptions F-M

Chapter 4

Record 59 – SPCOFF1(6210,62,344) Name

Word

Type

Description

1

C

I

Component numbers

2

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

3

I

ID

Grid or scalar point identification number

Word 3 repeats until End of Record THRUFLAG=1

Yes

3

ID1

I

First grid or scalar point identification number

4

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 60 – SUPORT(5601,56,14) Name

Word

Type

Description

1

ID

I

Grid or scalar point identification number

2

C

I

Component numbers

Record 61 – SUPORT1(10100,101,472) Name

Word

Type

Description

1

SID

I

Set identification number

2

ID

I

Grid point identification number

3

C

I

Component numbers

Words 2 through 3 repeat until (-1,-1) occurs

Record 62 – TEMPBC(11309,113,426) Word

Name

1

SID

4-142

DMAP Programmer’s Guide

Type I

Description Temperature set identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

TYPE

I

Type of temperature boundary condition: STAT or TRAN

3

TEMP

RS

Temperature

4

GID

I

Grid or scalar point identification number

Record 63 – USET(2010,20,193) Name

Word

Type

Description

1

SNAME

I

Set name

2

ID

I

Grid or scalar point identification number

3

C

I

Component numbers

Record 64 – USET1(2110,21,194) Name

Word

Type

Description

1

SNAME

I

Set name

2

C

I

Component numbers

3

THRUFLAG

I

Thru range flag

THRUFLAG=0

No

4

I

ID

Grid or scalar point identification number

Word 4 repeats until End of Record THRUFLAG=1

Yes

4

ID1

I

First grid or scalar point identification number

5

ID2

I

Second grid or scalar point identification number

End THRUFLAG

Record 65 – TRAILER Word 1

Name BIT(6)

Type I

Description Record presence trailer words

DMAP Programmer’s Guide

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Chapter 4

Notes: 1. GEOM4705 is the same as GEOM4 except that: •

In Record - MPC, coefficients A and AI are converted from RX to RS.

•

ALF is stripped from Record - RBAR. The record size is reduced from 8 words to 7 words.

•

ALF and UNDEF are stripped from Record - RBE1. The record size is reduced from 7 words to 5 words.

•

ALF is stripped from Record - RBE2. The record size is reduced from 5 words to 4 words.

•

ALF is stripped from Record - RBE3. The record size is reduced from 9 words to 8 words.

•

ALF is stripped from Record - RROD. The record size is reduced from 6 words to 5 words.

•

ALF is stripped from Record - RTRPLT. The record size is reduced from 12 words to 11 words.

•

4.8 GPDT Grid point definition table. Contains a list of all grid points and scalar points in internal sort, with (for grid points) their x, y, z locations in the location coordinate system along with a location and displacement coordinate system identification number, and constraint information.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – POINT Word

Name

Type

Description

1

ID

I

Internal grid point identification number

2

CP

I

Location coordinate system identification number

3

X1

RX

Location of the point in coordinate 1 of CP (X, R or Rho)

4

X2

RX

Location of the point in coordinate 2 of CP (Y, Theta or Theta)

5

X3

RX

Location of the point in coordinate 3 of CP (Z, Phi or Phi)

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Data Block Descriptions F-M

Word

Name

Type

Description

6

CD

I

Degree-of-freedom coordinate system identification number

7

PS

I

Permanent single-point constraints

Record 2 – TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of grid points and scalar points

Notes: 1. Scalar points are identified by CP=-1 and words X1 through PS are zero. 2. See the “GRID” bulk entry in the NX Nastran Quick Reference Guide for a description of the PS constraint code. 3. For fluid grid points, CD=-1.

4.9 GPDT68 Grid point definition table (Pre-MSC Nastran Version 69). Contains a list of all grid points and scalar points in internal sort, with (for grid points) their x, y, z locations in the location coordinate system along with a location and displacement coordinate system identification number, and constraint information. Note See the Note 4 for a listing of the differences between GPDT68 and GPDT.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – POINT Word

Name

Type

Description

1

ID

I

Internal grid point identification number

2

CP

I

Location coordinate system identification number

DMAP Programmer’s Guide

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Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

3

X1

RS

Location of the point in coordinate 1 of CP (X, R or Rho)

4

X2

RS

Location of the point in coordinate 2 of CP (Y, Theta or Theta)

5

X3

RS

Location of the point in coordinate 3 of CP (Z, Phi or Phi)

6

CD

I

Degree-of-freedom coordinate system identification number

7

PS

I

Permanent single-point constraints

Record 2 – TRAILER Word

Name

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of grid points and scalar points

Notes: 1. Scalar points are identified by CP=-1 and words X1 through PS are zero. 2. See the “GRID” bulk entry in the NX Nastran Quick Reference Guide for a description of the PS constraint code. 3. For fluid grid points, CD=-1. 4. GPDT68 is the same as GPDT except that: •

In Record - POINT, X1, X2, and X3 are converted from RX to RS.

4.10 GPL Grid point list.

Record 0 – HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

SEID

I

Superelement identification number

Record 1 – GRID Contains a list of external grid and scalar identification numbers in internal sort.

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Data Block Descriptions F-M

Word 1

Name GRIDID

Type I

Description External grid or scalar identification number

Record 2 – GRIDSIL Contains pairs of external grid and scalar identification numbers and sequence numbers in internal sort. Word

Name

Type

Description

1

GRIDID

I

External grid or scalar identification number

2

SEQNO

I

Sequence number = 1000 * external identification number

Record 3 – TRAILER Word

Name

Type

1

NGS

I

2

UNDEF(5)

None

Description Total number of grid and scalar points

Notes: 1. SEQNO, sequence number, can be overridden by the SEQGP Bulk Data entry. 2. With OMACHPR = NO, the MAKEOLD module removes the extra grids associated with Lagrange rigids.

4.11 HIS Table of design iteration history Contains a compilation of information from the convergence checks.

Record 0 – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name

Record 1 – Repeat Word 1

Name DSITER

Type I

Description Design iteration number

DMAP Programmer’s Guide

4-147

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

2

CVTYP

I

Convergence type: 1=soft or 2=hard

3

CVPROV

I

Convergence result: 0=no, 1=soft, or 2=hard

4

OBJ1

RS

Initial objective value

5

OBJO

RS

Final objective value

6

GMAX

RS

Maximum constraint value

7

IRMAX

I

Row of the maximum constraint value

8

XVAL

RS

Design variable value

Word 8 repeats until End of Record

Record 2 – TRAILER Name

Word

Type

1

NDV

I

2

UNDEF(5 )

None

Description Number of design variables

Notes: 1. For soft convergence, the final objective and constraint values are those obtained from DOM9. 2. For hard convergence, they are obtained from a re-analysis. 3. The design variable values are identical for soft and hard convergence and are repeated for consistency.

4.12 KDICT Element stiffness dictionary table Each record defines an element in terms of its connection data and address pointers into the corresponding element matrix in the KELM data block.

Record 0 – HEADER Word 1

4-148

Name NAME(2)

DMAP Programmer’s Guide

Type CHAR4

Description Data block name

Data Block Descriptions F-M

Record 1 – Repeat Repeats for each element type. Name

Word

Type

Description

1

ELTYPE

I

Element type

2

NUMWDS

I

Number of words per entry

3

NUMGRID(C)

I

Number of defined grid points

4

DOFPERG

I

Degrees of freedom per grid point

5

FORM(C)

I

Form of element matrix

Words 6 through max repeat until End of Record 6

EID

I

Element identification number

7

NACTIVEG

I

Number of active grid points

8

GE

RS

Material damping constant

9

ADDRESS1

I

GINO address of matrix

10

ADDRESS2

I

GINO address of matrix

FORM =3 11

Lower left triangle in global coord. system SIL

I

SIL values of connected grid points

Word 11 repeats NUMGRID times FORM =4 11

Lower left triangle and transformation matrices SIL

I

SIL values of connected grid points

Word 11 repeats NUMGRID times 12

E11

RX

Element to basic transformation

13

E21

RX

Element to basic transformation

14

E31

RX

Element to basic transformation

15

E12

RX

Element to basic transformation

16

E22

RX

Element to basic transformation

17

E32

RX

Element to basic transformation

18

E13

RX

Element to basic transformation

19

E23

RX

Element to basic transformation

DMAP Programmer’s Guide

4-149

Data Block Descriptions F-M

Chapter 4

Name

Word 20

Type

E33

RX

FORM =5 11

Description Element to basic transformation

Lower left triangle in basic coordinate system I

SIL

SIL values of connected grid points

Word 11 repeats NUMGRID times End FORM

Record 2 – TRAILER Name

Word

Type

Description

1

PREC

I

Precision of element matrices (1 or 2)

2

MAXROW

I

Maximum number of rows in an element matrix

3

MAXGRID

I

Maximum number of grid points in a FORM=4 record

4

UNDEF(3 )

None

Notes: 1. FORM=3 indicates that the element stiffness matrix is defined in the global coordinate system. 2. FORM=4 indicates that the element stiffness matrix is defined in the element coordinate system. The transformation matrix is also contained in each element dictionary. 3. FORM=5 indicates that the element stiffness matrix is defined in the basic coordinate system. 4. SIL=0 indicates inactive degrees-of-freedom.

4.13 LAMA Normal modes or buckling eigenvalue summary table

Record 0 – HEADER Word 1

4-150

Name NAME(2)

DMAP Programmer’s Guide

Type CHAR4

Description Data block name

Data Block Descriptions F-M

Record 1 – OFPID – OFP Header Record Word

Name

Type

Description

1

RECID(2)

I

3

UNDEF(7 )

None

10

SEVEN

I

Constant 7

11

RESFLG

I

Residual vector augmentation flag

12

UNDEF(39 )

None

51

TITLE(32)

CHAR4

Title character string (TITLE)

83

SUBTITLE(32)

CHAR4

Subtitle character string (SUBTITLE)

115

LABEL(32)

CHAR4

LABEL character string (LABEL)

Constants 21 and 6

Record 2 – LAMA Repeats for each eigenvalue. Word

Name

Type

Description

1

MODE

I

Mode number

2

ORDER

I

Extraction order

3

EIGEN

RS

Eigenvalue

4

OMEGA

RS

Square root of eigenvalue

5

FREQ

RS

Frequency

6

MASS

RS

Generalized mass

7

STIFF

RS

Generalized stiffness

Record 3 – TRAILER Word

Name

Type

1

NMODES

I

2

UNDEF(6 )

None

Description Number of modes

DMAP Programmer’s Guide

4-151

Data Block Descriptions F-M

Chapter 4

4.14 MPT Table of Bulk Data entry images related to material properties

Record – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record – CREEP(1003,10,245) Name

Word

Type

Description

1

MID

I

Material identification number

2

T0

RS

Reference temperature

3

EXP

RS

Temperature-dependent term in the creep rate expression

4

FORM

I

Form of the input data: "CRLAW" or "TABLE"

5

TIDKP

I

TABLES1 ID which defines creep model parameter Kp

6

TIDCP

I

TABLES1 ID which defines creep model parameter Cp

7

TIDCS

I

TABLES1 ID which defines creep model parameter Cs

8

THRESH

RS

Threshold limit for creep process

9

TYPE

I

Empirical creep law identification number

10

AG(7)

RS

Coefficients of the empirical creep law

Record – MAT1(103,1,77) Name

Word

Type

Description

1

MID

I

Material identification number

2

E

RS

Young’s modulus

3

G

RS

Shear modulus

4

NU

RS

Poisson’s ratio

5

RHO

RS

Mass density

4-152

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

6

A

RS

Thermal expansion coefficient

7

TREF

RS

Reference temperature

8

GE

RS

Structural element damping coefficient

9

ST

RS

Stress limit for tension

10

SC

RS

Stress limit for compression

11

SS

RS

Stress limit for shear

12

MCSID

I

Material coordinate system identification number

Record – MAT2(203,2,78) Name

Word

Type

Description

1

MID

I

Material identification number

2

CIJ(6)

RS

Material property matrix

8

RHO

RS

Mass density

9

AJ(3)

RS

Thermal expansion coefficients

12

TREF

RS

Reference temperature

13

GE

RS

Structural element damping coefficient

14

ST

RS

Stress limit for tension

15

SC

RS

Stress limit for compression

16

SS

RS

Stress limit for shear

17

MCSID

I

Material coordinate system identification number

Record – MAT3(1403,14,122) Word

Name

Type

Description

1

MID

I

Material identification number

2

EX

RS

Young’s modulus in the x direction

3

ETH

RS

Young’s modulus in the theta direction

DMAP Programmer’s Guide

4-153

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

4

EZ

RS

Young’s modulus in the z direction

5

NUXTH

RS

Poisson’s ratios in x-theta direction

6

NUTHZ

RS

Poisson’s ratios in theta-z direction

7

NUZX

RS

Poisson’s ratios in z-x direction

8

RHO

RS

Mass density

9-10

UNDEF(2)

None

11

GZX

RS

Shear modulus in the z-x direction

12

AX

RS

Thermal expansion coefficient in the x direction

13

ATH

RS

Thermal expansion coefficient in the theta direction

14

AZ

RS

Thermal expansion coefficient in the z direction

15

TREF

RS

Reference temperature

16

GE

RS

Structural element damping coefficient

Record – MAT4(2103,21,234) Name

Word

Type

Description

1

MID

I

Material identification number

2

K

RS

Thermal conductivity

3

CP

RS

Heat capacity per unit mass at constant pressure

4

RHO

RS

Mass density

5

H

RS

Free convection heat transfer coefficient

6

MU

RS

Dynamic viscosity

7

HGEN

RS

Heat generation capability used with QVOL entries

8

REFENTH

RS

Reference enthalpy

9

TCH

RS

Lower temperature limit for phase change region

10

TDELTA

RS

Total temperature change range

11

QLAT

RS

Latent heat of fusion per unit mass

4-154

DMAP Programmer’s Guide

Data Block Descriptions F-M

Record – MAT5(2203,22,235) Name

Word

Type

Description

1

MID

I

Material identification number

2

KIJ(6)

RS

Thermal conductivity matrix

8

CP

RS

Heat capacity per unit mass

9

RHO

RS

Mass density

10

HGEN

RS

Heat generation capability used with QVOL entries

Record – MAT8(2503,25,288) Name

Word

Type

Description

1

MID

I

Material identification number

2

E1

RS

Modulus of elasticity in longitudinal direction

3

E2

RS

Modulus of elasticity in lateral direction

4

NU12

RS

Poisson’s ratio

5

G12

RS

In-plane shear modulus

6

G1Z

RS

Transverse shear modulus for shear in 1-Z plane

7

G2Z

RS

Transverse shear modulus for shear in 2-Z plane

8

RHO

RS

Mass density

9

A1

RS

Thermal expansion coefficient in longitudinal direction

10

A2

RS

Thermal expansion coefficient in lateral direction

11

TREF

RS

Reference temperature for the calculation of thermal loads

12

XT

RS

Allowable longitudinal stress or strain in tension

13

XC

RS

Allowable longitudinal stress or strain in compression

14

YT

RS

Allowable lateral stress or strain in tension

15

YC

RS

Allowable lateral stress or strain in compression

16

S

RS

Allowable stress or strain for in-plane shear

DMAP Programmer’s Guide

4-155

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

17

GE

RS

Structural damping coefficient

18

F12

RS

Interaction term in the tensor polynomial theory of Tsai-Wu

19

STRN

RS

For the maximum strain theory only

Record – MAT9(2603,26,300) Name

Word

Type

Description

1

MID

I

Material identification number

2

G(21)

RS

Material property matrix

23

RHO

RS

Mass density

24

A(6)

RS

Thermal expansion coefficients

30

TREF

RS

Reference temperature for the calculation of thermal loads

31

GE

RS

Structural damping coefficient

32

UNDEF(4 )

None

Record – MAT10(2801,28,365) Name

Word

Type

Description

1

MID

I

Material identification number

2

BULK

RS

Bulk modulus

3

RHO

RS

Mass density

4

C

RS

Speed of sound

5

GE

RS

Structural damping coefficient

Record – MAT11(2903,29,371) Solid element orthotropic material property definition. Defines the material properties for a 3-D orthotropic material for isoparametric solid elements. Word 1

4-156

Name MID

DMAP Programmer’s Guide

Type I

Description Material identification number

Data Block Descriptions F-M

Word

Name

Type

Description

2

E1

RS

Modulus of elasticity in the longitudinal direction or 1-direction

3

E2

RS

Modulus of elasticity in the lateral direction or 2-direction

4

E3

RS

Modulus of elasticity in the thickness direction or 3-direction

5

NU12

RS

Poisson’s ratio (2/1 for uniaxial loading in the 1-direction)

6

NU13

RS

Poisson’s ratio (3/1 for uniaxial loading in the 1-direction)

7

NU23

RS

Poisson’s ratio (3/2 for uniaxial loading in the 2-direction)

8

G12

RS

In-plane shear modulus

9

G13

RS

Transverse shear modulus for shear in the 1–3 plane

10

G23

RS

Transverse shear modulus for shear in the 2–3 plane

11

RHO

RS

Mass density

12

A1

RS

Thermal expansion coefficient in the longitudinal direction

13

A2

RS

Thermal expansion coefficient in the lateral direction

14

A3

RS

Thermal expansion coefficient in the thickness direction

15

TREF

RS

Reference temperature for calculation of thermal loads

16

GE

RS

Structural damping coefficient

17

UNDEF(16)

None

Record – MATFT(3403,34,902) Word 1

Name MID

Type I

Description Material identification number

DMAP Programmer’s Guide

4-157

Chapter 4

Data Block Descriptions F-M

Name

Word 2

FTOPT

FTOPT=1

Type I

Description Failure theory option

Hill failure theory

3

XT

RS

Allowable longitudinal stress in tension

4

XC

RS

Allowable longitudinal stress in compression

5

YT

RS

Allowable lateral stress in tension

6

YC

RS

Allowable lateral stress in compression

7

ZT

RS

Allowable transverse stress in tension

8

ZC

RS

Allowable transverse stress in compression

9

SXY

RS

Allowable shear stress in the xy-plane

10

SYZ

RS

Allowable shear stress in the yz-plane

11

SZX

RS

Allowable shear stress in the zx-plane

FTOPT=2

Hoffman failure theory

3

XT

RS

Allowable longitudinal stress in tension

4

XC

RS

Allowable longitudinal stress in compression

5

YT

RS

Allowable lateral stress in tension

6

YC

RS

Allowable lateral stress in compression

7

ZT

RS

Allowable transverse stress in tension

8

ZC

RS

Allowable transverse stress in compression

9

SXY

RS

Allowable shear stress in the xy-plane

10

SYZ

RS

Allowable shear stress in the yz-plane

11

SZX

RS

Allowable shear stress in the zx-plane

FTOPT=3

Tsai-Wu failure theory

3

XT

RS

Allowable longitudinal stress in tension

4

XC

RS

Allowable longitudinal stress in compression

5

YT

RS

Allowable lateral stress in tension

6

YC

RS

Allowable lateral stress in compression

4-158

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

7

ZT

RS

Allowable transverse stress in tension

8

ZC

RS

Allowable transverse stress in compression

9

SXY

RS

Allowable shear stress in the xy-plane

10

SYZ

RS

Allowable shear stress in the yz-plane

11

SZX

RS

Allowable shear stress in the zx-plane

12

F12

RS

Interaction term in the tensor polynomial theory

13

F23

RS

Interaction term in the tensor polynomial theory

14

F31

RS

Interaction term in the tensor polynomial theory

FTOPT=4

Maximum strain failure theory

3

XT

RS

Allowable longitudinal strain in tension

4

XC

RS

Allowable longitudinal strain in compression

5

YT

RS

Allowable lateral strain in tension

6

YC

RS

Allowable lateral strain in compression

7

ZT

RS

Allowable transverse strain in tension

8

ZC

RS

Allowable transverse strain in compression

9

SXY

RS

Allowable shear strain in the xy-plane

10

SYZ

RS

Allowable shear strain in the yz-plane

11

SZX

RS

Allowable shear strain in the zx-plane

FTOPT=5

Maximum stress failure theory

3

XT

RS

Allowable longitudinal stress in tension

4

XC

RS

Allowable longitudinal stress in compression

5

YT

RS

Allowable lateral stress in tension

6

YC

RS

Allowable lateral stress in compression

7

ZT

RS

Allowable transverse stress in tension

8

ZC

RS

Allowable transverse stress in compression

9

SXY

RS

Allowable shear stress in the xy-plane

DMAP Programmer’s Guide

4-159

Chapter 4

Word

Data Block Descriptions F-M

Name

Type

Description

10

SYZ

RS

Allowable shear stress in the yz-plane

11

SZX

RS

Allowable shear stress in the zx-plane

FTOPT=6

Maximum transverse shear stress failure theory

3

SXZ

RS

Allowable shear stress in the xz-plane

4

SYZ

RS

Allowable shear stress in the yz-plane

Words 2 thru the last word of the selected option repeat until -1 is reached

Record – MATG (8310,83,403) Word

Name

Type

Description

1

MID

I

Material identification number

2

IDMEM

I

ID of MAT1

3

BEHAV

I

Behavior type (not used)

4

TABLD

I

ID of TABLES1

5

TABLUi

I

ID of TABLES1 (I=1 to 10)

15

YPRS

RS

Initial yield pressure

16

EPL

RS

Tensile modulus

17

GPL

RS

Transverse shear modulus

18

GAP

RS

Initial gap (not used)

19

TABYPRS

I

ID of TABLES1 (not used)

20

TABEPL

I

ID of TABLES1 (not used)

21

TABGPL

I

ID of TABLES1 (not used)

22

TABGAP

I

ID of TABLES1 (not used)

Record – MATHE(7910,79,596) MATHE format for Mooney-Rivlin (default) model (Model = Mooney in MATHE bulk entry): Word 1

4-160

Name MID

DMAP Programmer’s Guide

Type I

Description Material identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

MODEL

I

3

UNDEF

None

4

K

RS

Bulk Modulus

5

RHO

RS

Mass density

6

TEXP

RS

Coefficient of thermal expansion

7

TREF

RS

Reference temperature (not used)

8

GE

RS

Structural damping (not used)

9

C10

RS

Material constant

10

C01

RS

Material constant

11

UNDEF

None

12

TAB1

I

Table ID (not used)

13

TAB2

I

Table ID (not used)

14

TAB3

I

Table ID (not used)

15

TAB4

I

Table ID (not used)

16

TABD

I

Table ID (not used)

17

C20

RS

Material constant

18

C11

RS

Material constant

19

C02

RS

Material constant

20

C30

RS

Material constant

21

C21

RS

Material constant

22

C12

RS

Material constant

23

C03

RS

Material constant

24

-1

I

Delimiter

MODEL = 1 for Mooney-Rivlin model

MATHE format for Ogden model (Model = Ogden in MATHE bulk entry): Word 1

Name MID

Type I

Description Material identification number

DMAP Programmer’s Guide

4-161

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

2

MODEL

I

MODEL = 2 for Ogden model

3

NOT

I

Curve fitting terms (not used)

4

K

RS

Bulk Modulus

5

RHO

RS

Mass density

6

TEXP

RS

Coefficient of thermal expansion

7

TREF

RS

Reference temperature (not used)

8

GE

RS

Structural damping (not used)

9

MU1

RS

Coefficient

10

ALPHA1

RS

Coefficient

11

BETA1

None

Coefficient

12

TAB1

I

Table ID (not used)

13

TAB2

I

Table ID (not used)

14

TAB3

I

Table ID (not used)

15

TAB4

I

Table ID (not used)

16

TABD

I

Table ID (not used)

17

MU2

RS

Coefficient

18

ALPHA2

RS

Coefficient

19

BETA2

RS

Coefficient

20

MU3

RS

Coefficient

21

ALPHA3

RS

Coefficient

22

BETA3

RS

Coefficient

23

MU4

RS

Coefficient

24

ALPHA4

RS

Coefficient

25

BETA4

RS

Coefficient

26

MU5

RS

Coefficient

27

ALPHA5

RS

Coefficient

4-162

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

28

BETA5

RS

Coefficient

29

MU6

RS

Coefficient

30

ALPHA6

RS

Coefficient

31

BETA6

RS

Coefficient

32

MU7

RS

Coefficient

33

ALPHA7

RS

Coefficient

34

BETA7

RS

Coefficient

35

MU8

RS

Coefficient

36

ALPHA8

RS

Coefficient

37

BETA8

RS

Coefficient

38

MU9

RS

Coefficient

39

ALPHA9

RS

Coefficient

40

BETA9

RS

Coefficient

41

-1

I

Delimiter

MATHE format for Hyperfoam model (Model = Foam in MATHE bulk entry): Name

Word

Type

Description

1

MID

I

Material identification number

2

MODEL

I

MODEL = 3 for Hyperfoam model

3

NOT

I

Curve fitting terms (not used)

4

K

RS

Bulk Modulus

5

RHO

RS

Mass density

6

TEXP

RS

Coefficient of thermal expansion

7

TREF

RS

Reference temperature (not used)

8

GE

RS

Structural damping (not used)

9

MU1

RS

Coefficient

10

ALPHA1

RS

Coefficient

DMAP Programmer’s Guide

4-163

Chapter 4

Word

Data Block Descriptions F-M

Name

Type

Description

11

BETA1

None

Coefficient

12

TAB1

I

Table ID (not used)

13

TAB2

I

Table ID (not used)

14

TAB3

I

Table ID (not used)

15

TAB4

I

Table ID (not used)

16

TABD

I

Table ID (not used)

17

MU2

RS

Coefficient

18

ALPHA2

RS

Coefficient

19

BETA2

RS

Coefficient

20

MU3

RS

Coefficient

21

ALPHA3

RS

Coefficient

22

BETA3

RS

Coefficient

23

MU4

RS

Coefficient

24

ALPHA4

RS

Coefficient

25

BETA4

RS

Coefficient

26

MU5

RS

Coefficient

27

ALPHA5

RS

Coefficient

28

BETA5

RS

Coefficient

29

MU6

RS

Coefficient

30

ALPHA6

RS

Coefficient

31

BETA6

RS

Coefficient

32

MU7

RS

Coefficient

33

ALPHA7

RS

Coefficient

34

BETA7

RS

Coefficient

35

MU8

RS

Coefficient

36

ALPHA8

RS

Coefficient

4-164

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

37

BETA8

RS

Coefficient

38

MU9

RS

Coefficient

39

ALPHA9

RS

Coefficient

40

BETA9

RS

Coefficient

41

-1

I

Delimiter

MATHE format for Arruda-Boyce model (Model = Aboyce in MATHE bulk entry): Name

Word

Type

Description

1

MID

I

Material identification number

2

MODEL

I

MODEL = 4 for Arruda-Boyce model

3

UNDEF

None

4

K

RS

Bulk Modulus

5

RHO

RS

Mass density

6

TEXP

RS

Coefficient of thermal expansion

7

TREF

RS

Reference temperature (not used)

8

GE

RS

Structural damping (not used)

9

NKT

RS

Material constant

10

N

RS

Material constant

11

UNDEF

None

12

TAB1

I

Table ID (not used)

13

TAB2

I

Table ID (not used)

14

TAB3

I

Table ID (not used)

15

TAB4

I

Table ID (not used)

16

TABD

I

Table ID (not used)

17

-1

I

Delimiter

MATHE format for Sussman-Bathe model (Model=Sussbat in MATHE bulk entry):

DMAP Programmer’s Guide

4-165

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

1

MID

I

Material identification number

2

MODEL

I

MODEL = 5 for Sussman-Bathe model

3

UNDEF

None

4

K

RS

Bulk Modulus

5

RHO

RS

Mass density

6

TEXP

RS

Coefficient of thermal expansion

7

TREF

RS

Reference temperature (not used)

8

GE

RS

Structural damping (not used)

9

TAB1

I

Table ID

10

SSTYPE

I

Type of stress-strain data entered in TAB1

11

RELERR

RS

Relative error

12

UNDEF(5)

None

17

-1

I

Delimiter

Record – MATHEM(3501,35,977) Name

Word

Type

Description

1

MID

I

Material identification number

2

R

RS

Material constant of Ogden-Roxburgh model for Mullins effect

3

M

RS

Material constant of Ogden-Roxburgh model for Mullins effect

4

HGEN

RS

Fraction of energy dissipated by Mullins effect model

5

UNDEF(4)

None

Record – MATHEV(3601,36,976) Word 1

4-166

Name MID

DMAP Programmer’s Guide

Type I

Description Material identification number

Data Block Descriptions F-M

Name

Word

Type

Description

2

SHIFT

I

Time-temperature superposition shift law

3

C1

RS

Material constant for the WLF or Arrhenius shift functions

4

C2

RS

Material constant for the WLF or Arrhenius shift functions

5

TREF

RS

Reference temperature used by the WLF or Arrhenius shift functions

6

UNDEF(3)

None

9

BETA

RS

Beta factor for chain of the viscoelastic model

10

TAU

RS

Relaxation time for chain of the viscoelastic model

11

HGEN

RS

Fraction of energy dissipation that is considered as heat generation

12

USAGE

I

Usage of chain

Words 9 through 12 repeat until -1 occurs

Record – MATHP(4506,45,374) Name

Word

Type

Description

1

MID

I

Material identification number

2

A10

RS

Material constant related to distortional deformation

3

A01

RS

Material constant related to distortional deformation

4

D1

RS

Material constant related to volumetric deformation

5

RHO

RS

Mass density

6

ALPHA

RS

Coefficient of volumetric thermal expansion

7

TREF

RS

Reference temperature

8

GE

RS

Structural damping element coefficient

9

SF

I

???

10

NA

I

Order of the distortional strain energy polynomial function

DMAP Programmer’s Guide

4-167

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

11

ND

I

Order of the volumetric strain energy polynomial function

12

KP

RS

???

13

A20

RS

Material constant related to distortional deformation

14

A11

RS

Material constant related to distortional deformation

15

A02

RS

Material constant related to distortional deformation

16

D2

RS

Material constant related to volumetric deformation

17

A30

RS

Material constant related to distortional deformation

18

A21

RS

Material constant related to distortional deformation

19

A12

RS

Material constant related to distortional deformation

20

A03

RS

Material constant related to distortional deformation

21

D3

RS

Material constant related to volumetric deformation

22

A40

RS

Material constant related to distortional deformation

23

A31

RS

Material constant related to distortional deformation

24

A22

RS

Material constant related to distortional deformation

25

A13

RS

Material constant related to distortional deformation

26

A04

RS

Material constant related to distortional deformation

27

D4

RS

Material constant related to volumetric deformation

28

A50

RS

Material constant related to distortional deformation

4-168

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

29

A41

RS

Material constant related to distortional deformation

30

A32

RS

Material constant related to distortional deformation

31

A23

RS

Material constant related to distortional deformation

32

A14

RS

Material constant related to distortional deformation

33

A05

RS

Material constant related to distortional deformation

34

D5

RS

Material constant related to volumetric deformation

35

CONTFLG

I

Continuation flag

CONTFLG =1

With continuation

36

TAB1

I

TABLES1 identification number which defines tension/compression

37

TAB2

I

TABLES1 identification number which defines equibiaxial tension

38

TAB3

I

TABLES1 identification number which defines simple shear

39

TAB4

I

TABLES1 identification number which defines pure shear

40

UNDEF(3 )

None

43

TAB5

I

CONTFLG =0

TABLES1 identification number which defines volumetric compression

Without continuation

End CONTFLG

Record – MATS1(503,5,90) Word 1

Name MID

Type I

Description Material identification number

DMAP Programmer’s Guide

4-169

Data Block Descriptions F-M

Chapter 4

Name

Word

Type

Description

2

TID

I

TABLES1 or TABLEST entry identification number

3

TYPE

I

Type of material nonlinearity

4

H

RS

Work hardening slope

5

YF

I

Yield function criterion

6

HR

I

Hardening Rule

7

LIMIT1

RS

Initial yield point

8

LIMIT2

RS

Internal friction angle

9

UNDEF(3 )

None

Record – MATSMA(6001,60,990) Name

Word

Type

Description

1

MID

I

Material identification number

2

EM

RS

Young’s modulus for martensite phase

3

EA

RS

Young’s modulus for austenite phase}

4

NUM

RS

Poisson’s ratio for martensite

5

NUA

I

Poisson’s ratio for austenite

6

ETMAX

I

Maximum residual transformation strain

7

VTM0

RS

Initial volumetric fraction of martensite

8

RHO

RS

Mass density

9

AM

None

Mean coefficient of thermal expansion for martensite

10

AA

RS

Mean coefficient of thermal expansion for austenite

11

TREF

RS

Reference temperature for thermal expansion calculation

12

MS

RS

Temperature at which the transformation to martensite starts

13

MF

RS

Temperature at which the transformation to martensite is finished

4-170

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

14

AS

RS

Temperature at which the transformation to austenite starts

15

AF

RS

Temperature at which the transformation to austenite is finished

16

UNDEF

17

CM

RS

Slope of the martensite transformation conditions

18

CA

RS

Slope of the austenite transformation conditions

19

SIGMAR

RS

Martensite re-orientation yield property

20

CR

RS

Slope of the martensite re-orientation yield function

Record – MATT1(703,7,91) Word

Name

Type

Description

1

MID

I

Material identification number

2

TID(10)

I

TABLEMi entry identification numbers

12

UNDEF

None

Record – MATT2(803,8,102) Word

Name

Type

Description

1

MID

I

Material identification number

2

TID(15)

I

TABLEMi entry identification numbers

17

UNDEF

None

Record – MATT3(1503,15,189) Word

Name

Type

Description

1

MID

I

Material identification number

2

TID(15)

I

Entry identification numbers

DMAP Programmer’s Guide

4-171

Chapter 4

Data Block Descriptions F-M

Record – MATT4(2303,23,237) Word

Name

Type

Description

1

MID

I

Material identification number

2

TK

I

TABLEMi identification number for thermal conductivity

3

TCP

I

TABLEMi identification number for heat capacity per unit mass

4

UNDEF

None

5

TH

I

TABLEMi identification number for free convection heat transfer coefficient

6

TMU

I

TABLEMi identification number for dynamic viscosity

7

THGEN

I

TABLEMi identification number for heat generation with QVOL entries

Record – MATT5(2403,24,238) Word

Name

Type

Description

1

MID

I

Material identification number

2

TK(6)

I

TABLEMi identification numbers for thermal conductivity

8

TCP

I

TABLEMi identification number for heat capacity per unit mass

9

UNDEF

None

10

THGEN

I

TABLEMi identification number for heat generation with QVOL entries

Record – MATT8(903,9,336) Word

Name

Type

1

MID

I

2

TID(9)

I

11

UNDEF

None

12

TID(7)

I

4-172

DMAP Programmer’s Guide

Description

TABLEMi entry identification numbers

TABLEMi entry identification numbers

Data Block Descriptions F-M

Word 19

Name UNDEF

Type

Description

None

Record – MATT9(2703,27,301) Word

Name

Type

Description

1

MID

I

Material identification number

2

TC(21)

I

TABLEMi identification numbers for material property matrix

23

TRHO

I

TABLEMi identification number for mass density

24

TA(6)

I

TABLEMi identification numbers for thermal expansion coefficients

30

UNDEF

None

31

TGE

I

32

UNDEF(4 )

None

TABLEMi identification number for structural damping coefficient

Record – MATT11(3303,33,988) Solid orthotropic material temperature dependence. Defines the temperature dependent material property for a 3-D orthotropic material for isoparametric solid elements. Word

Name

Type

Description

1

MID

I

Material identification number

2

TE1

I

TABLEMi ID for modulus of elasticity in the 1-direction

3

TE2

I

TABLEMi ID for modulus of elasticity in the 2-direction

4

TE3

I

TABLEMi ID for modulus of elasticity in the 3-direction

5

TNU12

I

TABLEMi ID for Poisson’s ratio (2/1 for uniaxial loading in the 1-direction)

6

TNU13

I

TABLEMi ID for Poisson’s ratio (3/1 for uniaxial loading in the 1-direction)

DMAP Programmer’s Guide

4-173

Chapter 4

Word

Data Block Descriptions F-M

Name

Type

Description

7

TNU23

I

TABLEMi ID for Poisson’s ratio (3/2 for uniaxial loading in the 2-direction)

8

TRHO

I

TABLEMi ID for mass density

9

TG12

I

TABLEMi ID for shear modulus in 1–2 plane

10

TG13

I

TABLEMi ID for shear modulus in 1–3 plane

11

TG23

I

TABLEMi ID for shear modulus in 2–3 plane

12

TA1

I

TABLEMi ID for thermal expansion coefficient in the 1-direction

13

TA2

I

TABLEMi ID for thermal expansion coefficient in the 2-direction

14

TA3

I

TABLEMi ID for thermal expansion coefficient in the 3-direction

15

UNDEF

None

16

TGE

RS

17

UNDEF(16)

None

TABLEMi ID for structural damping coefficient

Record – MATTC(2008,20,249) Word

Name

Type

Description

1

MID

I

Material identification number

2

TID(6)

I

TABLEMi identification numbers for creep coefficients

Record – MATVE(3701,37,975) Word

Name

Type

Description

1

MID

I

Material identification number

2

GFUNC

I

TABVE ID for shear modulus relaxation function

3

KFUNC

I

TABVE ID for bulk modulus relaxation function

4

RHO

RS

Mass density

5

ALPHA

RS

Coefficient of thermal expansion

4-174

DMAP Programmer’s Guide

Data Block Descriptions F-M

Name

Word

Type

Description

6

UNDEF(3)

None

9

SHIFT

I

Time-temperature superposition shift law

10

C1

RS

Material constant for the WLF or Arrhenius shift functions

11

C2

RS

Material constant for the WLF or Arrhenius shift functions

12

T0

RS

Reference temperature used by the WLF or Arrhenius shift functions

13

UNDEF(4)

None

Record – NLPARM(3003,30,286) Name

Word

Type

Description

1

SID

I

Set identification number

2

NINC

I

Number of increments

3

DT

RS

Incremental time interval for creep analysis

4

KMETHOD

I

Method for controlling stiffness updates

5

KSTEP

I

Number of iterations before the stiffness update

6

MAXITER

I

Limit on number of iterations for each load increment

7

CONV

I

Flags to select convergence criteria

8

INTOUT

I

Intermediate output flag

9

EPSU

RS

Error tolerance for displacement U criterion

10

EPSP

RS

Error tolerance for displacement P criterion

11

EPSW

RS

Error tolerance for displacement W criterion

12

MAXDIV

I

Limit on probable divergence conditions

13

MAXQN

I

Maximum number of quasi-Newton correction vectors

14

MAXLS

I

Maximum number of line searches

15

FSTRESS

RS

Fraction of effective stress

DMAP Programmer’s Guide

4-175

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

16

LSTOL

RS

Line search tolerance

17

MAXBIS

I

Maximum number of bisections

18

MAXR

RS

Maximum ratio for the adjusted arc-length increment

19

RTOLB

RS

Maximum value of incremental rotation

Record – NLPCI(3104,32,350) Name

Word

Type

Description

1

SID

I

Set identification number

2

TYPE

CHAR4

Constraint type

3

MINALR

RS

Minimum allowable arc-length adjustment ratio

4

MAXALR

RS

Maximum allowable arc-length adjustment ratio

5

SCALE

RS

Scale factor (w) for controlling the loading contribution

6

UNDEF

None

7

DESITER

I

Desired number of iterations for convergence

8

MXINC

I

Maximum number of controlled increment steps

Record – RADBND(9002,90,410) Word

Name

Type

Description

1

NUMBER

I

Number of radiation wave bands

2

PLANCK2

RS

Planck’s second radiation constant

3

LAMBDA

RS

Highest wavelength of the i-th wave band

Word 3 repeats until End of Record

Record – RADM(8802,88,413) Word 1

4-176

Name NUMBER(C)

DMAP Programmer’s Guide

Type I

Description Number of emissivities including absorptivity

Data Block Descriptions F-M

Name

Word

Type

Description

2

MID

I

Material identification number

3

EMISI

RS

Surface emissivity at wavelength LAMBDAi

Word 3 repeats NUMBER times Words 2 through 3 repeat until End of Record

Record – RADMT(8902,89,423) Name

Word

Type

Description

1

NUMBER(C)

I

Number of emissivities

2

MID

I

Material identification number

3

TEMISI

I

TABLEMi ID for surface emissivity

Word 3 repeats NUMBER times Words 2 through 3 repeat until End of Record

Record – TSTEPNL(3103,31,337) Name

Word

Type

Description

1

SID

I

Set identification number

2

NDT

I

Number of time steps of value DT

3

DT

RS

Time increment

4

NO

I

Time step interval for output

5

METHOD

I

Method for dynamic matrix update

6

KSTEP

I

Time step interval or number of converged bisections

7

MAXITER

I

Limit on number of iterations

8

CONV

I

Flags to select convergence criteria

9

EPSU

RS

Error tolerance for displacement U criterion

10

EPSP

RS

Error tolerance for displacement P criterion

11

EPSW

RS

Error tolerance for displacement W criterion

DMAP Programmer’s Guide

4-177

Chapter 4

Data Block Descriptions F-M

Name

Word

Type

Description

12

MAXDIV

I

Limit on probable divergence conditions

13

MAXQN

I

Maximum number of quasi-Newton correction vectors

14

MAXLS

I

Maximum number of line searches

15

FSTRESS

RS

Fraction of effective stress

16

MAXBIS

I

Maximum number of bisections

17

ADJUST

I

Time step skip factor for automatic time step adjustment

18

MSTEP

I

Number of steps to obtain the dominant period response

19

RB

RS

Define bounds for maintaining the same time step

20

MAXR

RS

Maximum ratio for the adjusted arc-length increment

21

UTOL

RS

Tolerance on displacement or temperature increment

22

RTOLB

RS

Maximum value of incremental rotation

Record – TRAILER Word 1

4-178

Name BIT(6)

DMAP Programmer’s Guide

Type I

Description Record presence trailer words

Chapter

5

Data Block Descriptions O-V

•

OBC

•

OMSEO

•

OBJTAB

•

OPG

•

OEE

•

OPTPRM

•

OEF

•

OQG

•

OES

•

OUG

•

OGF

•

R1MAP

•

OGK

•

R1TAB

•

OGS

•

RESP12

•

OMECON

•

SEMAP

•

OMEOSC

•

SET

•

OMKEC

•

SIL

•

OMKEO

•

TOL

•

OMSEC

•

VIEWTB

5.1 OBC Output contact pressure and traction results For SOL 101, SOL 601,106, SOL 601,129 and SOL 701.

Record – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name, for example, OBC1

DMAP Programmer’s Guide

5-1

Chapter 5

Data Block Descriptions O-V

Record – IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10* Approach Code

2

TCODE(C)

I

Table code, 62

3

UNDEF

None

4

SUBCASE

I

TCODE=1

SORT1

ACODE=01

SOL 101 Linear Statics

5

I

LOADSET

ACODE=10 5

Load set or zero

601 & 701 Nonlinear TIME

RS

Time Step

End ACODE TCODE=2 5

SORT2 EKEY

I

6

UNDEF(2)

none

8

LOADSET

I

Load set or zero

9

FCODE

I

1

10

NUMWDE

I

Number of words per entry in DATA record

11-50

UNDEF

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Device code + 10 * point identification number

End TCODE

Record – DATA Word

Name

TCODE=1 1

5-2

Type

Description

SORT1 EKEY

DMAP Programmer’s Guide

I

Device code + 10 * point identification number

Data Block Descriptions O-V

Name

Word

Type

Description

TCODE=2

SORT2

ACODE=01

SOL 101 Linear Statics

1

LOADSET

ACODE=10 1

I

Load set or zero

601 & 701 Nonlinear TIME

RS

Time Step

2

P

RS

Contact Pressure

3

T1

RS

Contact tangential traction in direction X (Base C.S.)

4

T2

RS

Contact tangential traction in direction Y (Base C.S.)

5

T3

RS

Contact tangential traction in direction Z (Base C.S.)

End ACODE End TCODE

Repeat word 1-5 for each grid point.

Record – TRAILER Word 1

Name UNDEF(6 )

Type

Description

None

Notes: 1. Contact results are grid point based results. 2. Contact tangential traction is expressed as a vector data (magnitude and direction) in X, Y and Z components of Basic Coordinate System. 3. SORT2 is supported only for SOL 101 Linear Statics.

5.2 OBG Output glue normal and in-plane tractions for SOL 101, SOL 103 and SOL 105. SORT1 and SORT2 formats are supported.

DMAP Programmer’s Guide

5-3

Chapter 5

Data Block Descriptions O-V

Record – HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name, for example, OBG1

Record – IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10* Approach Code

2

TCODE(C)

I

Table code (66 for Glue tractions)

3

UNDEF

None

4

SUBCASE

I

TCODE=1

SORT1

ACODE=01

Statics

5

LSDVMN

I

6

UNDEF(2)

None

ACODE=02

Load set number

Real Eigenvalues

5

MODE

I

Mode number

6

EIGN

RS

Eigenvalue

7

MODECYCL

RS

Mode or cycle

ACODE=03

Differential stiffness 0

5

LSDVMN

I

6

UNDEF(2)

None

ACODE=04

Differential stiffness 1

5

LSDVMN

I

6

UNDEF(2)

None

Load set number

Frequency

ACODE=05 5

FREQ

RS

6

UNDEF(2)

None

ACODE=06

5-4

Load set number

DMAP Programmer’s Guide

Transient

Frequency

Data Block Descriptions O-V

Word

Name

Type

5

TIME

RS

6

UNDEF(2)

None

ACODE=07

Description Time step

Buckling Phase 0 (pre-buckling)

5

LSDVMN

I

6

UNDEF(2)

None

ACODE=08

Load set number

Buckling Phase 1 (post-buckling)

5

LSDVMN

I

Mode number

6

EIGN

RS

Eigenvalue

7

UNDEF

None

ACODE=09

Complex eigenvalues

5

MODE

I

Mode

6

EIGR

RS

Eigenvalue (real)

7

EIGI

RS

Eigenvalue (imaginary)

ACODE=10

Nonlinear statics

5

LFTSFQ

RS

6

UNDEF(2)

None

ACODE=11

Time step

Old geometric nonlinear statics

5

LSDVMN

I

6

UNDEF(2)

None

ACODE=12

Load set number

CONTRAN (may appear as ACODE = 6)

5

TIME

RS

6

UNDEF(2)

None

Time

End ACODE TCODE=2

SORT2

5

LSDVMN

I

6

UNDEF(2)

None

Load set, mode number

DMAP Programmer’s Guide

5-5

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

End TCODE 8

LSDVMN

I

Load set

9

FCODE

I

Format code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF

None

12

PID

I

13

UNDEF(38)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Physical property identification number

Record – DATA Name

Word TCODE=1 1

Type

Description

SORT1 EKEY

I

Device code + 10 * point identification number

TCODE=2

SORT2

ACODE=01

SOL 101 Linear Statics

1

LOADSET

I

Load set or zero

2

P

RS

Glue normal traction

3

T1

RS

Glue tangential traction in direction X (Base C.S.)

4

T2

RS

Glue tangential traction in direction Y (Base C.S.)

5

T3

RS

Glue tangential traction in direction Z (Base C.S.)

End ACODE End TCODE

Repeat word 1-5 for each grid point.

5-6

DMAP Programmer’s Guide

Data Block Descriptions O-V

Record – TRAILER Name

Word 1

Type

Description

None

UNDEF(6)

Notes: 1. Glue results are grid point based results. 2. Glue tangential traction is expressed as a vector data (magnitude and direction) in X, Y and Z components of Basic Coordinate System.

5.3 OBJTAB Design objective table OBJTAB is defined for a given analysis type and superelement and contains objective attributes with retained response identification numbers.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – REPEAT Word

Name

Type

Description

1

IRID

I

Response identification number

2

RTYPE1

I

Type of response: 1 or 2

3

RTYPE2

I

Type of response: 1 or 2

4

MINMAX

I

Minimum/maximum flag: -1=minimum and 1=maximum

5

SEID

I

Superelement identification number

6

SID

I

Subcase identification number

Record 2 – TRAILER Word 1

Name UNDEF(6 )

Type

Description

None

DMAP Programmer’s Guide

5-7

Chapter 5

Data Block Descriptions O-V

5.4 OCCORF Table of cross-correlation functions.

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code; always 4200

3

UNDEF

none

4

RANDID

I

RANDOM set identification number

5

DCODE

I

Device code +10*function number

6

RCROSSID

I

RCROSS identification number

7

UNDEF(2)

none

9

FCODE

I

Format Code

10

NUMWDE(C)

I

Length of entries in RECORD=DATA (always 3)

11

RTYPE1

CHAR4

Type of first response quantity

12

ID1

I

Element, grid or scalar point ID number

13

COMP1

I

Component code (item) ID number

14

RTYPE2

CHAR4

Type of second response quantity

15

ID2

I

Element, grid, or scalar point ID number

16

COMP2

I

Component code (item) ID number

17

CURID

I

Curve ID number

18

UNDEF(33)

none

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

5-8

DMAP Programmer’s Guide

Data Block Descriptions O-V

Record 2 – DATA Name

Word

Type

Description

1

FREQ

RS

Frequency (Hz)

2

CCORF

RS

Cross-correlation function

Record 3– TRAILER Name

Word

Type

Description

1

WORD1

I

Number of records

2

WORD2

I

Number of data values in record 2.

3

UNDEF(4)

none

5.5 OCPSDF Table of cross-power spectral density functions.

Record 0 – HEADER Word 1

Name

Type CHAR4

NAME(2)

Description Data block name

Record 1 – IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code; always 4100

3

UNDEF

none

4

RANDID

I

RANDOM set identification number

5

DCODE

I

Device code +10*function number

6

RCROSSID

I

RCROSS identification number

7

UNDEF(2)

none

9

FCODE

I

Format code

10

NUMWDE(C)

I

Length of entries in RECORD=DATA (always 3)

DMAP Programmer’s Guide

5-9

Chapter 5

Word

Data Block Descriptions O-V

Name

Type

Description

11

RTYPE1

CHAR4

Type of first response quantity

12

ID1

I

Element, grid or scalar point ID number

13

COMP1

I

Component code (item) ID number

14

RTYPE2

CHAR4

Type of second response quantity

15

ID2

I

Element, grid, or scalar point ID number

16

COMP2

I

Component code (item) ID number

17

CURID

I

Curve ID number

18

UNDEF(33)

none

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 – DATA Word

Name

Type

Description

1

FREQ

RS

Frequency (Hz)

2

CPSDFR

RS

Real part of cross-power spectral density function value

3

CPSDFI

RS

Imaginary part of cross-power spectral density function value

Record 3– TRAILER Word

Name

Type

Description

1

WORD1

I

Number of records

2

WORD2

I

Number of data values in record 2.

3

UNDEF(4)

none

5.6 OEE Output element energy (strain, kinetic, loss)

5-10

DMAP Programmer’s Guide

Data Block Descriptions O-V

Record 0 - HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Block Name

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*approach code

2

TCODE(C)

I

18 for strain, 36 for kinetic, and 37 for energy loss

3

ETOTAL

RS

Total strain energy of all elements in subcase/mode

4

SUBCASE

I

Subcase number

UNDEF

None

Not defined

ACODE,4 =0 5 ACODE,4 =01 5

Statics UNDEF

ACODE,4 =02 5

MODE

UNDEF

UNDEF

ACODE,4 =07

None

See word 8

None

See word 8

Frequency FREQ

RS

Frequency

Transient

ACODE,4 =06 5

Mode Number

Differential Stiffness

ACODE,4 =05 5

I Differential Stiffness

ACODE,4 =04 5

See word 8

Real Eigenvalues

ACODE,4 =03 5

None

TIME

RS

Time Step

Buckling 0 ( Pre buckling )

DMAP Programmer’s Guide

5-11

Chapter 5

Data Block Descriptions O-V

Name

Word 5

UNDEF

ACODE,4 =08 5 ACODE,4 =09

ACODE,4 =10

ACODE,4 =11

Mode Number

I

Mode Number

RS

Load factor

Geometric Nonlinear Statics UNDEF

ACODE,4 =12 5

I

Nonlinear Statics ( Sol 106 ) LOADFAC

5

See word 8

Complex Eigenvalues MODE

5

None

Description

Buckling 1 ( Post buckling ) MODE

5

Type

None

See word 8

CONTRAN ? ( Can appear as ACODE=6 ) TIME

RS

Time Step

6

ELNAME(2)

CHAR4

Element type name

8

LOADSET

I

Load set or zero

9

APROACH

I

Approach

10

NUMWDE

I

Number of words per entry in DATA record

11

CVALRES

I

C

12

ESUBT

RS

Subtotal of Strain Energy in the Set identification number

13

SETID

I

Set identification number Number

14

EIGENR

RS

Natural eigenvalue real part

15

EIGENI

RS

Natural eigenvalue imaginary part

16

FREQ

RS

Natural frequency

17

UNDEF

None

End ACODE,4

5-12

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

18

ETOTPOS

RS

Total positive energy

19

ETOTNEG

RS

Total negative energy

20

FCODE

I

Format Code 1 – Real 2 – Real/Imaginary 3 – Magnitude/Phase

21

ELTYPE

I

Element Type

22

THRESH

RS

Energy Threshold

23

UNDEF(28)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 - DATA Word

Name

TCODE,1 =1 1

Type

Description

Sort 1 EKEY

TCODE,1 =02

I Sort 2 - Swap with word 5 of IDENT

ACODE,4 =0 1

UNDEF

None

EKEY

I

EKEY

I

EKEY

I

Not defined

ACODE,4 =01 1 ACODE,4 =02 1 ACODE,4 =03 1 ACODE,4 =04

DMAP Programmer’s Guide

5-13

Chapter 5

Data Block Descriptions O-V

Name

Word 1

Type

Description

EKEY

I

FREQ

RS

Frequency

TIME

RS

Time step

EKEY

I

EKEY

I

EKEY

I

FQTS

RS

EKEY

I

EKEY

I

2

ENERGY

RS

Element Energy or Subtotal after all elements

3

PCT

RS

Percent of Total Energy

4

DEN

RS

Element Energy Density, or ’-1’ after all elements

ACODE,4 =05 1 ACODE,4 =06 1 ACODE,4 =07 1 ACODE,4 =08 1 ACODE,4 =09 1 ACODE,4 =10 1

Frequency or Time step

ACODE,4 =11 1 ACODE,4 =12 1 End ACODE,4 End TCODE,1

Real

TCODE,7=0 (Real) 1

ID

I

(depends on TCODE,1)

2

ENERGY

RS

Element Energy

5-14

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

3

PCT

RS

Percent of Total Energy

4

DEN

RS

Element Energy Density

1

ID

I

(depends on TCODE,1)

2

ENERGY.R

RS

Element Energy (real/mag part)

3

ENERGY.I

RS

Element Energy (imag/phase part)

4

PCT

RS

Percent of Total Energy

5

DEN

RS

Element Energy Density

1

ID

I

(depends on TCODE,1)

2

ENERGY.R

RS

Element Ave Energy (real/mag part)

3

ENERGY.I

RS

Element Ave Energy (imag/phase part)

4

ENERGY.R

RS

Element Amp Energy (real/mag part)

5

ENERGY.I

RS

Element Amp Energy (imag/phase part)

6

PCT

RS

Percent of Total Energy

7

DEN

RS

Element Energy Density

TCODE,7=1 (Real/Imaginary or Magnitude/Phase) CVALRES=1,2

CVALRES=4

End CVALRES End TCODE,7

Record 3- TRAILER Word 1

Name WORD1

Type I

Description Number of element types output

DMAP Programmer’s Guide

5-15

Data Block Descriptions O-V

Chapter 5

Name

Word 2

UNDEF(5 )

Type

Description

None

Notes: 1. Records are repeated for each element type having at least one element requested for output. They are also repeated for each subcase. 2. Device code: 1 = print 2 = plot 4 = punch 5 = print and punch, and so on 3. Approach code: 1 = statics 2 = reigen, 3=ds0 4 = ds1 5 = freq 6 = bkl0 7 = bkl 8 = ceigen 9 = pla 4. Nonexistent element energy densities are flagged by integer ’-1’ in the field.

5.7 OEF Table of element forces Also contains composite failure indices and analysis types (real and complex), and SORT1 and SORT2 formats.

Record - HEADER Word

Name

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

5-16

DMAP Programmer’s Guide

Description Data block name

Data Block Descriptions O-V

Name

Word 6

UNDEF(2 )

Type

Description

None

Record - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

ELTYPE(C)

I

Element type

4

SUBCASE

I

Subcase or Random identification number

TCODE,1 =1

SORT1 format

ACODE,4 =01

Statics

5

LOADID

I

6

UNDEF(2)

None

Load set identification number

ACODE,4 =02

Normal modes or buckling (real eigenvalues)

5

MODE

I

Mode number

6

EIGN

RS

Eigenvalue

7

UNDEF

None

ACODE,4 =03

Differential Stiffness 0

5

LOADID

I

6

UNDEF(2)

None

Load set identification number

ACODE,4 =04

Differential Stiffness 1

5

LOADID

I

6

UNDEF(2)

None

ACODE,4 =05

Frequency

5

FREQ

RS

6

UNDEF

None

7

RANDOM ID

I

ACODE,4 =06

Load set identification number

Frequency

Random identification number

Transient

DMAP Programmer’s Guide

5-17

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

5

TIME

RS

6

UNDEF(2)

None

ACODE,4 =07

Pre-buckling

5

LOADID

I

6

UNDEF(2)

None

Description Time step

Load set identification number

ACODE,4 =08

Post-buckling

5

LOADID

I

Load set identification number

6

EIGR

RS

Eigenvalue

7

RANDOM ID

I

Random identification number

ACODE,4 =09

Complex Eigenvalues

5

MODE

I

Mode number

6

EIGR

RS

Eigenvalue - real part

7

EIGI

RS

Eigenvalue - imaginary part

ACODE,4 =10

Nonlinear Statics

5

LOADSTEP

RS

6

UNDEF(2)

None

Load step

ACODE,4 =11

Geometric Nonlinear Statics

5

LOADID

I

6

UNDEF

None

7

RANDOM ID

I

Load set identification number

Random identification number

End ACODE,4 TCODE,1 =02

SORT2 format

5

LOADID

I

6

UNDEF(2)

None

Load set identification number

End TCODE,1 8

5-18

DLOADID

DMAP Programmer’s Guide

I

Dynamic load set or Random code identification number

Data Block Descriptions O-V

Name

Word

Type

Description

9

FCODE(C)

I

Format code

10

NUMWDE(C)

I

Number of words per entry

11

OCODE

I

12

PID (SOL 601 and 701 only)

I

13

UNDEF

None

14

Q4CSTR(C)

I

Corner Stress Flag

15

PLSLOC(C)

I

Ply stress/strain location

16

UNDEF(7)

None

23

THERMAL(C)

I

24

UNDEF(27)

None

51

TITLE(32)

CHAR4

Title character string (TITLE)

83

SUBTITLE(32)

CHAR4

Subtitle character string (SUBTITLE)

115

LABEL(32)

CHAR4

LABEL character string (LABEL)

Physical Property ID for SOL 601 & 701 only. UNDEF for all other SOLs

=1 for heat transfer and 0 otherwise

Record - DATA Name

Word

Type

TCODE,1 =1

SORT1 Format

1

I

EID

TCODE,1 =02

SORT2 Format

ACODE,4 =01

Statics

1

I

LOADID

Description

Element identification number

Load set identification number

ACODE,4 =02

Normal modes or buckling (real eigenvalues)

1

I

MODE

Mode number

ACODE,4 =03

Differential Stiffness 0

1

I

LOADID

ACODE,4 =04

Load set identification number

Differential Stiffness 1

DMAP Programmer’s Guide

5-19

Data Block Descriptions O-V

Chapter 5

Name

Word 1

LOADID

Type I

Load set identification number

ACODE,4 =05

Frequency

1

RS

FREQ

Frequency

ACODE,4 =06

Transient

1

RS

TIME

Time step

ACODE,4 =07

Pre-buckling

1

I

LOADID

Load set identification number

ACODE,4 =08

Post-buckling

1

I

LOADID

Description

Load set identification number

ACODE,4 =09

Complex Eigenvalues

1

I

MODE

Mode number

ACODE,4 =10

Nonlinear Statics

1

RS

LOADSTEP

Load step

ACODE,4 =11

Geometric Nonlinear Statics

1

I

LOADID

Load set identification number

End ACODE,4 End TCODE,1 Name

Word

Type

Description

THERMAL =1

Thermal data

NUMWDE =10

2-D and 3-D elements

2

NAME(2)

CHAR4

Element type

4

XGRAD

RS

x gradient or ’1’

5

YGRAD

RS

y gradient or ’1’

6

ZGRAD

RS

z gradient or ’1’

7

XFLUX

RS

x flux or ’1’

8

YFLUX

RS

y flux or ’1’

5-20

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

9

ZFLUX

RS

z flux or ’1’

10

ZED

I

zero

NUMWDE =8

(CHBDY) thermal 107,108,109

2

NAME(2)

CHAR4

Element name

4

FAPPLIED

RS

Applied load

5

FREECONV

RS

Free convection

6

FORCECON

RS

Forced convection

7

FRAD

RS

Radiation

8

FTOTAL

RS

Total

NUMWDE =2

conv elements

2

RS

FTOTAL

Total

NUMWDE =9

1-D elements; for example, CBEAM, CBEND, CTUBE

2

NAME(2)

CHAR4

Element type

4

XGRAD

RS

x gradient or ’1’

5

YGRAD

RS

y gradient or ’1’

6

ZGRAD

RS

z gradient or ’1’

7

XFLUX

RS

x flux or ’1’

8

YFLUX

RS

y flux or ’1’

9

ZFLUX

RS

z flux or ’1’

NUMWDE =58

VUHEXA 145 Thermal

2

PARENT

I

Parent C

3

VUGRID

I

VU Grid identification number

4

XGRAD

RS

x gradient or ’1’

5

YGRAD

RS

y gradient or ’1’

6

ZGRAD

RS

z gradient or ’1’

7

XFLUX

RS

x flux or ’1’

DMAP Programmer’s Guide

5-21

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

YFLUX

RS

y flux or ’1’

9

ZFLUX

RS

z flux or ’1’

Words 3 through 9 repeat 8 times NUMWDE =44

VUPENTA 146 Thermal

2

PARENT

I

Parent identification number

3

VUGRID

I

VU Grid identification number

4

XGRAD

RS

x gradient or ’1’

5

YGRAD

RS

y gradient or ’1’

6

ZGRAD

RS

z gradient or ’1’

7

XFLUX

RS

x flux or ’1’

8

YFLUX

RS

y flux or ’1’

9

ZFLUX

RS

z flux or ’1’

Words 3 through 9 repeat 6 times NUMWDE =30

VUTETRA 147 Thermal

2

PARENT

I

Parent identification number

3

VUGRID

I

VU Grid identification number

4

XGRAD

RS

x gradient or ’1’

5

YGRAD

RS

y gradient or ’1’

6

ZGRAD

RS

z gradient or ’1’

7

XFLUX

RS

x flux or ’1’

8

YFLUX

RS

y flux or ’1’

9

ZFLUX

RS

z flux or ’1’

Words 3 through 9 repeat 4 times NUMWDE =34

VUQUAD 189 Thermal

2

PARENT

I

Parent p-element identification number

3

COORD

I

Coordinate system identification number

5-22

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

4

ICORD

CHAR4

Flat/curved and so on

5

THETA

I

Material angle

6

UNDEF

None

7

VUGRID

I

VU Grid identification number

8

XGRAD

RS

x gradient or ’1’

9

YGRAD

RS

y gradient or ’1’

10

ZGRAD

RS

z gradient or ’1’

11

XFLUX

RS

x flux or ’1’

12

YFLUX

RS

y flux or ’1’

13

ZFLUX

RS

z flux or ’1’

Words 7 through 13 repeat 4 times NUMWDE =27

VUTRIA 190 Thermal

2

PARENT

I

Parent p-element identification number

3

COORD

I

Coordinate system identification number

4

ICORD

CHAR4

Flat/curved and so on

5

THETA

I

Material angle

6

UNDEF

None

7

VUGRID

I

VU Grid Id

8

XGRAD

RS

x gradient or ’1’

9

YGRAD

RS

y gradient or ’1’

10

ZGRAD

RS

z gradient or ’1’

11

XFLUX

RS

x flux or ’1’

12

YFLUX

RS

y flux or ’1’

13

ZFLUX

RS

z flux or ’1’

Words 7 through 13 repeat 3 times NUMWDE =18

VUBEAM 191 Thermal

DMAP Programmer’s Guide

5-23

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

PARENT

I

Parent p-element identification number

3

COORD

I

Coordinate system identification number

4

ICORD

CHAR4

Flat/curved and so on

5

VUGRID

I

VU Grid Id

6

XGRAD

RS

x gradient or ’1’

7

YGRAD

RS

y gradient or ’1’

8

ZGRAD

RS

z gradient or ’1’

9

XFLUX

RS

x flux or ’1’

10

YFLUX

RS

y flux or ’1’

11

ZFLUX

RS

z flux or ’1’

Words 5 through 11 repeat 2 times End NUMWDE Name

Word

Type

Description

THERMAL =00

Non-thermal element output

ELTYPE =01

Rod element (CROD)

TCODE,7 =0 or 2

Real or Random Response

2

AF

RS

Axial Force

3

TRQ

RS

Torque

TCODE,7 =1

Real/imaginary or magnitude/phase

2

AFR

RS

Axial Force - real/mag. part

3

AFI

RS

Axial Force - imag./phase part

4

TRQR

RS

Torque - real/mag. part

5

TRQI

RS

Torque - imag./phase part

End TCODE,7 ELTYPE =02

Beam element (CBEAM)

TCODE,7 =0 or 2

Real or Random Response

5-24

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

2

GRID

I

Grid point identification number

3

SD

RS

Station Distance divided by element’s length

4

BM1

RS

Bending moment plane 1

5

BM2

RS

Bending moment plane 2

6

TS1

RS

Shear Plane 1

7

TS2

RS

Shear Plane 2

8

AF

RS

Axial Force

9

TTRQ

RS

Total Torque

10

WTRQ

RS

Warping Torque

TCODE,7 =1

Real/imaginary or magnitude/phase

2

GRID

I

Grid point identification number

3

SD

RS

Station Distance divided by element’s length

4

BM1R

RS

Bending moment plane 1 - real/mag. part

5

BM2R

RS

Bending moment plane 2 - real/mag. part

6

TS1R

RS

Shear plane 1 - real/mag. part

7

TS2R

RS

Shear plane 2 - real/mag. part

8

AFR

RS

Axial force - real/mag. part

9

TTRQR

RS

Total torque - real/mag. part

10

WTRQR

RS

Warping torque - real/mag. part

11

BM1I

RS

Bending moment plane 1 - imag./phase part

12

BM2I

RS

Bending moment plane 2 - imag./phase part

13

TS1I

RS

Shear plane 1 - imag./phase part

14

TS2I

RS

Shear plane 2 - imag./phase part

15

AFI

RS

Axial force - imag./phase part

16

TTRQI

RS

Total torque - imag./phase part

17

WTRQI

RS

Warping torque - imag./phase part

DMAP Programmer’s Guide

5-25

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

End TCODE,7 Words 2 through max repeat 011 times ELTYPE =03

Tube element (CTUBE)

TCODE,7 =0 or 2

Real or Random Response

2

AF

RS

Axial Force

3

TRQ

RS

Torque

TCODE,7 =1

Real/imaginary or magnitude/phase

2

AFR

RS

Axial Force - real/mag. part

3

AFI

RS

Axial Force - imag./phase part

4

TRQR

RS

Torque - real/mag. part

5

TEQI

RS

Torque - imag./phase part

End TCODE,7 ELTYPE =04

Shear panel element (CSHEAR)

TCODE,7 =0 or 2

Real or Random Response

2

F41

RS

Force 4 to 1

3

F21

RS

Force 2 to 1

4

F12

RS

Force 1 to 2

5

F32

RS

Force 3 to 2

6

F23

RS

Force 2 to 3

7

F43

RS

Force 4 to 3

8

F34

RS

Force 3 to 4

9

F14

RS

Force 1 to 4

10

KF1

RS

Kick Force on 1

11

S12

RS

Shear 1 2

12

KF2

RS

Kick Force on 2

13

S23

RS

Shear 2 3

5-26

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

14

KF3

RS

Kick Force on 3

15

S34

RS

Shear 3 4

16

KF4

RS

Kick Force on 4

17

S41

RS

Shear 4 1

TCODE,7 =1

Real/imaginary or magnitude/phase

2

F41R

RS

Force 4 to 1 - real/mag. part

3

F21R

RS

Force 2 to 1 - real/mag. part

4

F12R

RS

Force 1 to 2 - real/mag. part

5

F32R

RS

Force 3 to 2 - real/mag. part

6

F23R

RS

Force 2 to 3 - real/mag. part

7

F43R

RS

Force 4 to 3 - real/mag. part

8

F34R

RS

Force 3 to 4 - real/mag. part

9

F14R

RS

Force 1 to 4 - real/mag. part

10

F41I

RS

Force 4 to 1 - imag./phase part

11

F21I

RS

Force 2 to 1 - imag./phase part

12

F12I

RS

Force 1 to 2 - imag./phase part

13

F32I

RS

Force 3 to 2 - imag./phase part

14

F23I

RS

Force 2 to 3 - imag./phase part

15

F43I

RS

Force 4 to 3 - imag./phase part

16

F34I

RS

Force 3 to 4 - imag./phase part

17

F14I

RS

Force 1 to 4 - imag./phase part

18

KF1R

RS

Kick Force on 1 - real/mag. part

19

S12R

RS

Shear 1 2 - real/mag. part

20

KF2R

RS

Kick Force on 2 - real/mag. part

21

S23R

RS

Shear 2 3 - real/mag. part

22

KF3R

RS

Kick Force on 3 - real/mag. part

DMAP Programmer’s Guide

5-27

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

23

S34R

RS

Shear 3 4 - real/mag. part

24

KF4R

RS

Kick Force on 4 - real/mag. part

25

S41R

RS

Shear 4 1 - real/mag. part

26

KF1I

RS

Kick Force on 1 - imag./phase part

27

S12I

RS

Shear 1 2 - imag./phase part

28

KF2I

RS

Kick Force on 2 - imag./phase part

29

S23I

RS

Shear 2 3 - imag./phase part

30

KF3I

RS

Kick Force on 3 - imag./phase part

31

S34I

RS

Shear 3 4 - imag./phase part

32

KF4I

RS

Kick Force on 4 - imag./phase part

33

S41I

RS

Shear 4 1 - imag./phase part

End TCODE,7 ELTYPE =05 2

FORCE1/FORCE2/MOMENT1/MOMENT2 (follower stiffness) UNDEF

ELTYPE =06 2

Unused UNDEF

ELTYPE =07 2 ELTYPE =08

None PLOADX1 (follower stiffness)

UNDEF

ELTYPE =09 2

None PLOAD4 (follower stiffness)

UNDEF

2

None

None PLOAD and PLOAD2 (follower stiffness)

UNDEF Word

Name

None Type

Description

ELTYPE =10

Rod element connection and property (CONROD)

TCODE,7 =0 or 2

Real or Random Response

5-28

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

2

AF

RS

Axial Force

3

TRQ

RS

Torque

TCODE,7 =1

Real/imaginary or magnitude/phase

2

AFR

RS

Axial Force - real/mag. part

3

AFI

RS

Axial Force - imag./phase part

4

TRQR

RS

Torque - real/mag. part

5

TRQI

RS

Torque - imag./phase part

End TCODE,7 ELTYPE =11

Scalar spring element (CELAS1)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1

Force

Real/imaginary or magnitude/phase

2

FR

RS

Force - real/mag. part

3

FI

RS

Force - imag./phase part

End TCODE,7 ELTYPE =12

Scalar spring element with properties (CELAS2)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1

Force

Real/imaginary or magnitude/phase

2

FR

RS

Force - real/mag. part

3

FI

RS

Force - imag./phase part

End TCODE,7 ELTYPE =13

Scalar spring element to scalar points only (CELAS3)

TCODE,7 =0 or 2

Real or Random Response

2

RS

TCODE,7 =1

F

Force

Real/imaginary or magnitude/phase

DMAP Programmer’s Guide

5-29

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

FR

RS

Force - real/mag. part

3

FI

RS

Force - imag./phase part

End TCODE,7 ELTYPE =14

Scalar spring element to scalar pts. only with prop. (CELAS4)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1

Force

Real/imaginary or magnitude/phase

2

FR

RS

Force - real/mag. part

3

FI

RS

Force - imag./phase part

End TCODE,7 ELTYPE =15 2

AEROT3 UNDEF

ELTYPE =16 2

AEROBEAM UNDEF

ELTYPE =17 2 ELTYPE =18

None Unused (Pre-V69 CQUAD2)

UNDEF

ELTYPE =19 2

None Unused (Pre-V69 CTRIA2)

UNDEF

2

None

None Unused (Pre-V69 CQUAD1)

UNDEF

None

Name

Word

Type

Description

ELTYPE =20

Scalar damper (CDAMP1)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1 2

5-30

Force

Real/imaginary or magnitude/phase FR

DMAP Programmer’s Guide

RS

Force

Data Block Descriptions O-V

Name

Word 3

FI

Type RS

Description Force

End TCODE,7 ELTYPE =21

Scalar damper with properties (CDAMP2)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1

Force

Real/imaginary or magnitude/phase

2

FR

RS

Force

3

FI

RS

Force

End TCODE,7 ELTYPE =22

Scalar damper to scalar points only (CDAMP3)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1

Force

Real/imaginary or magnitude/phase

2

FR

RS

Force

3

FI

RS

Force

End TCODE,7 ELTYPE =23

Scalar damper to scalar points only with prop (CDAMP4)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F

TCODE,7 =1

Force

Real/imaginary or magnitude/phase

2

FR

RS

Force

3

FI

RS

Force

End TCODE,7 ELTYPE =24

Viscous damper (CVISC)

TCODE,7 =1

Real/imaginary or magnitude/phase

2

AFR

RS

Axial Force - real/mag. part

DMAP Programmer’s Guide

5-31

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

3

AFI

RS

Axial Force - imag./phase part

4

TRQR

RS

Torque - real/mag. part

5

TRQI

RS

Torque - imag./phase part

TCODE,7 =0 or 2

Real or Random Response

2

AF

RS

Axial Force

3

TRQ

RS

Torque

ELTYPE =25 2

Scalar mass (CMASS1) UNDEF

ELTYPE =26 2

Scalar mass with properties (CMASS2) UNDEF

ELTYPE =27 2 ELTYPE =28

ELTYPE =29

ELTYPE =30

Type

Description

Concentrated mass element - rigid body form (CONM2) UNDEF

ELTYPE =31

None Dummy plot element (PLOTEL)

UNDEF

ELTYPE =32 2

None

Name

Word

2

None Concentrated mass element - general form (CONM1)

UNDEF

2

None Scalar mass to scalar pts. only with properties (CMASS4)

UNDEF

2

None Scalar mass to scalar pts. only (CMASS3)

UNDEF

2

None

None Unused

UNDEF

None

ELTYPE =33

Quadrilateral plate element (CQUAD4)

TCODE,7 =0 or 2

Real or Random Response

2

RS

5-32

MX

DMAP Programmer’s Guide

Membrane in x

Data Block Descriptions O-V

Name

Word

Type

Description

3

MY

RS

Membrane in y

4

MXY

RS

Membrane in xy

5

BMX

RS

Bending in x

6

BMY

RS

Bending in y

7

BMXY

RS

Bending in xy

8

TX

RS

Transverse Shear in x

9

TY

RS

Transverse Shear in y

TCODE,7 =1

Real/imaginary or magnitude/phase

2

MXR

RS

Membrane in x - real/mag. part

3

MYR

RS

Membrane in y - real/mag. part

4

MXYR

RS

Membrane in xy - real/mag. part

5

BMXR

RS

Bending in x - real/mag. part

6

BMYR

RS

Bending in y - real/mag. part

7

BMXYR

RS

Bending in xy - real/mag. part

8

TXR

RS

Transverse Shear in x - real/mag. part

9

TYR

RS

Transverse Shear in y - real/mag. part

10

MXI

RS

Membrane in x - imag./phase part

11

MYI

RS

Membrane in y - imag./phase part

12

MXYI

RS

Membrane in xy - imag./phase part

13

BMXI

RS

Bending in x - imag./phase part

14

BMYI

RS

Bending in y - imag./phase part

15

BMXYI

RS

Bending in xy - imag./phase part

16

TXI

RS

Transverse Shear in x - imag./phase part

17

TYI

RS

Transverse Shear in y - imag./phase part

End TCODE,7 ELTYPE =34

Simple beam element (CBAR and see also ELTYPE=100)

DMAP Programmer’s Guide

5-33

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

TCODE,7 =0 or 2

Real or Random Response

2

BM1A

RS

Bending moment end A plane 1

3

BM2A

RS

Bending moment end A plane 2

4

BM1B

RS

Bending moment end B plane 1

5

BM2B

RS

Bending moment end B plane 2

6

TS1

RS

Shear plane 1

7

TS2

RS

Shear plane 2

8

AF

RS

Axial Force

9

TRQ

RS

Torque

TCODE,7 =1

Real/imaginary or magnitude/phase

2

BM1AR

RS

Bending moment end A plane 1 - real part

3

BM2AR

RS

Bending moment end A plane 2 - real part

4

BM1BR

RS

Bending moment end B plane 1 - real part

5

BM2BR

RS

Bending moment end B plane 2 - real part

6

TS1R

RS

Shear plane 1 - real part

7

TS2R

RS

Shear plane 2 - real part

8

AFR

RS

Axial force - real part

9

TRQR

RS

Torque - real part

10

BM1AI

RS

Bending moment end A plane 1 - imaginary part

11

BM2AI

RS

Bending moment end A plane 2 - imaginary part

12

BM1BI

RS

Bending moment end B plane 1 - imaginary part

13

BM2BI

RS

Bending moment end B plane 2 - imaginary part

14

TS1I

RS

Shear plane 1 - imaginary part

15

TS2I

RS

Shear plane 2 - imaginary part

5-34

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

16

AFI

RS

Axial Force - imaginary part

17

TRQI

RS

Torque - imaginary part

End TCODE,7 ELTYPE =35

Axisymmetric shell element (CCONEAX)

2

HOPA

RS

Harmonic or point angle

3

BMU

RS

Bending Moment u

4

BMV

RS

Bending Moment v

5

TM

RS

Twisting Moment

6

SU

RS

Shear u

7

SV

RS

Shear v

ELTYPE =36 2

Unused (Pre-V69 CTRIARG) UNDEF

ELTYPE =37 2

None Unused (Pre-V69 CTRAPRG)

UNDEF

None

ELTYPE =38

Gap element (CGAP)

TCODE,7 =0

Real

2

FX

RS

Comp. Force in x

3

SFY

RS

Shear Force in y

4

SFZ

RS

Shear Force in z

5

U

RS

Axial Disp in u

6

V

RS

Shear Disp in v

7

W

RS

Shear Disp in w

8

SV

RS

Slip Disp in v

9

SW

RS

Slip Disp in w

TCODE,7 =1 2

Real/imaginary or magnitude/phase FX

RS

Comp. Force in x

DMAP Programmer’s Guide

5-35

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

3

SFY

RS

Shear Force in y

4

SFZ

RS

Shear Force in z

5

U

RS

Axial Disp in u

6

V

RS

Shear Disp in v

7

W

RS

Shear Disp in w

8

SV

RS

Slip Disp in v

9

SW

RS

Slip Disp in w

End TCODE,7 ELTYPE =39

Acoustics - Tetra

2

AXR

RS

Acceleration in x (real)

3

AYR

RS

Acceleration in y (real)

4

AZR

RS

Acceleration in z (real)

5

VXR

RS

Velocity in x (real)

6

VYR

RS

Velocity in y (real)

7

VXR

RS

Velocity in z (real)

8

AXI

RS

Acceleration in x (imaginary)

9

AYI

RS

Acceleration in y (imaginary)

10

AZI

RS

Acceleration in z (imaginary)

11

VXI

RS

Velocity in x (imaginary)

12

VYI

RS

Velocity in y (imaginary)

13

VXI

RS

Velocity in z (imaginary)

14

DB

RS

Pressure

Name

Word ELTYPE =40

Type

Description

Rod type spring and damper (CBUSH1D)

2

FE

RS

Element Force

3

UE

RS

Axial Displacement

5-36

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

4

VE

RS

Axial Velocity*

5

AS

RS

Axial Stress*

6

AE

RS

Axial Strain*

7

EP

RS

Plastic Strain*

8

FAIL

I

Failed Element Flag

ELTYPE =41 2

Unused (Pre-V69 CHEXA1) UNDEF

ELTYPE =42 2

Unused (Pre-V69 CHEXA2) UNDEF

ELTYPE =43 2 ELTYPE =44

ELTYPE =45

ELTYPE =46

ELTYPE =47

ELTYPE =48

ELTYPE =49

Name

ELTYPE =50 2

None Fluid element with 4 points (CAXIF4)

UNDEF Word

None Fluid element with 3 points (CAXIF3)

UNDEF

2

None Fluid element with 2 points (CAXIF2)

UNDEF

2

None Cflmass

UNDEF

2

None Fluid element with 4 points (CFLUID4)

UNDEF

2

None Fluid element with 3 points (CFLUID3)

UNDEF

2

None Fluid element with 2 points (CFLUID2)

UNDEF

2

None

None Type

Description

Three-point slot element (CSLOT3) UNDEF

None

DMAP Programmer’s Guide

5-37

Data Block Descriptions O-V

Chapter 5

Name

Word ELTYPE =51 2 ELTYPE =52

ELTYPE =53

None Axisymmetric triangular element (CTRIAX6)

UNDEF

ELTYPE =54 2

None Heat transfer plot element for CHBDYG and CHBDYP

UNDEF

2

Description

Four-point slot element (CSLOT4) UNDEF

2

Type

None Unused (Pre-V69 CTRIM6)

UNDEF

None

ELTYPE =55

Three-point dummy element (CDUM3)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =56

Four-point dummy element (CDUM4)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =57

Five-point dummy element (CDUM5)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

5-38

DMAP Programmer’s Guide

User defined

Real/imaginary or magnitude/phase

Data Block Descriptions O-V

Name

Word

Type

Description

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =58

Six-point dummy element (CDUM6)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =59

Seven-point dummy element (CDUM7)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 Name

Word

Type

Description

ELTYPE =60

Two-dimensional crack tip element (CRAC2D or CDUM8)

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =61

Three-dimensional crack tip element (CRAC3D or CDUM9)

DMAP Programmer’s Guide

5-39

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

TCODE,7 =0 or 2

Real or Random Response

2

RS

F(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

FR(9)

RS

User defined - real/mag.

11

FI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =62 2

Unused (Pre-V69 CQDMEM1) UNDEF

ELTYPE =63 2

None Unused (Pre-V69 CQDMEM2)

UNDEF

ELTYPE =64

None Curved quadrilateral shell element (CQUAD8)

2

TERM

CHAR4

Character string "CEN/"

3

GRID

I

Number of active grids or corner grid identification number

TCODE,7 =0 or 2

Real or Random Response

4

MX

RS

Membrane force in x

5

MY

RS

Membrane force in y

6

MXY

RS

Membrane force in xy

7

BMX

RS

Bending moment in x

8

BMY

RS

Bending moment in y

9

BMXY

RS

Bending moment in xy

10

TX

RS

Shear force in x

11

TY

RS

Shear force in y

TCODE,7 =1

Real/imaginary or magnitude/phase

4

MXR

RS

Membrane force in x - real/mag. part

5

MYR

RS

Membrane force in y - real/mag. part

6

MXYR

RS

Membrane force in xy - real/mag. part

5-40

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

7

BMXR

RS

Bending moment in x - real/mag. part

8

BMYR

RS

Bending moment in y - real/mag. part

9

BMXYR

RS

Bending moment in xy - real/mag. part

10

TXR

RS

Shear force in x - real/mag. part

11

TYR

RS

Shear force in y - real/mag. part

12

MXI

RS

Membrane force in x - imag./phase part

13

MYI

RS

Membrane force in y - imag./phase part

14

MXYI

RS

Membrane force in xy - imag./phase part

15

BMXI

RS

Bending moment in x - imag./phase part

16

BMYI

RS

Bending moment in y - imag./phase part

17

BMXYI

RS

Bending moment in xy - imag./phase part

18

TXI

RS

Shear force in x - imag./phase part

19

TYI

RS

Shear force in y - imag./phase part

End TCODE,7 Words 3 through max repeat 005 times ELTYPE =65 2

Unused (Pre-V69 CHEX8) UNDEF

ELTYPE =66 2

None Unused (Pre-V69 CHEX20)

UNDEF

ELTYPE =67

None Acoustics in HEXA

2

AXR

RS

3

AYR

RS

4

AZR

RS

5

VXR

RS

6

VYR

RS

7

VXR

RS

DMAP Programmer’s Guide

5-41

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

8

AXI

RS

9

AYI

RS

10

AZI

RS

11

VXI

RS

12

VYI

RS

13

VXI

RS

14

DB

RS

ELTYPE =68

Description

Acoustics in PENTA

2

AXR

RS

3

AYR

RS

4

AZR

RS

5

VXR

RS

6

VYR

RS

7

VXR

RS

8

AXI

RS

9

AYI

RS

10

AZI

RS

11

VXI

RS

12

VYI

RS

13

VXI

RS

14

DB

RS

ELTYPE =69

Curved beam or pipe element (CBEND - see note.)

TCODE,7 =0 or 2

Real or Random Response

2

GRID

I

Grid point identification number

3

BM1

RS

Bending moment plane 1

4

BM2

RS

Bending moment plane 1

5-42

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

5

TS1

RS

Shear plane 1

6

TS2

RS

Shear plane 2

7

AF

RS

Axial force

8

TRQ

RS

Torque

TCODE,7 =1

Real/imaginary or magnitude/phase

2

GRID

I

Grid point identification number - real/mag. part

3

BM1R

RS

Bending moment plane 1 - real/mag. part

4

BM2R

RS

Bending moment plane 1 - real/mag. part

5

TS1R

RS

Shear plane 1 - real/mag. part

6

TS2R

RS

Shear plane 2 - real/mag. part

7

AFR

RS

Axial force - real/mag. part

8

TRQR

RS

Torque - real/mag. part

9

BM1I

RS

Bending moment plane 1 - imag./phase part

10

BM2I

RS

Bending moment plane 1 - imag./phase part

11

TS1I

RS

Shear plane 1 - imag./phase part

12

TS2I

RS

Shear plane 2 - imag./phase part

13

AFI

RS

Axial force - imag./phase part

14

TRQI

RS

Torque - imag./phase part

End TCODE,7 Words 2 through max repeat 002 times Name

Word ELTYPE =70

Type

Description

Triangular plate element (CTRIAR)

2

TERM

CHAR4

Character string "CEN/"

3

GRID

I

Number of active grids or corner grid ID

TCODE,7 =0 or 2

Real or Random Response

DMAP Programmer’s Guide

5-43

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

4

MX

RS

Membrane force in x

5

MY

RS

Membrane force in y

6

MXY

RS

Membrane force in xy

7

BMX

RS

Bending moment in x

8

BMY

RS

Bending moment in y

9

BMXY

RS

Bending moment in xy

10

TX

RS

Shear force in x

11

TY

RS

Shear force in y

TCODE,7 =1

Real/imaginary or magnitude/phase

4

MXR

RS

Membrane force in x - real/mag. part

5

MYR

RS

Membrane force in y - real/mag. part

6

MXYR

RS

Membrane force in xy - real/mag. part

7

BMXR

RS

Bending moment in x - real/mag. part

8

BMYR

RS

Bending moment in y - real/mag. part

9

BMXYR

RS

Bending moment in xy - real/mag. part

10

TXR

RS

Shear force in x - real/mag. part

11

TYR

RS

Shear force in y - real/mag. part

12

MXI

RS

Membrane force in x - imag./phase part

13

MYI

RS

Membrane force in y - imag./phase part

14

MXYI

RS

Membrane force in xy - imag./phase part

15

BMXI

RS

Bending moment in x - imag./phase part

16

BMYI

RS

Bending moment in y - imag./phase part

17

BMXYI

RS

Bending moment in xy - imag./phase part

18

TXI

RS

Shear force in x - imag./phase part

19

TYI

RS

Shear force in y - imag./phase part

End TCODE,7

5-44

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

Words 3 through max repeat 004 times ELTYPE =71 2

Unused UNDEF

ELTYPE =72 2

AEROQ4 UNDEF

ELTYPE =73 2

None

None Unused (Pre-V69 CFTUBE)

UNDEF

None

ELTYPE =74

Triangular shell element (CTRIA3)

TCODE,7 =0 or 2

Real or Random Response

2

MX

RS

Membrane in x

3

MY

RS

Membrane in y

4

MXY

RS

Membrane in xy

5

BMX

RS

Bending in x

6

BMY

RS

Bending in y

7

BMXY

RS

Bending in xy

8

TX

RS

Transverse Shear in x

9

TY

RS

Transverse Shear in y

TCODE,7 =1

Real/imaginary or magnitude/phase

2

MXR

RS

Membrane in x - real/mag. part

3

MYR

RS

Membrane in y - real/mag. part

4

MXYR

RS

Membrane in xy - real/mag. part

5

BMXR

RS

Bending in x - real/mag. part

6

BMYR

RS

Bending in y - real/mag. part

7

BMXYR

RS

Bending in xy - real/mag. part

8

TXR

RS

Transverse Shear in x - real/mag. part

9

TYR

RS

Transverse Shear in y - real/mag. part

DMAP Programmer’s Guide

5-45

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

10

MXI

RS

Membrane in x - imag./phase part

11

MYI

RS

Membrane in y - imag./phase part

12

MXYI

RS

Membrane in xy - imag./phase part

13

BMXI

RS

Bending in x - imag./phase part

14

BMYI

RS

Bending in y - imag./phase part

15

BMXYI

RS

Bending in xy - imag./phase part

16

TXI

RS

Transverse Shear in x - imag./phase part

17

TYI

RS

Transverse Shear in y - imag./phase part

End TCODE,7 ELTYPE =75

Curved triangular shell element (CTRIA6)

2

TERM

CHAR4

Character string "CEN/"

3

GRID

I

Number of active grids or corner grid ID

TCODE,7 =0 or 2

Real or Random Response

4

MX

RS

Membrane force in x

5

MY

RS

Membrane force in y

6

MXY

RS

Membrane force in xy

7

BMX

RS

Bending moment in x

8

BMY

RS

Bending moment in y

9

BMXY

RS

Bending moment in xy

10

TX

RS

Shear force in x

11

TY

RS

Shear force in y

TCODE,7 =1

Real/imaginary or magnitude/phase

4

MXR

RS

Membrane force in x - real/mag. part

5

MYR

RS

Membrane force in y - real/mag. part

6

MXYR

RS

Membrane force in xy - real/mag. part

7

BMXR

RS

Bending moment in x - real/mag. part

5-46

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

8

BMYR

RS

Bending moment in y - real/mag. part

9

BMXYR

RS

Bending moment in xy - real/mag. part

10

TXR

RS

Shear force in x - real/mag. part

11

TYR

RS

Shear force in y - real/mag. part

12

MXI

RS

Membrane force in x - imag./phase part

13

MYI

RS

Membrane force in y - imag./phase part

14

MXYI

RS

Membrane force in xy - imag./phase part

15

BMXI

RS

Bending moment in x - imag./phase part

16

BMYI

RS

Bending moment in y - imag./phase part

17

BMXYI

RS

Bending moment in xy - imag./phase part

18

TXI

RS

Shear force in x - imag./phase part

19

TYI

RS

Shear force in y - imag./phase part

End TCODE,7 Words 3 through max repeat 004 times ELTYPE =76 2

Acoustic velocity/pressures in six-sided solid element (CHEXA) ELNAME(2)

CHAR4

Element name: "HEXPR"

TCODE,7 = 1

Real/imaginary or magnitude/phase

4

AXR

RS

Acceleration in x - real/mag. part

5

AYR

RS

Acceleration in y - real/mag. part

6

AZR

RS

Acceleration in z - real/mag. part

7

VXR

RS

Velocity in x - real/mag. part

8

VYR

RS

Velocity in y - real/mag. part

9

VZR

RS

Velocity in z - real/mag. part

10

PRESSURE

RS

Pressure in dB

11

AXI

RS

Acceleration in x - imag./phase part

12

AYI

RS

Acceleration in y - imag./phase part

DMAP Programmer’s Guide

5-47

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

13

AZI

RS

Acceleration in z - imag./phase part

14

VXI

RS

Velocity in x - imag./phase part

15

VYI

RS

Velocity in y - imag./phase part

16

VXI

RS

Velocity in z - imag./phase part

TCODE,7 =0 or 2

Real or Random Response

4

AX

RS

Acceleration in x - real/mag. part

5

AY

RS

Acceleration in y - real/mag. part

6

AZ

RS

Acceleration in z - real/mag. part

7

VX

RS

Velocity in x - real/mag. part

8

VY

RS

Velocity in y - real/mag. part

9

VZ

RS

Velocity in z - real/mag. part

10

PRESSURE

RS

Pressure in dB

ELTYPE =77 2

Acoustic velocity/pressures in five-sided solid element (CPENTA) ELNAME(2)

CHAR4

Element name: "PENPR"

TCODE,7 =0 or 2

Real or Random Response

4

AX

RS

Acceleration in x

5

AY

RS

Acceleration in y

6

AZ

RS

Acceleration in z

7

VX

RS

Velocity in x

8

VY

RS

Velocity in y

9

VZ

RS

Velocity in z

10

PRESSURE

RS

Pressure in dB

TCODE,7 =1

Complex

4

AXR

RS

Acceleration in x - real/mag. part

5

AYR

RS

Acceleration in y - real/mag. part

6

AZR

RS

Acceleration in z - real/mag. part

5-48

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

7

VXR

RS

Velocity in x - real/mag. part

8

VYR

RS

Velocity in y - real/mag. part

9

VZR

RS

Velocity in z - real/mag. part

10

PRESSURE

RS

Pressure in dB

11

AXI

RS

Acceleration in x - imag./phase part

12

AYI

RS

Acceleration in y - imag./phase part

13

AZI

RS

Acceleration in z - imag./phase part

14

VXI

RS

Velocity in x - imag./phase part

15

VYI

RS

Velocity in y - imag./phase part

16

VZI

RS

Velocity in z - imag./phase part

End TCODE,7 ELTYPE =78 2

Acoustic velocity/pressures in four-sided solid element (CTETRA) ELNAME(2)

CHAR4

Element name: "TETPR"

TCODE,7 =0 or 2

Real or Random Response

4

AX

RS

Acceleration in x

5

AY

RS

Acceleration in y

6

AZ

RS

Acceleration in z

7

VX

RS

Velocity in x

8

VY

RS

Velocity in y

9

VZ

RS

Velocity in z

10

PRESSURE

RS

Pressure in dB

4

AXR

RS

Acceleration in x - real/mag. part

5

AYR

RS

Acceleration in y - real/mag. part

6

AZR

RS

Acceleration in z - real/mag. part

7

VXR

RS

Velocity in x - real/mag. part

TCODE,7 =1

DMAP Programmer’s Guide

5-49

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

VYR

RS

Velocity in y - real/mag. part

9

VZR

RS

Velocity in z - real/mag. part

10

PRESSURE

RS

Pressure in dB

11

AXI

RS

Acceleration in x - imag./phase part

12

AYI

RS

Acceleration in y - imag./phase part

13

AZI

RS

Acceleration in z - imag./phase part

14

VXI

RS

Velocity in x - imag./phase part

15

VYI

RS

Velocity in y - imag./phase part

16

VZI

RS

Velocity in z - imag./phase part

End TCODE,7 ELTYPE =79 2

Acoustic velocity/pressures in five-sided solid element (CPYRAM) ELNAME(2)

CHAR4

Element name: “PYRAMPR”

TCODE,7 = 0 or 2

Real or Random Response

4

AX

RS

Acceleration in x

5

AY

RS

Acceleration in y

6

AZ

RS

Acceleration in z

7

VX

RS

Velocity in x

8

VY

RS

Velocity in y

9

VZ

RS

Velocity in z

10

PRESSURE

RS

Pressure in dB

TCODE,7 = 1 4

AXR

RS

Acceleration in x – real/mag. part

5

AYR

RS

Acceleration in y – real/mag. part

6

AZR

RS

Acceleration in z – real/mag. part

7

VXR

RS

Velocity in x – real/mag. part

8

VYR

RS

Velocity in y– real/mag. part

5-50

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

9

VZR

RS

Velocity in z– real/mag. part

10

PRESSURE

RS

Pressure in dB

11

AXI

RS

Acceleration in x – imag./phase part

12

AYI

RS

Acceleration in y – imag./phase part

13

AZI

RS

Acceleration in z – imag./phase part

14

VXI

RS

Velocity in x – imag./phase part

15

VYI

RS

Velocity in y – imag./phase part

16

VZI

RS

Velocity in z – imag./phase part

End TCODE,7 Name

Word ELTYPE =80 2

Description

Unused UNDEF

ELTYPE =81 2

Type

None Unused

UNDEF

ELTYPE =82

None Quadrilateral plate element (CQUADR)

2

TERM

CHAR4

Character string "CEN/"

3

GRID

I

Number of active grids (4) or corner grid identification number

TCODE,7 =0 or 2

Real or Random Response

4

MX

RS

Membrane force in x

5

MY

RS

Membrane force in y

6

MXY

RS

Membrane force in xy

7

BMX

RS

Bending moment in x

8

BMY

RS

Bending moment in y

9

BMXY

RS

Bending moment in xy

10

TX

RS

Shear force in x

DMAP Programmer’s Guide

5-51

Data Block Descriptions O-V

Chapter 5

Name

Word 11

TY

TCODE,7 =1

Type RS

Description Shear force in y

Real/imaginary or magnitude/phase

4

MXR

RS

Membrane force in x - real/mag. part

5

MYR

RS

Membrane force in y - real/mag. part

6

MXYR

RS

Membrane force in xy - real/mag. part

7

BMXR

RS

Bending moment in x - real/mag. part

8

BMYR

RS

Bending moment in y - real/mag. part

9

BMXYR

RS

Bending moment in xy - real/mag. part

10

TXR

RS

Shear force in x - real/mag. part

11

TYR

RS

Shear force in y - real/mag. part

12

MXI

RS

Membrane force in x - imag./phase part

13

MYI

RS

Membrane force in y - imag./phase part

14

MXYI

RS

Membrane force in xy - imag./phase part

15

BMXI

RS

Bending moment in x - imag./phase part

16

BMYI

RS

Bending moment in y - imag./phase part

17

BMXYI

RS

Bending moment in xy - imag./phase part

18

TXI

RS

Shear force in x - imag./phase part

19

TYI

RS

Shear force in y - imag./phase part

End TCODE,7 Words 3 through max repeat 005 times ELTYPE =83 2

Acoustic absorber element (CHACAB) UNDEF

ELTYPE =84 2

Acoustic barrier element (CHACBR) UNDEF

ELTYPE =85 2

5-52

None

None Nonlinear TETRA

UNDEF

DMAP Programmer’s Guide

None

Data Block Descriptions O-V

Name

Word ELTYPE =86 2 ELTYPE =87

ELTYPE =88

ELTYPE =89

ELTYPE =90

Type

Description

Nonlinear QUAD4 UNDEF

ELTYPE =91

None Nonlinear PENTA

UNDEF

ELTYPE =92 2

None

Name

Word

2

None Nonlinear ROD

UNDEF

2

None Nonlinear TRIA3

UNDEF

2

None Nonlinear TUBE

UNDEF

2

Description

Nonlinear GAP UNDEF

2

Type

None Nonlinear CONROD

UNDEF

ELTYPE =93

None Acoustics in HEXA

2

AXR

RS

3

AYR

RS

4

AZR

RS

5

VXR

RS

6

VYR

RS

7

VXR

RS

8

AXI

RS

9

AYI

RS

10

AZI

RS

11

VXI

RS

DMAP Programmer’s Guide

5-53

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

12

VYI

RS

13

VXI

RS

14

DB

RS

ELTYPE =94 2

Description

Nonlinear BEAM UNDEF

ELTYPE =95

None Composite quadrilateral plate element (CQUAD4)

2

THEORY(2)

CHAR4

Theory

4

LAMID

I

Lamina number

5

FP

RS

Failure index for direct stresses

6

FM

CHAR4

Failure mode for maximum strain theory

7

FB

RS

Failure index for interlaminar shear stress or -1

8

FMAX

RS

Maximum of FP and FB or -1.

9

FFLAG

CHAR4

Failure flag

ELTYPE =96

Composite curved quadrilateral shell element (CQUAD8)

2

THEORY(2)

CHAR4

Theory

4

LAMID

I

Lamina number

5

FP

RS

Failure index for direct stresses

6

FM

CHAR4

Failure mode for maximum strain theory

7

FB

RS

Failure index for interlaminar shear stress or -1

8

FMAX

RS

Maximum of FP and FB or -1.

9

FFLAG

CHAR4

Failure flag

ELTYPE =97

Composite triangular shell element (CTRIA3)

2

THEORY(2)

CHAR4

Theory

4

LAMID

I

Lamina number

5

FP

RS

Failure index for direct stresses

5-54

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

6

FM

CHAR4

Failure mode for maximum strain theory

7

FB

RS

Failure index for interlaminar shear stress or -1

8

FMAX

RS

Maximum of FP and FB or -1.

9

FFLAG

CHAR4

Failure flag

ELTYPE =98

Composite curved triangular shell element (CTRIA6)

2

THEORY(2)

CHAR4

Theory

4

LAMID

I

Lamina number

5

FP

RS

Failure index for direct stresses

6

FM

CHAR4

Failure mode for maximum strain theory

7

FB

RS

Failure index for interlaminar shear stress or -1

8

FMAX

RS

Maximum of FP and FB or -1.

9

FFLAG

CHAR4

Failure flag

ELTYPE =99 2

Unused UNDEF

None

Name

Word

Type

Description

ELTYPE =100

Simple beam element w/stations (CBAR with CBARAO or PLOAD1)

TCODE,7 =0 or 2

Real or Random Response

2

SD

RS

Station distance divided by length

3

BM1

RS

Bending moment plane 1

4

BM2

RS

Bending moment plane 2

5

TS1

RS

Shear plane 1

6

TS2

RS

Shear plane 2

7

AF

RS

Axial force

8

TRQ

RS

Torque

DMAP Programmer’s Guide

5-55

Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7 =1

Type

Description

Real/imaginary or magnitude/phase

2

SD

RS

Station distance divided by length

3

BM1R

RS

Bending moment plane 1 - real/mag. part

4

BM2R

RS

Bending moment plane 2 - real/mag. part

5

TP1R

RS

Shear plane 1 - real/mag. part

6

TP2R

RS

Shear plane 2 - real/mag. part

7

AFR

RS

Axial force - real/mag. part

8

TRQR

RS

Torque - real/mag. part

9

BM1I

RS

Bending moment plane 1 - imag./phase part

10

BM2I

RS

Bending moment plane 2 - imag./phase part

11

TS1I

RS

Shear plane 1 - imag./phase part

12

TS2I

RS

Shear plane 2 - imag./phase part

13

AFI

RS

Axial force - imag./phase part

14

TRQI

RS

Torque - imag./phase part

End TCODE,7 ELTYPE =101

Acoustic absorber element with freq. dependence (CAABSF)

2

IMPEDR

RS

Impedance - real/mag. part

3

IMPEDI

RS

Impedance - imag./phase part

4

ABSORB

RS

Absorption coefficient

ELTYPE =102

Generalized spring and damper element (CBUSH)

TCODE,7 =0 or 2

Real or Random Response

2

FX

RS

Force x

3

FY

RS

Force y

4

FZ

RS

Force z

5

MX

RS

Moment x

6

MY

RS

Moment y

5-56

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word 7

MZ

TCODE,7 =1

Type RS

Description Moment z

Real/imaginary or magnitude/phase

2

FXR

RS

Force x - real/mag. part

3

FYR

RS

Force y - real/mag. part

4

FZR

RS

Force z - real/mag. part

5

MXR

RS

Moment x - real/mag. part

6

MYR

RS

Moment y - real/mag. part

7

MZR

RS

Moment z - real/mag. part

8

FXI

RS

Force x - imag./phase part

9

FYI

RS

Force y - imag./phase part

10

FZI

RS

Force z - imag./phase part

11

MXI

RS

Moment x - imag./phase part

12

MYI

RS

Moment y - imag./phase part

13

MZI

RS

Moment z - imag./phase part

End TCODE,7 ELTYPE =103

Quadrilateral shell element (QUADP)

2

None

UNDEF

ELTYPE =104

Triangular shell p-element (TRIAP)

2

None

UNDEF

ELTYPE =105

Beam p-element (BEAMP)

2

None

UNDEF

ELTYPE =106

Scalar damper with material property (CDAMP5)

2

None

UNDEF

ELTYPE =107

Heat transfer boundary condition element - (CHBDYE)

2

NAME(2)

CHAR4

Element name

4

FAPPLIED

RS

Applied load

DMAP Programmer’s Guide

5-57

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

5

FREECONV

RS

Free convection

6

FORCECON

RS

Forced convection

7

FRAD

RS

Radiation

8

FTOTAL

RS

Total

ELTYPE =108

Heat transfer boundary condition element (CHBDYG)

2

NAME(2)

CHAR4

Element name

4

FAPPLIED

RS

Applied load

5

FREECONV

RS

Free convection

6

FORCECON

RS

Forced convection

7

FRAD

RS

Radiation

8

FTOTAL

RS

Total

ELTYPE =109

Heat transfer boundary condition element (CHBDYP)

2

NAME(2)

CHAR4

Element name

4

FAPPLIED

RS

Applied load

5

FREECONV

RS

Free convection

6

FORCECON

RS

Forced convection

7

FRAD

RS

Radiation

8

FTOTAL

RS

Total

Name

Word

Type

ELTYPE =110

CONV

2

None

UNDEF

ELTYPE =111

CONVM

2

None

UNDEF

ELTYPE =112

QBDY3

2

None

UNDEF

ELTYPE =113

5-58

DMAP Programmer’s Guide

QVECT

Description

Data Block Descriptions O-V

Name

Word 2

UNDEF

Type None

ELTYPE =114

QVOL

2

None

UNDEF

ELTYPE =115

Radbc

2

None

UNDEF

Description

ELTYPE =116

Slideline contact (SLIF1D)

2

UNDEF

None

Word

Name

Type

Description

ELTYPE =117

CWELDC

TCODE,7 =0 or 2

Real or Random Response

2

BM1A

RS

Bending moment end A plane 1

3

BM2A

RS

Bending moment end A plane 2

4

BM1B

RS

Bending moment end B plane 1

5

BM2B

RS

Bending moment end B plane 2

6

TS1

RS

Shear plane 1

7

TS2

RS

Shear plane 2

8

AF

RS

Axial Force

9

TRQ

RS

Torque

TCODE,7 =1

Real / Imaginary

2

BM1AR

RS

Bending moment end A plane 1 - real part

3

BM2AR

RS

Bending moment end A plane 2 - real part

4

BM1BR

RS

Bending moment end B plane 1 - real part

5

BM2BR

RS

Bending moment end B plane 2 - real part

6

TS1R

RS

Shear plane 1 - real part

7

TS2R

RS

Shear plane 2 - real part

8

AFR

RS

Axial force - real part

DMAP Programmer’s Guide

5-59

Data Block Descriptions O-V

Chapter 5

Word

Name

Type

Description

9

TRQR

RS

Torque - real part

10

BM1AI

RS

Bending moment end A plane 1 - imaginary part

11

BM2AI

RS

Bending moment end A plane 2 - imaginary part

12

BM1BI

RS

Bending moment end B plane 1 - imaginary part

13

BM2BI

RS

Bending moment end B plane 2 - imaginary part

14

TS1I

RS

Shear plane 1 - imaginary part

15

TS2I

RS

Shear plane 2 - imaginary part

16

AFI

RS

Axial Force - imaginary part

17

TRQI

RS

Torque - imaginary part

Type

Description

End TCODE,7 Word

Name

ELTYPE =118

CWELDP

TCODE,7 =0 or 2

Real or Random Response

2

BM1A

RS

Bending moment end A plane 1

3

BM2A

RS

Bending moment end A plane 2

4

BM1B

RS

Bending moment end B plane 1

5

BM2B

RS

Bending moment end B plane 2

6

TS1

RS

Shear plane 1

7

TS2

RS

Shear plane 2

8

AF

RS

Axial Force

9

TRQ

RS

Torque

TCODE,7 =1

Real / Imaginary

2

BM1AR

RS

Bending moment end A plane 1 - real part

3

BM2AR

RS

Bending moment end A plane 2 - real part

5-60

DMAP Programmer’s Guide

Data Block Descriptions O-V

Word

Name

Type

Description

4

BM1BR

RS

Bending moment end B plane 1 - real part

5

BM2BR

RS

Bending moment end B plane 2 - real part

6

TS1R

RS

Shear plane 1 - real part

7

TS2R

RS

Shear plane 2 - real part

8

AFR

RS

Axial force - real part

9

TRQR

RS

Torque - real part

10

BM1AI

RS

Bending moment end A plane 1 - imaginary part

11

BM2AI

RS

Bending moment end A plane 2 - imaginary part

12

BM1BI

RS

Bending moment end B plane 1 - imaginary part

13

BM2BI

RS

Bending moment end B plane 2 - imaginary part

14

TS1I

RS

Shear plane 1 - imaginary part

15

TS2I

RS

Shear plane 2 - imaginary part

16

AFI

RS

Axial Force - imaginary part

17

TRQI

RS

Torque - imaginary part

Type

Description

End TCODE,7 Word

Name

ELTYPE =119

CFAST

TCODE,7 =0 or 2

Real or Random Response

2

BM1A

RS

Bending moment end A plane 1

3

BM2A

RS

Bending moment end A plane 2

4

BM1B

RS

Bending moment end B plane 1

5

BM2B

RS

Bending moment end B plane 2

6

TS1

RS

Shear plane 1

7

TS2

RS

Shear plane 2

DMAP Programmer’s Guide

5-61

Data Block Descriptions O-V

Chapter 5

Word

Name

Type

Description

8

AF

RS

Axial Force

9

TRQ

RS

Torque

TCODE,7 =1

Real / Imaginary

2

BM1AR

RS

Bending moment end A plane 1 - real part

3

BM2AR

RS

Bending moment end A plane 2 - real part

4

BM1BR

RS

Bending moment end B plane 1 - real part

5

BM2BR

RS

Bending moment end B plane 2 - real part

6

TS1R

RS

Shear plane 1 - real part

7

TS2R

RS

Shear plane 2 - real part

8

AFR

RS

Axial force - real part

9

TRQR

RS

Torque - real part

10

BM1AI

RS

Bending moment end A plane 1 - imaginary part

11

BM2AI

RS

Bending moment end A plane 2 - imaginary part

12

BM1BI

RS

Bending moment end B plane 1 - imaginary part

13

BM2BI

RS

Bending moment end B plane 2 - imaginary part

14

TS1I

RS

Shear plane 1 - imaginary part

15

TS2I

RS

Shear plane 2 - imaginary part

16

AFI

RS

Axial Force - imaginary part

17

TRQI

RS

Torque - imaginary part

End TCODE,7 Name

Word

Type

ELTYPE =127

CQUAD

2

None

UNDEF

ELTYPE =128

5-62

DMAP Programmer’s Guide

CQUADX

Description

Data Block Descriptions O-V

Name

Word 2

UNDEF

Type None

ELTYPE =129

RELUC

2

None

UNDEF Name

Word

Type

ELTYPE =130

RES

2

None

UNDEF

ELTYPE =131

TETRAE

2

None

UNDEF

ELTYPE =132

CTRIA

2

None

UNDEF

ELTYPE =133

CTRIAX

2

None

UNDEF

ELTYPE =134

LINEOB

2

None

UNDEF

ELTYPE =135

LINXOB

2

None

UNDEF

ELTYPE =136

QUADOB

2

None

UNDEF

ELTYPE =137

TRIAOB

2

None

UNDEF

ELTYPE =138

LINEX

2

None

UNDEF

ELTYPE =139

Hyperelastic QUAD4FD

2

None

UNDEF Word

ELTYPE =140

Name

Description

Type

Description

Description

HEXA8FD

DMAP Programmer’s Guide

5-63

Data Block Descriptions O-V

Chapter 5

Name

Word 2

UNDEF

Type

Description

None

ELTYPE =141

Six-sided solid p-element (HEXAP)

2

None

UNDEF

ELTYPE =142

Five-sided solid p-element (PENTAP)

2

None

UNDEF

ELTYPE =143

Four-sided solid p-element (TETRAP)

2

None

UNDEF

ELTYPE =144

Quadrilateral plate element for corner stresses (QUAD144)

2

TERM

CHAR4

Character string "CEN/"

3

GRID

I

Number of active grids (4) or corner grid ID

TCODE,7 =0 or 2

Real or Random Response

4

MX

RS

Membrane x

5

MY

RS

Membrane y

6

MXY

RS

Membrane xy

7

BMX

RS

Bending x

8

BMY

RS

Bending y

9

BMXY

RS

Bending xy

10

TX

RS

Shear x

11

TY

RS

Shear y

TCODE,7 =1

Real/imaginary or magnitude/phase

4

MXR

RS

Membrane x - real/mag. part

5

MYR

RS

Membrane y - real/mag. part

6

MXYR

RS

Membrane xy - real/mag. part

7

BMXR

RS

Bending x - real/mag. part

8

BMYR

RS

Bending y - real/mag. part

9

BMXYR

RS

Bending xy - real/mag. part

5-64

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

10

TXR

RS

Shear x - real/mag. part

11

TYR

RS

Shear y - real/mag. part

12

MXI

RS

Membrane x - imag./phase part

13

MYI

RS

Membrane y - imag./phase part

14

MXYI

RS

Membrane xy - imag./phase part

15

BMXI

RS

Bending x - imag./phase part

16

BMYI

RS

Bending y - imag./phase part

17

BMXYI

RS

Bending xy - imag./phase part

18

TXI

RS

Shear x - imag./phase part

19

TYI

RS

Shear y - imag./phase part

End TCODE,7 Words 3 through max repeat 005 times ELTYPE =145

Six-sided solid display element (VUHEXA)

2

None

UNDEF

ELTYPE =146

Five-sided solid display element (VUPENTA)

2

None

UNDEF

ELTYPE =147

Four-sided solid display element (VUTETRA)

2

None

UNDEF

ELTYPE =148

HEXAM

2

None

UNDEF

ELTYPE =149

PENTAM

2

None

UNDEF Name

Word

Type

ELTYPE =150

TETRAM

2

None

UNDEF

ELTYPE =151

Description

QUADM

DMAP Programmer’s Guide

5-65

Data Block Descriptions O-V

Chapter 5

Name

Word 2

UNDEF

Type None

ELTYPE =152

TRIAM

2

None

UNDEF

ELTYPE =153

QUADXM

2

None

UNDEF

ELTYPE =154

TRIAXM

2

None

UNDEF

ELTYPE =155

QUADPW

2

None

UNDEF

ELTYPE =156

TRIAPW

2

None

UNDEF

ELTYPE =157

LINEPW

2

None

UNDEF

ELTYPE =158

QUADOBM

2

None

UNDEF

ELTYPE =159

TRIAOBM

2

None

UNDEF Name

Word

Description

Type

Description

ELTYPE =160

Five-sided finite deformation solid element (PENTA6FD)

2

None

UNDEF

ELTYPE =161

Five-sided finite deformation solid element (TETRA4FD)

2

None

UNDEF

ELTYPE =162

Triangular finite deformation shell element (TRIA3FD)

2

None

UNDEF

ELTYPE =163

HEXAFD

2

None

5-66

UNDEF

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

ELTYPE =164

QUADFD

2

None

UNDEF

ELTYPE =165

PENTAFD

2

None

UNDEF

ELTYPE =166

TETRAFD

2

None

UNDEF

ELTYPE =167

TRIAFD

2

None

UNDEF

ELTYPE =168

TRIAX3FD

2

None

UNDEF

ELTYPE =169

TRIAXFD

2

None

UNDEF Name

Word

Type

ELTYPE =170

QUADX4FD

2

None

UNDEF

ELTYPE =171

QUADXFD

2

None

UNDEF

ELTYPE =174

LINEOBM

2

None

UNDEF

ELTYPE =175

LINXOBM

2

None

UNDEF

ELTYPE =176

QUADWGM

2

None

UNDEF

ELTYPE =177

TRIAWGM

2

None

UNDEF

ELTYPE =178

Description

Description

QUADIB

DMAP Programmer’s Guide

5-67

Data Block Descriptions O-V

Chapter 5

Name

Word 2

UNDEF

Type None

ELTYPE =179

TRIAIB

2

None

UNDEF Name

Word

Type

ELTYPE =180

LINEIB

2

None

UNDEF

ELTYPE =181

LINXIB

2

None

UNDEF

ELTYPE =182

QUADIBM

2

None

UNDEF

ELTYPE =183

TRIAIBM

2

None

UNDEF

ELTYPE =184

LINEIBM

2

None

UNDEF

ELTYPE =185

LINXIBM

2

None

UNDEF

ELTYPE =186

QUADPWM

2

None

UNDEF

ELTYPE =187

TRIAPWM

2

None

UNDEF

ELTYPE =188

LINEPWM

2

None

UNDEF

Description

Description

ELTYPE =189

Quadrilateral plate view element (VUQUAD)

2

PARENT

I

Parent p-element identification number

3

COORD

I

Coordinate system identification number

4

ICORD

CHAR4

Flat/curved and so on

5-68

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

5

THETA

I

6

UNDEF

None

TCODE,7 =0

Description Material angle

Real

7

VUID

I

VU-grid identification number ID for corner

8

MFX

RS

Membrane force x

9

MFY

RS

Membrane force y

10

MFXY

RS

Membrane force xy

11

UNDEF(3 )

None

14

BMX

RS

Bending moment x

15

BMY

RS

Bending moment y

16

BMXY

RS

Bending moment xy

17

SYZ

RS

Shear yz

18

SZX

RS

Shear zx

19

UNDEF

None

Words 7 through 19 repeat 004 times TCODE,7 =1

Real/imaginary or magnitude/phase

7

VUID

I

VU-grid identification number for corner

8

MFXR

RS

Membrane force x real/mag.

9

MFYR

RS

Membrane force y real/mag.

10

MFXYR

RS

Membrane force xy real/mag.

11

UNDEF(3 )

None

14

BMXR

RS

Bending moment x real/mag.

15

BMYR

RS

Bending moment y real/mag.

16

BMXYR

RS

Bending moment xy real/mag.

17

SYZR

RS

Shear yz real/mag.

18

SZXR

RS

Shear zx real/mag.

DMAP Programmer’s Guide

5-69

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

19

UNDEF

None

20

MFXI

RS

Membrane force x imag./phase

21

MFYI

RS

Membrane force y imag./phase

22

MFXYI

RS

Membrane force xy imag./phase

23

UNDEF(3 )

None

26

BMXI

RS

Bending moment x imag./phase

27

BMYI

RS

Bending moment y imag./phase

28

BMXYI

RS

Bending moment xy imag./phase

29

SYZI

RS

Shear yz imag./phase

30

SZXI

RS

Shear zx imag./phase

31

UNDEF

None

Words 7 through 31 repeat 004 times End TCODE,7 Name

Word

Type

Description

ELTYPE =190

Triangular shell view element (VUTRIA)

2

PARENT

I

Parent p-element identification number

3

COORD

I

Coordinate system identification number

4

ICORD

CHAR4

Flat/curved and so on

5

THETA

I

Material angle

6

UNDEF

None

TCODE,7 =0

Real

7

VUID

I

VU grid ID for this corner

8

MFX

RS

Membrane force x

9

MFY

RS

Membrane force y

10

MFXY

RS

Membrane force xy

11

UNDEF(3 )

None

5-70

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

14

BMX

RS

Bending moment x

15

BMY

RS

Bending moment y

16

BMXY

RS

Bending moment xy

17

SYZ

RS

Shear yz

18

SZX

RS

Shear zx

19

UNDEF

None

Words 7 through 19 repeat 003 times TCODE,7 =1

Real/imaginary or magnitude/phase

7

VUID

I

VU grid ID this corner

8

MFXR

RS

Membrane force x real/mag.

9

MFYR

RS

Membrane force y real/mag.

10

MFXYR

RS

Membrane force xy real/mag.

11

UNDEF(3 )

None

14

BMXR

RS

Bending moment x real/mag.

15

BMYR

RS

Bending moment y real/mag.

16

BMXYR

RS

Bending moment xy real/mag.

17

SYZR

RS

Shear yz real/mag.

18

SZXR

RS

Shear zx real/mag.

19

UNDEF

None

20

MFXI

RS

Membrane force x imag./phase

21

MFYI

RS

Membrane force y imag./phase

22

MFXYI

RS

Membrane force xy imag./phase

23

UNDEF(3 )

None

26

BMXI

RS

Bending moment x imag./phase

27

BMYI

RS

Bending moment y imag./phase

28

BMXYI

RS

Bending moment xy imag./phase

DMAP Programmer’s Guide

5-71

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

29

SYZI

RS

Shear yz imag./phase

30

SZXI

RS

Shear zx imag./phase

31

UNDEF

None

Words 7 through 31 repeat 003 times End TCODE,7 ELTYPE =191

Beam view element (VUBEAM)

2

PARENT

I

Parent p-element identification number

3

COORD

I

Coordinate system identification number

4

ICORD

CHAR4

Flat/curved and so on

TCODE,7 =0

Real

5

VUGRID

I

VU grid ID for output grid

6

POSIT

RS

x/L position of VU grid identification number

7

FORCEX

RS

Force x

8

SHEARY

RS

Shear force y

9

SHEARZ

RS

Shear force z

10

TORSION

RS

Torsional moment x

11

BENDY

RS

Bending moment y

12

BENDZ

RS

Bending moment z

TCODE,7 =1

Real/imaginary or magnitude/phase

5

VUGRID

I

VU grid identification number for output grid

6

POSIT

RS

x/L position of VU grid identification number

7

FORCEXR

RS

Force x real/mag.

8

SHEARYR

RS

Shear force y real/mag.

9

SHEARZR

RS

Shear force z real/mag.

10

TORSINR

RS

Torsional moment x real/mag.

11

BENDYR

RS

Bending moment y real/mag.

5-72

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

12

BENDZR

RS

Bending moment z real/mag.

13

FORCEXI

RS

Force x imag./phase

14

SHEARYI

RS

Shear force y imag./phase

15

SHEARZI

RS

Shear force z imag./phase

16

TORSINI

RS

Torsional moment x imag./phase

17

BENDYI

RS

Bending moment y imag./phase

18

BENDZI

RS

Bending moment z imag./phase

End TCODE,7 Words 5 through max repeat 2 times ELTYPE =192

CVINT

2

None

UNDEF

ELTYPE =193

QUADFR

2

None

UNDEF

ELTYPE =194

TRIAFR

2

None

UNDEF

ELTYPE =195

LINEFR

2

None

UNDEF

ELTYPE =196

LINXFR

2

None

UNDEF

ELTYPE =197

GMINTS

2

None

UNDEF

ELTYPE =198

CNVPEL

2

None

UNDEF

ELTYPE =199

VUHBDY

2

None

UNDEF

DMAP Programmer’s Guide

5-73

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ELTYPE =200

CWELD

TCODE,7 =0 or 2

Real or Random Response

2

BM1A

RS

Bending moment end A plane 1

3

BM2A

RS

Bending moment end A plane 2

4

BM1B

RS

Bending moment end B plane 1

5

BM2B

RS

Bending moment end B plane 2

6

TS1

RS

Shear plane 1

7

TS2

RS

Shear plane 2

8

AF

RS

Axial Force

9

TRQ

RS

Torque

TCODE,7 =1

Real / Imaginary

2

BM1AR

RS

Bending moment end A plane 1 - real part

3

BM2AR

RS

Bending moment end A plane 2 - real part

4

BM1BR

RS

Bending moment end B plane 1 - real part

5

BM2BR

RS

Bending moment end B plane 2 - real part

6

TS1R

RS

Shear plane 1 - real part

7

TS2R

RS

Shear plane 2 - real part

8

AFR

RS

Axial force - real part

9

TRQR

RS

Torque - real part

10

BM1AI

RS

Bending moment end A plane 1 - imaginary part

11

BM2AI

RS

Bending moment end A plane 2 - imaginary part

12

BM1BI

RS

Bending moment end B plane 1 - imaginary part

13

BM2BI

RS

Bending moment end B plane 2 - imaginary part

14

TS1I

RS

Shear plane 1 - imaginary part

5-74

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

15

TS2I

RS

Shear plane 2 - imaginary part

16

AFI

RS

Axial Force - imaginary part

17

TRQI

RS

Torque - imaginary part

End TCODE,7 ELTYPE =201

Nonlinear hyperelastic QUAD4FD

TCODE,7 =0 or 2

Real or Random Response

2

BM1A

RS

Bending moment end A plane 1

3

BM2A

RS

Bending moment end A plane 2

4

BM1B

RS

Bending moment end B plane 1

5

BM2B

RS

Bending moment end B plane 2

6

TS1

RS

Shear plane 1

7

TS2

RS

Shear plane 2

8

AF

RS

Axial Force

9

TRQ

RS

Torque

TCODE,7 =1

Real / Imaginary

2

BM1AR

RS

Bending moment end A plane 1 - real part

3

BM2AR

RS

Bending moment end A plane 2 - real part

4

BM1BR

RS

Bending moment end B plane 1 - real part

5

BM2BR

RS

Bending moment end B plane 2 - real part

6

TS1R

RS

Shear plane 1 - real part

7

TS2R

RS

Shear plane 2 - real part

8

AFR

RS

Axial force - real part

9

TRQR

RS

Torque - real part

10

BM1AI

RS

Bending moment end A plane 1 - imaginary part

11

BM2AI

RS

Bending moment end A plane 2 - imaginary part

DMAP Programmer’s Guide

5-75

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

12

BM1BI

RS

Bending moment end B plane 1 - imaginary part

13

BM2BI

RS

Bending moment end B plane 2 - imaginary part

14

TS1I

RS

Shear plane 1 - imaginary part

15

TS2I

RS

Shear plane 2 - imaginary part

16

AFI

RS

Axial Force - imaginary part

17

TRQI

RS

Torque - imaginary part

End TCODE,7 ELTYPE =202

Nonlinear hyperelastic HEXA4FD

2

None

UNDEF

ELTYPE =203

Slideline contact (SLIF1D)

2

None

UNDEF

ELTYPE =204 2

UNDEF

None

ELTYPE =205 2

UNDEF

None

ELTYPE =206

Hyperelastic triangular 3-noded nonlinear format (TRIA3FD) Gaus

2

None

UNDEF

ELTYPE =207

Hyperelastic hexahedron 20-noded nonlinear format (HEXAFD) Gaus

2

None

UNDEF

ELTYPE =208 2

UNDEF

None

ELTYPE =209 2

5-76

UNDEF

DMAP Programmer’s Guide

None

Data Block Descriptions O-V

Name

Word

Type

Description

ELTYPE =210 2

UNDEF

None

ELTYPE =211 2

UNDEF

None

ELTYPE =212 2

UNDEF

None

ELTYPE =213 2

UNDEF

None

ELTYPE =214 2

UNDEF

None

ELTYPE =215 2

UNDEF

None

ELTYPE =216 2

UNDEF

None

ELTYPE =217

Hyperelastic triangular 3-noded nonlinear format (TRIA3FD) Grid

2

None

UNDEF

ELTYPE =218

Hyperelastic hexahedron 20-noded nonlinear format (HEXAFD) Grid

2

None

UNDEF

ELTYPE =219 2

UNDEF Name

Word

None Type

Description

ELTYPE =220 2

UNDEF

None

ELTYPE =221 2

UNDEF

None

DMAP Programmer’s Guide

5-77

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ELTYPE =222 2

UNDEF

None

ELTYPE =223 2

UNDEF

None

ELTYPE =224

Nonlinear ELAS1

2

None

UNDEF

ELTYPE =225

Nonlinear ELAS3

2

None

UNDEF

ELTYPE =226

Nonlinear BUSH

2

None

UNDEF

ELTYPE =227

Triangular shell element (CTRIAR)

TCODE,7 =0 or 2

Real or Random Response

2

MX

RS

Membrane in x

3

MY

RS

Membrane in y

4

MXY

RS

Membrane in xy

5

BMX

RS

Bending in x

6

BMY

RS

Bending in y

7

BMXY

RS

Bending in xy

8

TX

RS

Transverse Shear in x

9

TY

RS

Transverse Shear in y

TCODE,7 =1

Real/imaginary or magnitude/phase

2

MXR

RS

Membrane in x - real/mag. part

3

MYR

RS

Membrane in y - real/mag. part

4

MXYR

RS

Membrane in xy - real/mag. part

5

BMXR

RS

Bending in x - real/mag. part

6

BMYR

RS

Bending in y - real/mag. part

5-78

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

7

BMXYR

RS

Bending in xy - real/mag. part

8

TXR

RS

Transverse Shear in x - real/mag. part

9

TYR

RS

Transverse Shear in y - real/mag. part

10

MXI

RS

Membrane in x - imag./phase part

11

MYI

RS

Membrane in y - imag./phase part

12

MXYI

RS

Membrane in xy - imag./phase part

13

BMXI

RS

Bending in x - imag./phase part

14

BMYI

RS

Bending in y - imag./phase part

15

BMXYI

RS

Bending in xy - imag./phase part

16

TXI

RS

Transverse Shear in x - imag./phase part

17

TYI

RS

Transverse Shear in y - imag./phase part

End TCODE,7 ELTYPE =228

Quadrilateral plate element (CQUADR)

TCODE,7 =0 or 2

Real or Random Response

2

MX

RS

Membrane in x

3

MY

RS

Membrane in y

4

MXY

RS

Membrane in xy

5

BMX

RS

Bending in x

6

BMY

RS

Bending in y

7

BMXY

RS

Bending in xy

8

TX

RS

Transverse Shear in x

9

TY

RS

Transverse Shear in y

TCODE,7 =1

Real/imaginary or magnitude/phase

2

MXR

RS

Membrane in x - real/mag. part

3

MYR

RS

Membrane in y - real/mag. part

4

MXYR

RS

Membrane in xy - real/mag. part

DMAP Programmer’s Guide

5-79

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

5

BMXR

RS

Bending in x - real/mag. part

6

BMYR

RS

Bending in y - real/mag. part

7

BMXYR

RS

Bending in xy - real/mag. part

8

TXR

RS

Transverse Shear in x - real/mag. part

9

TYR

RS

Transverse Shear in y - real/mag. part

10

MXI

RS

Membrane in x - imag./phase part

11

MYI

RS

Membrane in y - imag./phase part

12

MXYI

RS

Membrane in xy - imag./phase part

13

BMXI

RS

Bending in x - imag./phase part

14

BMYI

RS

Bending in y - imag./phase part

15

BMXYI

RS

Bending in xy - imag./phase part

16

TXI

RS

Transverse Shear in x - imag./phase part

17

TYI

RS

Transverse Shear in y - imag./phase part

End TCODE,7 Name

Word

Type

Description

ELTYPE =232

Composite quadrilateral plate element (CQUADR)

2

THEORY(2)

CHAR4

Theory

4

LAMID

I

Lamina number

5

FP

RS

Failure index for direct stresses

6

FM

CHAR4

Failure mode for maximum strain theory

7

FB

RS

Failure index for interlaminar shear stress or -1

8

FMAX

RS

Maximum of FP and FB or -1.

9

FFLAG

CHAR4

Failure flag

ELTYPE =233

Composite triangular shell element (CTRIAR)

2

THEORY(2)

CHAR4

5-80

DMAP Programmer’s Guide

Theory

Data Block Descriptions O-V

Name

Word

Type

Description

4

LAMID

I

Lamina number

5

FP

RS

Failure index for direct stresses

6

FM

CHAR4

Failure mode for maximum strain theory

7

FB

RS

Failure index for interlaminar shear stress or -1

8

FMAX

RS

Maximum of FP and FB or -1.

9

FFLAG

CHAR4

Failure flag

End ELTYPE End THERMAL Name

Word

Type

Description

ELTYPE =267

Ply failure for HEXAL

2

I

PLY

PLSLOC=0

Lamina number

Center option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

6

V1

RS

Failure value 1

7

V2

RS

Failure value 2

8

V3

RS

Failure value 3

9

V4

RS

Failure value 4

10

V5

RS

Failure value 5

11

V6

RS

Failure value 6

PLSLOC=1

Corner option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

DMAP Programmer’s Guide

5-81

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

6

V1

RS

Failure value 1

7

V2

RS

Failure value 2

8

V3

RS

Failure value 3

9

V4

RS

Failure value 4

10

V5

RS

Failure value 5

11

V6

RS

Failure value 6

Words 3 thru 11 repeat 5 times Name

Word

Type

Description

ELTYPE =268

Ply failure for PENTAL

2

I

PLY

PLSLOC=0

Lamina number

Center option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

6

V1

RS

Failure value 1

7

V2

RS

Failure value 2

8

V3

RS

Failure value 3

9

V4

RS

Failure value 4

10

V5

RS

Failure value 5

11

V6

RS

Failure value 6

PLSLOC=1

Corner option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

6

V1

RS

Failure value 1

7

V2

RS

Failure value 2

5-82

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

8

V3

RS

Failure value 3

9

V4

RS

Failure value 4

10

V5

RS

Failure value 5

11

V6

RS

Failure value 6

Words 3 thru 11 repeat 4 times Name

Word

Type

Description

ELTYPE =269

Inter-laminar failure for HEXAL

2

I

PLY

PLSLOC=0

Lamina number

Center option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

6

FSV

RS

Failure value

PLSLOC=1

Corner option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

6

FSV

RS

Failure value

Words 3 thru 6 repeat 5 times Name

Word

Type

Description

ELTYPE =270

Inter-laminar failure for PENTAL

2

I

PLY

PLSLOC=0

Lamina number

Center option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

DMAP Programmer’s Guide

5-83

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

5

THEORY

CHAR4

Failure theory

6

FSV

RS

Failure value

PLSLOC=1

Corner option

3

FLOC

CHAR4

Fiber location (BOT, MID, and TOP)

4

GRID

I

Edge grid ID (0=center)

5

THEORY

CHAR4

Failure theory

6

FSV

RS

Failure value

Words 3 thru 6 repeat 4 times

Record - TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

Notes: 1. The RECORD=IDENT and DATA pair is repeated for each subcase. 2. For composite elements, ELTYPEs 95 through 98, OEF contains composite failure indices and the DATA record is repeated for each ply as well as each element. Also, if EID=-1, the OFP module prints a blank line.

5.8 OEFMC Table of modal contributions of element forces. For all analysis types (real and complex), and SORT1 and SORT2 formats.

Record 0 - HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

5-84

DMAP Programmer’s Guide

Data Block Descriptions O-V

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

MCODE

I

Modal contributions code: 1=absolute, 2=normalized

4

SUBCASE

I

Subcase number

5

EICODE

I

Element item code (1000*element ID + item code)

TCODE,1 =1

Sort 1

ACODE,4 = 05

Frequency

6

FREQ

RS

7

UNDEF

None

ACODE,4 =06

Transient

6

TIME

RS

7

UNDEF

None

Frequency (Hz)

Time step

ACODE,4 =09

Complex Eigenvalues

6

EIGR

RS

Eigenvalue – real part

7

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 TCODE,1 =02

Sort 2

6

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

7

MFREQ

RS

Modal frequency (Hz)

End TCODE,1

8

UNDEF

None

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

DMAP Programmer’s Guide

5-85

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 - DATA Name

Word

Type

Description

TCODE,1 =01

Sort 1

1

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

2

MFREQ

RS

Modal frequency (Hz)

TCODE,1 =02

Sort 2

ACODE,4 =05 1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

ACODE,4 =06 1

TIME

RS

2

UNDEF

None

Time step

ACODE,4 =09 1

EIGR

RS

Eigenvalue – real part

2

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 End TCODE,1 TCODE,7 = 0 or 2

Real

3

RS

MC

TCODE,7 =1 3

5-86

Modal contribution

Real/ Imaginary MCR

DMAP Programmer’s Guide

RS

Modal contribution – real part

Data Block Descriptions O-V

Name

Word 4

MCI

Type RS

Description Modal contribution – imaginary part

End TCODE,7

Record 3 - TRAILER Name

Word

Type

1

NREC

I

2

UNDEF(5 )

None

Description Number of records

5.9 OES Table of element stresses or strains For all analysis types (real and complex) and SORT1 and SORT2 formats.

Record - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block Name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

ELTYPE(C)

I

Element Type

4

SUBCASE

I

Subcase or Random identification number

TCODE,1 =1

Sort 1

ACODE,4 =01

Statics

5

LSDVMN

I

6

UNDEF(2 )

None

Load set number

DMAP Programmer’s Guide

5-87

Chapter 5

Word

Data Block Descriptions O-V

Name

ACODE,4 =02

Type

Description

Real Eigenvalues

5

MODE

I

Mode Number

6

EIGN

RS

Eigenvalue

7

MODECYCL

RS

Mode or Cycle

ACODE,4 =03

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE,4 =04

Load set number

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

Load set number

Frequency

ACODE,4 =05 5

FREQ

RS

6

UNDEF

None

7

RANDOM ID

I

Frequency

Random identification number

Transient

ACODE,4 =06 5

TIME

RS

6

UNDEF(2 )

None

ACODE,4 =07

Time Step

Buckling Phase 0 (Pre-buckling)

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE,4 =08

Load set

Buckling Phase 1 (Post-buckling)

5

LSDVMN

I

Mode Number

6

EIGR

RS

Eigenvalue

7

RANDID

I

Random ID number

ACODE,4 =09 5

5-88

Complex Eigenvalues MODE

DMAP Programmer’s Guide

I

Mode

Data Block Descriptions O-V

Name

Word

Type

Description

6

EIGR

RS

Eigenvalue (real)

7

EIGI

RS

Eigenvalue (imaginary)

ACODE,4 =10

Nonlinear statics

5

LFTSFQ

RS

6

UNDEF(2 )

None

ACODE,4 =11

Load step

Old geometric nonlinear statics

5

LSDVMN

I

6

UNDEF

None

7

RANDID

I

ACODE,4 =12

Load set

Random ID number

CONTRAN (Can appear as ACODE=6)

5

TIME

RS

6

UNDEF(2 )

None

Time step

End ACODE,4 TCODE,1 =02

Sort 2

5

LSDVMN

I

6

UNDEF(2 )

None

Load set, mode number, time step, and so on

End TCODE,1 8

LOADSET

I

Load set number, Random code ID or Zero

9

FCODE

I

Format Code

10

NUMWDE(C)

I

Number of words per entry in DATA record

11

SCODE(C)

I

Stress/Strain code

12

PID (SOL 601 and 701 only)

I

Physical Property ID for SOL 601 & 701 only. UNDEF for all other SOLs

DMAP Programmer’s Guide

5-89

Data Block Descriptions O-V

Chapter 5

Name

Word 13

Type I

ELRESCS

Description Coordinate system in which stresses are written. Applicable to SOL 601/701, solid elements only. 0 = in element coordinate system (default) 1 = stresses are written according to CORDM

14

Q4CSTR(C)

I

Corner Stress Flag

15

PLSLOC(C)

I

Ply stress/strain location

16

UNDEF(35)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record - DATA Word

Name

Type

Description

SORTCODE=1

Sort 1 - SortCode=((TCODE/1000)+2)/2

TCODE,1 =1

o

1

EKEY

I

Device code + 10*Point identification number

TCODE,1 =02

Sort 2

ACODE/10=01

Analysis type

ACODE,4 =01

n

1

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

EKEY

ACODE,4 =02 1

EKEY

ACODE,4 =03 1

EKEY

ACODE,4 =04 1

5-90

EKEY

DMAP Programmer’s Guide

Data Block Descriptions O-V

Word

Name

Type

Description

RS

Frequency

RS

Time step

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

RS

Frequency or Time step

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

ACODE,4 =05 1

FREQ

ACODE,4 =06 1

TIME

ACODE,4 =07 1

EKEY

ACODE,4 =08 1

EKEY

ACODE,4 =09 1

EKEY

ACODE,4 =10 1

FQTS

ACODE,4 =11 1

EKEY

ACODE,4 =12 1

EKEY

End ACODE,4 End ACODE/10 Name

Word ELTYPE =00

Type

Description

Grid - OES1G table

2

MATID

I

Material identification number

3

NX1

RS

Normal in x at d1

4

NY1

RS

Normal in y at d1

5

TXY1

RS

Shear in xy at d1

6

SA1

RS

Theta ( Shear Angle ) at d1

7

MJRP1

RS

Major Principal at d1

DMAP Programmer’s Guide

5-91

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

MNRP1

RS

Minor Principal at d1

9

TMAX1

RS

Maximum Shear at d1

10

PCODE

I

10*interpolation points + projection code

11

NX2

RS

Normal in x at d2

12

NY2

RS

Normal in y at d2

13

TXY2

RS

Shear in xy at d2

14

SA2

RS

Theta ( Shear Angle ) at d2

15

MJRP2

RS

Major Principal at d2

16

MNRP2

RS

Minor Principal at d2

17

TMAX2

RS

Maximum Shear at d2

ELTYPE =01

Rod element (CROD)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

AE

RS

Axial Strain

3

MSA

RS

Axial Safety Margin*

4

TE

RS

Torsional Strain

5

MST

RS

Torsional Safety Margin*

TCODE,7 =1

Real / Imaginary

2

AER

RS

Axial Strain

3

AEI

RS

Axial Strain

4

TER

RS

Torsional Strain

5

TEI

RS

Torsional Strain

TCODE,7 =2

Random Response

2

AE

RS

Axial Strain

3

TE

RS

Torsional Strain

End TCODE,7

5-92

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

SCODE,6 =01

Stress

TCODE,7 =0

Real

Description

2

AS

RS

Axial Stress

3

MSA

RS

Axial Safety Margin*

4

TS

RS

Torsional Stress

5

MST

RS

Torsional Safety Margin*

TCODE,7 =1

Real / Imaginary

2

ASR

RS

Axial Stress

3

ASI

RS

Axial Stress

4

TSR

RS

Torsional Stress

5

TSI

RS

Torsional Stress

TCODE,7 =2

Random Response

2

AS

RS

Axial Stress

3

TS

RS

Torsional Stress

End TCODE,7 End SCODE,6 ELTYPE =02

Beam element (CBEAM)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

GRID

I

External Grid Point identification number

3

SD

RS

Station Distance/Length

4

EXC

RS

Long. Strain at Point C

5

EXD

RS

Long. Strain at Point D

6

EXE

RS

Long. Strain at Point E

7

EXF

RS

Long. Strain at Point F

8

EMAX

RS

Maximum stress

DMAP Programmer’s Guide

5-93

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

9

EMIN

RS

Minimum stress

10

MST

RS

Margin of Safety in Tension

11

MSC

RS

Margin of Safety in Compression

Words 2 through 11 repeat 011 times TCODE,7 =1

Real / Imaginary

2

GRID

I

External Grid Point identification number

3

SD

RS

Station Distance/Length

4

ERCR

RS

Long. Strain at Point C

5

EXDR

RS

Long. Strain at Point D

6

EXER

RS

Long. Strain at Point E

7

EXFR

RS

Long. Strain at Point F

8

EXCI

RS

Long. Strain at Point C

9

EXDI

RS

Long. Strain at Point D

10

EXEI

RS

Long. Strain at Point E

11

EXFI

RS

Long. Strain at Point F

Words 2 through 11 repeat 011 times TCODE,7 =2

Random Response

2

GRID

I

External Grid Point identification number

3

SD

RS

Station Distance/Length

4

EXC

RS

Long. Strain at Point C

5

EXD

RS

Long. Strain at Point D

6

EXE

RS

Long. Strain at Point E

7

EXF

RS

Long. Strain at Point F

Words 2 through 7 repeat 011 times End TCODE,7 SCODE,6 =01

5-94

DMAP Programmer’s Guide

Stress

Data Block Descriptions O-V

Name

Word TCODE,7 =0

Type

Description

Real

2

GRID

I

External Grid Point identification number

3

SD

RS

Station Distance/Length

4

SXC

RS

Long. Stress at Point C

5

SXD

RS

Long. Stress at Point D

6

SXE

RS

Long. Stress at Point E

7

SXF

RS

Long. Stress at Point F

8

SMAX

RS

Maximum stress

9

SMIN

RS

Minimum stress

10

MST

RS

Margin of Safety in Tension

11

MSC

RS

Margin of Safety in Compression

Words 2 through 11 repeat 011 times TCODE,7=1

Real/Imaginary

2

GRID

I

External Grid Point identification number

3

SD

RS

Station Distance/Length

4

SRCR

RS

Long. Stress at Point C

5

SXDR

RS

Long. Stress at Point D

6

SXER

RS

Long. Stress at Point E

7

SXFR

RS

Long. Stress at Point F

8

SXCI

RS

Long. Stress at Point C

9

SXDI

RS

Long. Stress at Point D

10

SXEI

RS

Long. Stress at Point E

11

SXFI

RS

Long. Stress at Point F

Words 2 through 11 repeat 011 times TCODE,7 =2 2

Random Response GRID

I

External Grid Point identification number

DMAP Programmer’s Guide

5-95

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

3

SD

RS

Station Distance/Length

4

SXC

RS

Long. Stress at Point C

5

SXD

RS

Long. Stress at Point D

6

SXE

RS

Long. Stress at Point E

7

SXF

RS

Long. Stress at Point F

Words 2 through 7 repeat 011 times End TCODE,7 End SCODE,6 ELTYPE=03

Tube element (CTUBE)

SCODE,6=0

Strain

TCODE,7 =0

Real

2

AE

RS

Axial Strain

3

MSA

RS

Axial Safety Margin*

4

TE

RS

Torsional Strain

5

MST

RS

Torsional Safety Margin*

TCODE,7=1

Real / Imaginary

2

AER

RS

Axial Strain

3

AEI

RS

Axial Strain

4

TER

RS

Torsional Strain

5

TEI

RS

Torsional Strain

TCODE,7 =2

Random Response

2

AE

RS

Axial Strain

3

TE

RS

Torsional Strain

End TCODE,7 SCODE,6 =01

5-96

DMAP Programmer’s Guide

Stress

Data Block Descriptions O-V

Name

Word TCODE,7 =0

Type

Description

Real

2

AS

RS

Axial Stress

3

MSA

RS

Axial Safety Margin*

4

TS

RS

Torsional Stress

5

MST

RS

Torsional Safety Margin*

TCODE,7 =1

Real / Imaginary

2

ASR

RS

Axial Stress

3

ASI

RS

Axial Stress

4

TSR

RS

Torsional Stress

5

TSI

RS

Torsional Stress

TCODE,7 =2

Random Response

2

AS

RS

Axial Stress

3

TS

RS

Torsional Stress

End TCODE,7 End SCODE,6 ELTYPE =04

Shear panel element (CSHEAR)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

ETMAX

RS

Maximum Shear

3

ETAVG

RS

Average Shear

4

MS

RS

Safety Margin*

TCODE,7 =1

Real / Imaginary

2

ETMAXR

RS

Maximum Shear

3

ETMAXI

RS

Maximum Shear

4

ETAVGR

RS

Average Shear

5

ETAVGI

RS

Average Shear

DMAP Programmer’s Guide

5-97

Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7 =2

Type

Description

Random Response

2

ETMAX

RS

Maximum Shear

3

ETAVG

RS

Average Shear

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

TMAX

RS

Maximum Shear

3

TAVG

RS

Average Shear

4

MS

RS

Safety Margin*

TCODE,7 =1

Real / Imaginary

2

TMAXR

RS

Maximum Shear

3

TMAXI

RS

Maximum Shear

4

TAVGR

RS

Average Shear

5

TAVGI

RS

Average Shear

TCODE,7 =2

Random Response

2

TMAX

RS

Maximum Shear

3

TAVG

RS

Average Shear

End TCODE,7 End SCODE,6 ELTYPE =05 2

FORCE1/FORCE2/MOMENT1/MOMENT2 (follower stiffness) UNDEF

ELTYPE =06 2

Unused UNDEF

ELTYPE =07 2

5-98

None

None PLOAD4 (follower stiffness)

UNDEF

DMAP Programmer’s Guide

None

Data Block Descriptions O-V

Name

Word ELTYPE =08 2

Description

PLOADX1 (follower stiffness) UNDEF

ELTYPE =09 2

Type

None PLOAD and PLOAD2 (follower stiffness)

UNDEF

None

Name

Word

Type

Description

ELTYPE =10

Rod element connection and property (CONROD)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

AE

RS

Axial Strain

3

MSA

RS

Axial Safety Margin*

4

TE

RS

Torsional Strain

5

MST

RS

Torsional Safety Margin*

TCODE,7 =1

Real / Imaginary

2

AER

RS

Axial Strain

3

AEI

RS

Axial Strain

4

TER

RS

Torsional Strain

5

TEI

RS

Torsional Strain

TCODE,7 =2

Random Response

2

AE

RS

Axial Strain

3

TE

RS

Torsional Strain

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

AS

RS

Axial Stress

3

MSA

RS

Axial Safety Margin*

DMAP Programmer’s Guide

5-99

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

4

TS

RS

Torsional Stress

5

MST

RS

Torsional Safety Margin*

TCODE,7 =1

Real / Imaginary

2

ASR

RS

Axial Stress

3

ASI

RS

Axial Stress

4

TSR

RS

Torsional Stress

5

TSI

RS

Torsional Stress

TCODE,7 =2

Random Response

2

AS

RS

Axial Stress

3

TS

RS

Torsional Stress

End TCODE,7 End SCODE,6 ELTYPE =11

Scalar spring element (CELAS1)

SCODE,6 =0

Strain

TCODE,7 =0 or 2

Real or Random Response

2

RS

E

TCODE,7 =1

Real / Imaginary

2

ER

RS

3

EI

RS

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0 or 2

Real or Random Response

2

RS

S

TCODE,7 =1

Stress

Real / Imaginary

2

SR

RS

Stress

3

SI

RS

Stress

5-100

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

End TCODE,7 End SCODE,6 ELTYPE =12

Scalar spring element with properties (CELAS2)

SCODE,6 =0

Strain

TCODE,7 =0 or 2

Real or Random Response

2

RS

E

TCODE,7 =1

Real / Imaginary

2

ER

RS

3

EI

RS

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0 or 2

Real or Random Response

2

RS

S

TCODE,7 =1

Stress

Real/Imaginary

2

SR

RS

Stress

3

SI

RS

Stress

End TCODE,7 End SCODE,6 ELTYPE =13

Scalar spring element to scalar points only (CELAS3)

SCODE,6 =0

Strain

TCODE,7 =0 or 2

Real or Random Response

2

RS

E

TCODE,7 =1

Real / Imaginary

2

ER

RS

3

EI

RS

End TCODE,7

DMAP Programmer’s Guide

5-101

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

SCODE,6 =01

Stress

TCODE,7 =0 or 2

Real or Random Response

2

S

RS

Stress

2

SR

RS

Stress

3

SI

RS

Stress

TCODE,7 =1

End TCODE,7 End SCODE,6 ELTYPE =14 2

Scalar spring element to scalar points only with properties (CELAS4) UNDEF

ELTYPE =15 2

AEROT3 UNDEF

ELTYPE =16 2 ELTYPE =17

ELTYPE =18

ELTYPE =19

Name

ELTYPE =20 2

5-102

None Type

Description

Scalar damper (CDAMP1) UNDEF

ELTYPE =21 2

None Unused (pre-V69 QUAD1 Same as TRIA1)

UNDEF Word

None Unused (pre-V69 QUAD2 Same as TRIA1)

UNDEF

2

None Unused (pre-V69 TRIA2 Same as TRIA1)

UNDEF

2

None AEROBEAM

UNDEF

2

None

None Scalar damper with properties (CDAMP2)

UNDEF

DMAP Programmer’s Guide

None

Data Block Descriptions O-V

Name

Word ELTYPE =22 2

Description

Scalar damper to scalar points only (CDAMP3) UNDEF

ELTYPE =23 2

Type

None Scalar damper to scalar points only with properties (CDAMP4)

UNDEF

None

ELTYPE =24

Viscous damper (CVISC)

TCODE,7 =0

Real

2

UNDEF

TCODE,7 =1

None Real / Imaginary

2

ASR

RS

Axial Stress

3

ASI

RS

Axial Stress

4

TAUR

RS

Torque

5

TAUI

RS

Torque

TCODE,7 =2

Random Response

2

AS

RS

Axial Stress

3

TAU

RS

Torque

End TCODE,7 ELTYPE =25 2

Scalar mass (CMASS1) UNDEF

ELTYPE =26 2

Scalar mass with properties (CMASS2) UNDEF

ELTYPE =27 2

UNDEF

None Scalar mass to scalar pts. only with properties (CMASS4)

UNDEF

ELTYPE =29 2

None Scalar mass to scalar points only (CMASS3)

ELTYPE =28 2

None

None Concentrated mass element - general form (CONM1)

UNDEF

None

DMAP Programmer’s Guide

5-103

Chapter 5

Data Block Descriptions O-V

Name

Word ELTYPE =30 2 ELTYPE =31

None Dummy plot element (PLOTEL)

UNDEF

ELTYPE =32 2

Description

Concentrated mass element - rigid body form (CONM2) UNDEF

2

Type

None Unused

UNDEF

None

ELTYPE =33

Quadrilateral plate element (CQUAD4)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5

EXY1

RS

Shear in xy at Z1

6

EA1

RS

Theta ( Shear Angle ) at Z1

7

EMJRP1

RS

Major Principal at Z1

8

EMNRP1

RS

Minor Principal at Z1

9

EMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

EX2

RS

Normal in x at Z2

12

EY2

RS

Normal in y at Z2

13

EXY2

RS

Shear in xy at Z2

14

EA2

RS

Theta (Shear Angle) at Z2

15

EMJRP2

RS

Major Principal at Z2

16

EMNRP2

RS

Minor Principal at Z2

17

EMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

5-104

DMAP Programmer’s Guide

Real / Imaginary

Data Block Descriptions O-V

Name

Word

Type

Description

2

FD1

RS

Z1 = Fibre Distance

3

EX1R

RS

Normal in x at Z1

4

EX1I

RS

Normal in x at Z1

5

EY1R

RS

Normal in y at Z1

6

EY1I

RS

Normal in y at Z1

7

EXY1R

RS

Shear in xy at Z1

8

EXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

EX2R

RS

Normal in x at Z2

11

EX2I

RS

Normal in x at Z2

12

EY2R

RS

Normal in y at Z2

13

EY2I

RS

Normal in y at Z2

14

EXY2R

RS

Shear in xy at Z2

15

EXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5

EXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

EX2

RS

Normal in x at Z2

8

EY2

RS

Normal in y at Z2

9

EXY2

RS

Shear in xy at Z2

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

DMAP Programmer’s Guide

5-105

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

SA1

RS

Theta ( Shear Angle ) at Z1

7

SMJRP1

RS

Major Principal at Z1

8

SMNRP1

RS

Minor Principal at Z1

9

SMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

SX2

RS

Normal in x at Z2

12

SY2

RS

Normal in y at Z2

13

TXY2

RS

Shear in xy at Z2

14

SA2

RS

Theta (Shear Angle) at Z2

15

SMJRP2

RS

Major Principal at Z2

16

SMNRP2

RS

Minor Principal at Z2

17

SMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

Real / Imaginary

2

FD1

RS

Z1 = Fibre Distance

3

SX1R

RS

Normal in x at Z1

4

SX1I

RS

Normal in x at Z1

5

SY1R

RS

Normal in y at Z1

6

SY1I

RS

Normal in y at Z1

7

TXY1R

RS

Shear in xy at Z1

8

TXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

SX2R

RS

Normal in x at Z2

5-106

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

11

SX2I

RS

Normal in x at Z2

12

SY2R

RS

Normal in y at Z2

13

SY2I

RS

Normal in y at Z2

14

TXY2R

RS

Shear in xy at Z2

15

TXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

SX2

RS

Normal in x at Z2

8

SY2

RS

Normal in y at Z2

9

TXY2

RS

Shear in xy at Z2

End TCODE,7 End SCODE,6 ELTYPE =34

Simple beam element (CBAR and see also ELTYPE=100)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

EX1A

RS

SA1

3

EX2A

RS

SA2

4

EX3A

RS

SA3

5

EX4A

RS

SA4

6

AE

RS

Axial

7

EBMAXA

RS

SA maximum

8

EBMINA

RS

SA minimum

DMAP Programmer’s Guide

5-107

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

9

MST

RS

Safety Margin in Tension*

10

EXIB

RS

SB1

11

EX2B

RS

SB2

12

EX3B

RS

SB3

13

EX4B

RS

SB4

14

EBMAXB

RS

SB maximum

15

EBMINB

RS

SB minimum

16

MSC

RS

Safety Margin in Comp*

TCODE,7 =1

Real / Imaginary

2

EX1AR

RS

SA1

3

EX2AR

RS

SA2

4

EX3AR

RS

SA3

5

EX4AR

RS

SA4

6

AER

RS

Axial

7

EX1AI

RS

SA1

8

EX2AI

RS

SA2

9

EX3AI

RS

SA3

10

EX4AI

RS

SA4

11

AEI

RS

Axial

12

EX1BR

RS

SB1

13

EX2BR

RS

SB2

14

EX3BR

RS

SB3

15

EX4BR

RS

SB4

16

EX1BI

RS

SB1

17

EX2BI

RS

SB2

18

EX3BI

RS

SB3

5-108

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word 19

EX4BI

TCODE,7 =2

Type RS

Description SB4

Random Response

2

EX1A

RS

SA1

3

EX2A

RS

SA2

4

EX3A

RS

SA3

5

EX4A

RS

SA4

6

AE

RS

Axial

7

EX1B

RS

SB1

8

EX2B

RS

SB2

9

EX3B

RS

SB3

10

EX4B

RS

SB4

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

SX1A

RS

SA1

3

SX2A

RS

SA2

4

SX3A

RS

SA3

5

SX4A

RS

SA4

6

AS

RS

Axial

7

BMAXA

RS

SA maximum

8

BMINA

RS

SA minimum

9

MST

RS

Safety Margin in Tension

10

SX1B

RS

SB1

11

SX2B

RS

SB2

12

SX3B

RS

SB3

13

SX4B

RS

SB4

DMAP Programmer’s Guide

5-109

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

14

BMAXB

RS

SB maximum

15

BMINB

RS

SB minimum

16

MSC

RS

Safety Margin in Comp*

TCODE,7 =1

Real / Imaginary

2

SX1AR

RS

SA1

3

SX2AR

RS

SA2

4

SX3AR

RS

SA3

5

SX4AR

RS

SA4

6

ASR

RS

Axial

7

SX1AI

RS

SA1

8

SX2AI

RS

SA2

9

SX3AI

RS

SA3

10

SX4AI

RS

SA4

11

ASI

RS

Axial

12

SX1BR

RS

SB1

13

SX2BR

RS

SB2

14

SX3BR

RS

SB3

15

SX4BR

RS

SB4

16

SX1BI

RS

SB1

17

SX2BI

RS

SB2

18

SX3BI

RS

SB3

19

SX4BI

RS

SB4

TCODE,7 =2

Random Response

2

SX1A

RS

SA1

3

SX2A

RS

SA2

4

SX3A

RS

SA3

5-110

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

5

SX4A

RS

SA4

6

AS

RS

Axial

7

SX1B

RS

SB1

8

SX2B

RS

SB2

9

SX3B

RS

SB3

10

SX4B

RS

SB4

End TCODE,7 End SCODE,6 ELTYPE =35

Axisymmetric shell element (CCONEAX)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

HOPA

RS

Harmonic or point angle

3

FD1

RS

Z1=Fibre Distance

4

EU1

RS

Normal in u at z1

5

EV1

RS

Normal in v at z1

6

ET1

RS

Shear in uv at z1

7

A1

RS

Theta (Shear Angle) at z1

8

EMJRP1

RS

Major Principal at z1

9

EMNRP1

RS

Minor Principal at z1

10

ETMAX1

RS

Maximum Shear at z1

11

FD2

RS

Z2=Fibre Distance

12

EU2

RS

Normal in u at z2

13

EV2

RS

Normal in v at z2

14

ET2

RS

Shear in uv at z2

15

A2

RS

Theta (Shear Angle) at z2

16

EMJRP2

RS

Major Principal at z2

DMAP Programmer’s Guide

5-111

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

17

EMNRP2

RS

Minor Principal at z2

18

ETMAX2

RS

Maximum Shear at z2

TCODE,7 =1 2

Real / Imaginary UNDEF

TCODE,7 =2 2

None Random Response

UNDEF

None

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

HOPA

RS

Harmonic or point angle

3

FD1

RS

Z1=Fibre Distance

4

SU1

RS

Normal in u at z1

5

SV1

RS

Normal in v at z1

6

ST1

RS

Shear in uv at z1

7

A1

RS

Theta (Shear Angle) at z1

8

SMJRP1

RS

Major Principal at z1

9

SMNRP1

RS

Minor Principal at z1

10

STMAX1

RS

Maximum Shear at z1

11

FD2

RS

Z2=Fibre Distance

12

SU2

RS

Normal in u at z2

13

SV2

RS

Normal in v at z2

14

ST2

RS

Shear in uv at z2

15

A2

RS

Theta (Shear Angle) at z2

16

SMJRP2

RS

Major Principal at z2

17

SMNRP2

RS

Minor Principal at z2

18

STMAX2

RS

Maximum Shear at z2

5-112

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word TCODE,7 =1 2

Description

Real / Imaginary UNDEF

TCODE,7 =2 2

Type

None Random Response

UNDEF

None

End TCODE,7 End SCODE,6 ELTYPE =36 2

Unused (Pre-V69 CTRIARG) UNDEF

ELTYPE =37 2

None Unused (Pre-V69 CTRAPRG)

UNDEF

ELTYPE =38

None Gap element (CGAP)

2

FX

RS

3

SFY

RS

4

SFZ

RS

5

U

RS

6

V

RS

7

W

RS

8

SV

RS

9

SW

RS

ELTYPE =39

Tetra

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Grid or Gaus

4

NODEF

I

Number of Active Points

5

GRID

I

External grid ID (0=center)

DMAP Programmer’s Guide

5-113

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

6

EX

RS

Normal in x

7

ETXY

RS

Shear in xy

8

EP1

RS

First principal stress

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

EPR

RS

Mean pressure

13

EOCT

RS

Octahedral shear stress

14

EY

RS

Normal in y

15

ETYZ

RS

Shear in yz

16

EP2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

EZ

RS

Normal in z

21

ETZX

RS

Shear in zx

22

EP3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 repeat 005 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid ID (0=center)

5-114

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

6

EXR

RS

Normal in x

7

EYR

RS

Normal in y

8

EZR

RS

Normal in z

9

ETXYR

RS

Shear in xy

10

ETYZR

RS

Shear in yz

11

ETZXR

RS

Shear in zx

12

EXI

RS

Normal in x

13

EYI

RS

Normal in y

14

EZI

RS

Normal in z

15

ETXYI

RS

Shear in xy

16

ETYZI

RS

Shear in yz

17

ETZXI

RS

Shear in zx

Words 5 through 17 repeat 005 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid ID (0=center)

6

EX

RS

Normal in x

7

EY

RS

Normal in y

8

EZ

RS

Normal in z

9

ETXY

RS

Shear in xy

10

ETYZ

RS

Shear in yz

11

ETZX

RS

Shear in zx

Words 5 through 11 repeat 005 times End TCODE,7

DMAP Programmer’s Guide

5-115

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

SCODE,6 =01

Stress

TCODE,7 =0

Real

Description

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

TXY

RS

Shear in xy

8

P1

RS

First principal stress

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

PR

RS

Mean pressure

13

OCT

RS

Octahedral shear stress

14

SY

RS

Normal in y

15

TYZ

RS

Shear in yz

16

P2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

SZ

RS

Normal in z

21

TZX

RS

Shear in zx

22

P3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

5-116

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

Words 5 through 25 repeat 005 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SXR

RS

Normal in x

7

SYR

RS

Normal in y

8

SZR

RS

Normal in z

9

TXYR

RS

Shear in xy

10

TYZR

RS

Shear in yz

11

TZXR

RS

Shear in zx

12

SXI

RS

Normal in x

13

SYI

RS

Normal in y

14

SZI

RS

Normal in z

15

TXYI

RS

Shear in xy

16

TYZI

RS

Shear in yz

17

TZXI

RS

Shear in zx

Words 5 through 17 repeat 005 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

SY

RS

Normal in y

DMAP Programmer’s Guide

5-117

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

SZ

RS

Normal in z

9

TXY

RS

Shear in xy

10

TYZ

RS

Shear in yz

11

TZX

RS

Shear in zx

Words 5 through 11 repeat 005 times End TCODE,7 End SCODE,6 Name

Word

Type

Description

ELTYPE =40

Rod type spring and damper (CBUSH1D)

TCODE,7 =0

Real

2

FE

RS

Element Force

3

UE

RS

Axial Displacement

4

VE

RS

Axial Velocity*

5

AS

RS

Axial Stress*

6

AE

RS

Axial Strain*

7

EP

RS

Plastic Strain*

8

FAIL

I

Failed Element Flag

TCODE,7 =1

Real / Imaginary

2

FER

RS

Element Force

3

UER

RS

Axial Displacement

4

ASR

RS

Axial Stress*

5

AER

RS

Axial Strain*

6

FEI

RS

Element Force

7

UEI

RS

Axial Displacement

8

ASI

RS

Axial Stress*

9

AEI

RS

Axial Strain*

5-118

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word TCODE,7 =2

Type

Description

Random Response

2

FE

RS

Element Force

3

UE

RS

Axial Displacement

4

AS

RS

Axial Stress*

5

AE

RS

Axial Strain*

End TCODE,7 ELTYPE =41 2

Unused (Pre-V69 CHEXA1) UNDEF

ELTYPE =42 2

Unused (Pre-V69 CHEXA2) UNDEF

ELTYPE =43 2

UNDEF

UNDEF

None Fluid element with 4 points (CFLUID4)

UNDEF

ELTYPE =46 2

None Fluid element with 3 points (CFLUID3)

ELTYPE =45 2

None Fluid element with 2 points (CFLUID2)

ELTYPE =44 2

None

None Cflmass

UNDEF

None

ELTYPE =47

Fluid element with 2 points (CAXIF2)

TCODE,7 =0 or 2

Real or Random Response

2

RA

RS

Radial Axis

3

AA

RS

Axial Axis

4

TE

RS

Tangential Edge

5

CE

RS

Circumferential Edge

TCODE,7 =1 2

Real / Imaginary RAR

RS

Radial Axis

DMAP Programmer’s Guide

5-119

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

3

AAR

RS

Axial Axis

4

TER

RS

Tangential Edge

5

CER

RS

Circumferential Edge

6

RAI

RS

Radial Axis

7

AAI

RS

Axial Axis

8

TEI

RS

Tangential Edge

9

CEI

RS

Circumferential Edge

End TCODE,7 ELTYPE =48

Fluid element with 3 points (CAXIF3)

TCODE,7 =0 or 2

Real or Random Response

2

RC

RS

Radial centroid

3

CC

RS

Circumferential centroid

4

AC

RS

Axial centroid

5

TE1

RS

Tangential edge 1

6

CE1

RS

Circumferential edge 1

7

TE2

RS

Tangential edge 2

8

CE2

RS

Circumferential edge 2

9

TE3

RS

Tangential edge 3

10

CE3

RS

Circumferential edge 3

TCODE,7 =1

Real / Imaginary

2

RCR

RS

Radial centroid

3

CCR

RS

Circumferential centroid

4

ACR

RS

Axial centroid

5

TE1R

RS

Tangential edge 1

6

CE1R

RS

Circumferential edge 1

7

TE2R

RS

Tangential edge 2

5-120

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

8

CE2R

RS

Circumferential edge 2

9

TE3R

RS

Tangential edge 3

10

CE3R

RS

Circumferential edge 3

11

RCI

RS

Radial centroid

12

CCI

RS

Circumferential centroid

13

ACR

RS

Axial centroid

14

TE1I

RS

Tangential edge 1

15

CE1I

RS

Circumferential edge 1

16

TE2I

RS

Tangential edge 2

17

CE2I

RS

Circumferential edge 2

18

TE3I

RS

Tangential edge 3

19

CE3I

RS

Circumferential edge 3

End TCODE,7 ELTYPE =49

Fluid element with 4 points (CAXIF4)

TCODE,7 =0 or 2

Real or Random Response

2

RC

RS

Radial centroid

3

CC

RS

Circumferential centroid

4

AC

RS

Axial centroid

5

TE1

RS

Tangential edge 1

6

CE1

RS

Circumferential edge 1

7

TE2

RS

Tangential edge 2

8

CE2

RS

Circumferential edge 2

9

TE3

RS

Tangential edge 3

10

CE3

RS

Circumferential edge 3

11

TE4

RS

Tangential edge 4

12

CE4

RS

Circumferential edge 4

DMAP Programmer’s Guide

5-121

Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7 =1

Type

Description

Real / Imaginary

2

RCR

RS

Radial centroid

3

CCR

RS

Circumferential centroid

4

ACR

RS

Axial centroid

5

TE1R

RS

Tangential edge 1

6

CE1R

RS

Circumferential edge 1

7

TE2R

RS

Tangential edge 2

8

CE2R

RS

Circumferential edge 2

9

TE3R

RS

Tangential edge 3

10

CE3R

RS

Circumferential edge 3

11

TE4R

RS

Tangential edge 4

12

CE4R

RS

Circumferential edge 4

13

RCI

RS

Radial centroid

14

CCI

RS

Circumferential centroid

15

ACR

RS

Axial centroid

16

TE1I

RS

Tangential edge 1

17

CE1I

RS

Circumferential edge 1

18

TE2I

RS

Tangential edge 2

19

CE2I

RS

Circumferential edge 2

20

TE3I

RS

Tangential edge 3

21

CE3I

RS

Circumferential edge 3

22

TE4I

RS

Tangential edge 4

23

CE4I

RS

Circumferential edge 4

End TCODE,7 Word

Name

ELTYPE =50

5-122

DMAP Programmer’s Guide

Type

Description

Three-point slot element (CSLOT3)

Data Block Descriptions O-V

Name

Word

Type

Description

TCODE,7 =0 or 2

Real or Random Response

2

RC

RS

Radial centroid

3

AC

RS

Axial centroid

4

TE1

RS

Tangential edge 1

5

TE2

RS

Tangential edge 2

6

TE3

RS

Tangential edge 3

TCODE,7 =1

Real / Imaginary

2

RCR

RS

Radial centroid

3

ACR

RS

Axial centroid

4

TE1R

RS

Tangential edge 1

5

TE2R

RS

Tangential edge 2

6

TE3R

RS

Tangential edge 3

7

RCI

RS

Radial centroid

8

ACI

RS

Axial centroid

9

TE1I

RS

Tangential edge 1

10

TE2I

RS

Tangential edge 2

11

TE3I

RS

Tangential edge 3

End TCODE,7 ELTYPE =51

Four-point slot element (CSLOT4)

TCODE,7 =0 or 2

Real or Random Response

2

RC

RS

Radial centroid

3

AC

RS

Axial centroid

4

TE1

RS

Tangential edge 1

5

TE2

RS

Tangential edge 2

6

TE3

RS

Tangential edge 3

7

TE4

RS

Tangential edge 4

DMAP Programmer’s Guide

5-123

Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7 =1

Type

Description

Real / Imaginary

2

RCR

RS

Radial centroid

3

ACR

RS

Axial centroid

4

TE1R

RS

Tangential edge 1

5

TE2R

RS

Tangential edge 2

6

TE3R

RS

Tangential edge 3

7

TE4R

RS

Tangential edge 4

8

RCI

RS

Radial centroid

9

ACI

RS

Axial centroid

10

TE1I

RS

Tangential edge 1

11

TE2I

RS

Tangential edge 2

12

TE3I

RS

Tangential edge 3

13

TE4I

RS

Tangential edge 4

End TCODE,7 ELTYPE =52 2

Heat transfer plot element for CHBDYG and CHBDYP UNDEF

None

ELTYPE =53

Axisymmetric triangular element (CTRIAX6)

TCODE,7 =0

Real

2

LOC

I

Location Code

3

RS

RS

Radial Stress

4

AZS

RS

Azimuthal Stress

5

AS

RS

Axial Stress

6

SS

RS

Shear Stress

7

MAXP

RS

Maximum Principal

8

TMAX

RS

Maximum Shear

9

OCTS

RS

Octahedral

5-124

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

Words 2 through 9 repeat 004 times TCODE,7 =1

Real / Imaginary

2

LOC

I

Location Code

3

RSR

RS

Radial Stress

4

RSI

RS

Radial Stress

5

AZSR

RS

Azimuthal Stress

6

AZSI

RS

Azimuthal Stress

7

ASR

RS

Axial Stress

8

ASI

RS

Axial Stress

9

SSR

RS

Shear Stress

10

SSI

RS

Shear Stress

Words 2 through 10 repeat 004 times TCODE,7 =2

Random Response

2

LOC

I

Location Code

3

RS

RS

Radial Stress

4

AZS

RS

Azimuthal Stress

5

AS

RS

Axial Stress

6

SS

RS

Shear Stress

7

MAXP

RS

Maximum Principal

8

TMAX

RS

Maximum Shear

9

OCTS

RS

Octahedral

Words 2 through 6 repeat 004 times End TCODE,7 ELTYPE =54 2 ELTYPE =55

Unused (Pre-V69 CTRIM6) UNDEF

None Three-point dummy element (CDUM3)

DMAP Programmer’s Guide

5-125

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

TCODE,7 =0 or 2

Real or Random Response

2

RS

S(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

SR(9)

RS

User defined - real/mag.

11

SI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =56

Four-point dummy element (CDUM4)

TCODE,7 =0 or 2

Real or Random Response

2

RS

S(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

SR(9)

RS

User defined - real/mag.

11

SI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =57

Five-point dummy element (CDUM5)

TCODE,7 =0 or 2

Real or Random Response

2

RS

S(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

SR(9)

RS

User defined - real/mag.

11

SI(9)

RS

User defined - mag./phase

End TCODE,7 ELTYPE =58

Six-point dummy element (CDUM6)

TCODE,7 =0 or 2

Real or Random Response

2

RS

S(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

SR(9)

RS

User defined - real/mag.

11

SI(9)

RS

User defined - mag./phase

5-126

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

End TCODE,7 ELTYPE =59

Seven-point dummy element (CDUM7)

TCODE,7 =0 or 2

Real or Random Response

2

RS

S(9)

TCODE,7 =1

User defined

Real/imaginary or magnitude/phase

2

SR(9)

RS

User defined - real/mag.

11

SI(9)

RS

User defined - mag./phase

End TCODE,7 Name

Word ELTYPE =60

Type

Description

Two-dimensional crack tip element (CRAC2D or CDUM8)

2

X

RS

X coordinate

3

Y

RS

Y coordinate

4

SX

RS

Normal X

5

SY

RS

Normal Y

6

TXY

RS

Shear XY

7

KI

RS

Stress Intensity Factor KI

8

KII

RS

Stress Intensity Factor KII

9

S8

RS

10

S9

RS

ELTYPE =61

Three-dimensional crack tip element (CRAC3D or CDUM9)

2

X

RS

Normal X

3

Y

RS

Normal Y

4

Z

RS

Normal Z

5

TXY

RS

Shear XY

6

TYZ

RS

Shear YZ

7

TZX

RS

Shear ZX

DMAP Programmer’s Guide

5-127

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

KI

RS

Stress Intensity Factor KI

9

KII

RS

Stress Intensity Factor KII

10

KIII

RS

Stress Intensity Factor KIII

ELTYPE =62 2

Unused (Pre-V69 CQDMEM1) UNDEF

ELTYPE =63 2

None Unused (Pre-V69 CQDMEM2)

UNDEF

None

ELTYPE =64

Curved quadrilateral shell element (CQUAD8)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

EMJRP1

RS

Major Principal at Z1

10

EMNRP1

RS

Minor Principal at Z1

11

ETMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

EX2

RS

Normal in x at Z2

14

EY2

RS

Normal in y at Z2

15

ETXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

EMRPJ2

RS

Major Principal at Z2

5-128

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

18

EMNRP2

RS

Minor Principal at Z2

19

ETMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 005 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1R

RS

Normal in x at Z1

6

EX1I

RS

Normal in x at Z1

7

EY1R

RS

Normal in y at Z1

8

EY1I

RS

Normal in y at Z1

9

ETXY1R

RS

Shear in xy at Z1

10

ETXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

EX2R

RS

Normal in x at Z2

13

EX2I

RS

Normal in x at Z2

14

EY2R

RS

Normal in y at Z2

15

EY2I

RS

Normal in y at Z2

16

ETXY2R

RS

Shear in xy at Z2

17

ETXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 005 times TCODE,7 =2

Random Response

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

DMAP Programmer’s Guide

5-129

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

EX2

RS

Normal in x at Z2

10

EY2

RS

Normal in y at Z2

11

ETXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 005 times End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

7

TXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

SMJRP1

RS

Major Principal at Z1

10

SMNRP1

RS

Minor Principal at Z1

11

TMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

SX2

RS

Normal in x at Z2

14

SY2

RS

Normal in y at Z2

15

TXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

5-130

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

17

SMJRP2

RS

Major Principal at Z2

18

SMNRP2

RS

Minor Principal at Z2

19

TMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 005 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

3

GRID

I

Number active grids identification numbers or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1R

RS

Normal in x at Z1

6

SX1I

RS

Normal in x at Z1

7

SY1R

RS

Normal in y at Z1

8

SY1I

RS

Normal in y at Z1

9

TXY1R

RS

Shear in xy at Z1

10

TXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

SX2R

RS

Normal in x at Z2

13

SX2I

RS

Normal in x at Z2

14

SY2R

RS

Normal in y at Z2

15

SY2I

RS

Normal in y at Z2

16

TXY2R

RS

Shear in xy at Z2

17

TXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 005 times TCODE,7 =2

Random Response

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

DMAP Programmer’s Guide

5-131

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

EX2

RS

Normal in x at Z2

10

EY2

RS

Normal in y at Z2

11

ETXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 005 times End TCODE,7 End SCODE,6 ELTYPE =65 2

Unused (Pre-V69 CHEX8) UNDEF

ELTYPE =66 2

None Unused (Pre-V69 CHEX20)

UNDEF

None

ELTYPE =67

Hexa

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Grid or Gaus

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

EX

RS

Normal in x

7

ETXY

RS

Shear in xy

8

EP1

RS

First principal stress

9

P1X

RS

First principal x cosine

5-132

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

EPR

RS

Mean pressure

13

EOCT

RS

Octahedral shear stress

14

EY

RS

Normal in y

15

ETYZ

RS

Shear in yz

16

EP2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

EZ

RS

Normal in z

21

ETZX

RS

Shear in zx

22

EP3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 repeat 009 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

EXR

RS

Normal in x

7

EYR

RS

Normal in y

8

EZR

RS

Normal in z

9

ETXYR

RS

Shear in xy

DMAP Programmer’s Guide

5-133

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

10

ETYZR

RS

Shear in yz

11

ETZXR

RS

Shear in zx

12

EXI

RS

Normal in x

13

EYI

RS

Normal in y

14

EZI

RS

Normal in z

15

ETXYI

RS

Shear in xy

16

ETYZI

RS

Shear in yz

17

ETZXI

RS

Shear in zx

Words 5 through 17 repeat 009 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

EX

RS

Normal in x

7

EY

RS

Normal in y

8

EZ

RS

Normal in z

9

ETXY

RS

Shear in xy

10

ETYZ

RS

Shear in yz

11

ETZX

RS

Shear in zx

Words 5 through 11 repeat 009 times End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate Type (BCD)

5-134

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

TXY

RS

Shear in xy

8

P1

RS

First principal stress

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

PR

RS

Mean pressure

13

OCT

RS

Octahedral shear stress

14

SY

RS

Normal in y

15

TYZ

RS

Shear in yz

16

P2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

SZ

RS

Normal in z

21

TZX

RS

Shear in zx

22

P3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 repeat 009 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

DMAP Programmer’s Guide

5-135

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SXR

RS

Normal in x

7

SYR

RS

Normal in y

8

SZR

RS

Normal in z

9

TXYR

RS

Shear in xy

10

TYZR

RS

Shear in yz

11

TZXR

RS

Shear in zx

12

SXI

RS

Normal in x

13

SYI

RS

Normal in y

14

SZI

RS

Normal in z

15

TXYI

RS

Shear in xy

16

TYZI

RS

Shear in yz

17

TZXI

RS

Shear in zx

Words 5 through 17 repeat 009 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

SY

RS

Normal in y

8

SZ

RS

Normal in z

9

TXY

RS

Shear in xy

10

TYZ

RS

Shear in yz

11

TZX

RS

Shear in zx

5-136

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

Words 5 through 11 repeat 009 times End TCODE,7 End SCODE,6 ELTYPE =68

Penta

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Grid or Gaus

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

EX

RS

Normal in x

7

ETXY

RS

Shear in xy

8

EP1

RS

First principal stress

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

EPR

RS

Mean pressure

13

EOCT

RS

Octahedral shear stress

14

EY

RS

Normal in y

15

ETYZ

RS

Shear in yz

16

EP2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

EZ

RS

Normal in z

21

ETZX

RS

Shear in zx

DMAP Programmer’s Guide

5-137

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

22

EP3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 repeat 007 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

EXR

RS

Normal in x

7

EYR

RS

Normal in y

8

EZR

RS

Normal in z

9

ETXYR

RS

Shear in xy

10

ETYZR

RS

Shear in yz

11

ETZXR

RS

Shear in zx

12

EXI

RS

Normal in x

13

EYI

RS

Normal in y

14

EZI

RS

Normal in z

15

ETXYI

RS

Shear in xy

16

ETYZI

RS

Shear in yz

17

ETZXI

RS

Shear in zx

Words 5 through 17 repeat 007 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

5-138

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

EX

RS

Normal in x

7

EY

RS

Normal in y

8

EZ

RS

Normal in z

9

ETXY

RS

Shear in xy

10

ETYZ

RS

Shear in yz

11

ETZX

RS

Shear in zx

Words 5 through 11 repeat 007 times End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

TXY

RS

Shear in xy

8

P1

RS

First principal stress

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

PR

RS

Mean pressure

13

OCT

RS

Octahedral shear stress

14

SY

RS

Normal in y

15

TYZ

RS

Shear in yz

DMAP Programmer’s Guide

5-139

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

16

P2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

SZ

RS

Normal in z

21

TZX

RS

Shear in zx

22

P3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 repeat 007 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SXR

RS

Normal in x

7

SYR

RS

Normal in y

8

SZR

RS

Normal in z

9

TXYR

RS

Shear in xy

10

TYZR

RS

Shear in yz

11

TZXR

RS

Shear in zx

12

SXI

RS

Normal in x

13

SYI

RS

Normal in y

14

SZI

RS

Normal in z

15

TXYI

RS

Shear in xy

5-140

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

16

TYZI

RS

Shear in yz

17

TZXI

RS

Shear in zx

Words 5 through 17 repeat 007 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

SY

RS

Normal in y

8

SZ

RS

Normal in z

9

TXY

RS

Shear in xy

10

TYZ

RS

Shear in yz

11

TZX

RS

Shear in zx

Words 5 through 11 repeat 007 times End TCODE,7 End SCODE,6 ELTYPE =69

Curved beam or pipe element (CBEND)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

GRID

I

External Grid Point identification number

3

CA

RS

Circumferential Angle

4

EC

RS

Long. strain at Point C

5

ED

RS

Long. strain at Point D

6

EE

RS

Long. strain at Point E

7

EF

RS

Long. strain at Point F

DMAP Programmer’s Guide

5-141

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

EMAX

RS

Maximum strain

9

EMIN

RS

Minimum strain

10

MST

RS

Margin of Safety in Tension

11

MSC

RS

Margin of Safety in Compression

Words 2 through 11 repeat 002 times TCODE,7 =1

Real / Imaginary

2

GRID

I

External Grid Point identification number

3

CA

RS

Circumferential Angle

4

ECR

RS

Long. strain at Point C

5

EDR

RS

Long. strain at Point D

6

EER

RS

Long. strain at Point E

7

EFR

RS

Long. strain at Point F

8

ECI

RS

Long. strain at Point C

9

EDI

RS

Long. strain at Point D

10

EEI

RS

Long. strain at Point E

11

EFI

RS

Long. strain at Point F

Words 2 through 11 repeat 002 times TCODE,7 =2

Random Response

2

GRID

I

External Grid Point identification number

3

CA

RS

Circumferential Angle

4

EC

RS

Long. strain at Point C

5

ED

RS

Long. strain at Point D

6

EE

RS

Long. strain at Point E

7

EF

RS

Long. strain at Point F

Words 2 through 7 repeat 002 times End TCODE,7

5-142

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

SCODE,6 =01

Stress

TCODE,7 =0

Real

Description

2

GRID

I

External Grid Point identification number

3

CA

RS

Circumferential Angle

4

SC

RS

Long. Stress at Point C

5

SD

RS

Long. Stress at Point D

6

SE

RS

Long. Stress at Point E

7

SF

RS

Long. Stress at Point F

8

SMAX

RS

Maximum stress

9

SMIN

RS

Minimum stress

10

MST

RS

Margin of Safety in Tension

11

MSC

RS

Margin of Safety in Compression

Words 2 through 11 repeat 002 times TCODE,7 =1

Real / Imaginary

2

GRID

I

External Grid Point identification number

3

CA

RS

Circumferential Angle

4

SCR

RS

Long. Stress at Point C

5

SDR

RS

Long. Stress at Point D

6

SER

RS

Long. Stress at Point E

7

SFR

RS

Long. Stress at Point F

8

SCI

RS

Long. Stress at Point C

9

SDI

RS

Long. Stress at Point D

10

SEI

RS

Long. Stress at Point E

11

SFI

RS

Long. Stress at Point F

Words 2 through 11 repeat 002 times TCODE,7 =2

Random Response

DMAP Programmer’s Guide

5-143

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

GRID

I

External Grid Point identification number

3

CA

RS

Circumferential Angle

4

SC

RS

Long. Stress at Point C

5

SD

RS

Long. Stress at Point D

6

SE

RS

Long. Stress at Point E

7

SF

RS

Long. Stress at Point F

Words 2 through 7 repeat 002 times End TCODE,7 End SCODE,6 Name

Word

Type

Description

ELTYPE =70

Triangular plate element (CTRIAR)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids ID or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

EMJRP1

RS

Major Principal at Z1

10

EMNRP1

RS

Minor Principal at Z1

11

ETMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

EX2

RS

Normal in x at Z2

5-144

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

14

EY2

RS

Normal in y at Z2

15

ETXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

EMJRP2

RS

Major Principal at Z2

18

EMNRP2

RS

Minor Principal at Z2

19

ETMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 004 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1R

RS

Normal in x at Z1

6

EX1I

RS

Normal in x at Z1

7

EY1R

RS

Normal in y at Z1

8

EY1I

RS

Normal in y at Z1

9

ETXY1R

RS

Shear in xy at Z1

10

ETXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

EX2R

RS

Normal in x at Z2

13

EX2I

RS

Normal in x at Z2

14

EY2R

RS

Normal in y at Z2

15

EY2I

RS

Normal in y at Z2

16

ETXY2R

RS

Shear in xy at Z2

17

ETXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 004 times TCODE,7 =2

Random Response

DMAP Programmer’s Guide

5-145

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

EX2

RS

Normal in x at Z2

10

EY2

RS

Normal in y at Z2

11

ETXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 004 times End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

7

TXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

MJRP1

RS

Major Principal at Z1

10

MNRP1

RS

Minor Principal at Z1

11

TMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

5-146

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

13

SX2

RS

Normal in x at Z2

14

SY2

RS

Normal in y at Z2

15

TXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

MJRP2

RS

Major Principal at Z2

18

MNRP2

RS

Minor Principal at Z2

19

TMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 004 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1R

RS

Normal in x at Z1

6

SX1I

RS

Normal in x at Z1

7

SY1R

RS

Normal in y at Z1

8

SY1I

RS

Normal in y at Z1

9

TXY1R

RS

Shear in xy at Z1

10

TXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

SX2R

RS

Normal in x at Z2

13

SX2I

RS

Normal in x at Z2

14

SY2R

RS

Normal in y at Z2

15

SY2I

RS

Normal in y at Z2

16

TXY2R

RS

Shear in xy at Z2

17

TXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 004 times

DMAP Programmer’s Guide

5-147

Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7 =2

Type

Description

Random Response

2

TERM

CHAR4

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

7

TXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

SX2

RS

Normal in x at Z2

10

SY2

RS

Normal in y at Z2

11

TXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 004 times End TCODE,7 End SCODE,6 ELTYPE =71 2

Unused UNDEF

ELTYPE =72 2

AEROQ4 UNDEF

ELTYPE =73 2

None

None Unused (Pre-V69 CFTUBE)

UNDEF

None

ELTYPE =74

Triangular shell element (CTRIA3)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5-148

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

5

EXY1

RS

Shear in xy at Z1

6

EA1

RS

Theta ( Shear Angle ) at Z1

7

EMJRP1

RS

Major Principal at Z1

8

EMNRP1

RS

Minor Principal at Z1

9

EMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

EX2

RS

Normal in x at Z2

12

EY2

RS

Normal in y at Z2

13

EXY2

RS

Shear in xy at Z2

14

EA2

RS

Theta (Shear Angle) at Z2

15

EMJRP2

RS

Major Principal at Z2

16

EMNRP2

RS

Minor Principal at Z2

17

EMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

Real / Imaginary

2

FD1

RS

Z1 = Fibre Distance

3

EX1R

RS

Normal in x at Z1

4

EX1I

RS

Normal in x at Z1

5

EY1R

RS

Normal in y at Z1

6

EY1I

RS

Normal in y at Z1

7

EXY1R

RS

Shear in xy at Z1

8

EXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

EX2R

RS

Normal in x at Z2

11

EX2I

RS

Normal in x at Z2

12

EY2R

RS

Normal in y at Z2

13

EY2I

RS

Normal in y at Z2

DMAP Programmer’s Guide

5-149

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

14

EXY2R

RS

Shear in xy at Z2

15

EXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5

EXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

EX2

RS

Normal in x at Z2

8

EY2

RS

Normal in y at Z2

9

EXY2

RS

Shear in xy at Z2

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

SA1

RS

Theta ( Shear Angle ) at Z1

7

SMJRP1

RS

Major Principal at Z1

8

SMNRP1

RS

Minor Principal at Z1

9

SMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

SX2

RS

Normal in x at Z2

12

SY2

RS

Normal in y at Z2

13

TXY2

RS

Shear in xy at Z2

5-150

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

14

SA2

RS

Theta (Shear Angle) at Z2

15

SMJRP2

RS

Major Principal at Z2

16

SMNRP2

RS

Minor Principal at Z2

17

TMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

Real / Imaginary

2

FD1

RS

Z1 = Fibre Distance

3

SX1R

RS

Normal in x at Z1

4

SX1I

RS

Normal in x at Z1

5

SY1R

RS

Normal in y at Z1

6

SY1I

RS

Normal in y at Z1

7

TXY1R

RS

Shear in xy at Z1

8

TXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

SX2R

RS

Normal in x at Z2

11

SX2I

RS

Normal in x at Z2

12

SY2R

RS

Normal in y at Z2

13

SY2I

RS

Normal in y at Z2

14

TXY2R

RS

Shear in xy at Z2

15

TXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

SX2

RS

Normal in x at Z2

DMAP Programmer’s Guide

5-151

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

SY2

RS

Normal in y at Z2

9

TXY2

RS

Shear in xy at Z2

End TCODE,7 End SCODE,6 ELTYPE =75

Curved triangular shell element (CTRIA6)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

EMJRP1

RS

Major Principal at Z1

10

EMNRP1

RS

Minor Principal at Z1

11

ETMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

EX2

RS

Normal in x at Z2

14

EY2

RS

Normal in y at Z2

15

ETXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

EMJRP2

RS

Major Principal at Z2

18

EMNRP2

RS

Minor Principal at Z2

19

ETMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 004 times

5-152

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word TCODE,7 =1

Type

Description

Real / Imaginary

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1R

RS

Normal in x at Z1

6

EX1I

RS

Normal in x at Z1

7

EY1R

RS

Normal in y at Z1

8

EY1I

RS

Normal in y at Z1

9

ETXY1R

RS

Shear in xy at Z1

10

ETXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

EX2R

RS

Normal in x at Z2

13

EX2I

RS

Normal in x at Z2

14

EY2R

RS

Normal in y at Z2

15

EY2I

RS

Normal in y at Z2

16

ETXY2R

RS

Shear in xy at Z2

17

ETXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 004 times TCODE,7 =2

Random Response

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

DMAP Programmer’s Guide

5-153

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

FD2

RS

Fiber distance at Z2

9

EX2

RS

Normal in x at Z2

10

EY2

RS

Normal in y at Z2

11

ETXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 004 times End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

7

TXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

SMJRP1

RS

Major Principal at Z1

10

SMNRP1

RS

Minor Principal at Z1

11

TMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

SX2

RS

Normal in x at Z2

14

SY2

RS

Normal in y at Z2

15

TXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

SMJRP2

RS

Major Principal at Z2

18

SMNRP2

RS

Minor Principal at Z2

19

TMAX2

RS

Maximum Shear at Z2

5-154

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

Words 3 through 19 repeat 004 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1R

RS

Normal in x at Z1

6

SX1I

RS

Normal in x at Z1

7

SY1R

RS

Normal in y at Z1

8

SY1I

RS

Normal in y at Z1

9

TXY1R

RS

Shear in xy at Z1

10

TXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

SX2R

RS

Normal in x at Z2

13

SX2I

RS

Normal in x at Z2

14

SY2R

RS

Normal in y at Z2

15

SY2I

RS

Normal in y at Z2

16

TXY2R

RS

Shear in xy at Z2

17

TXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 004 times TCODE,7 =2

Random Response

2

TERM

CHAR4

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

DMAP Programmer’s Guide

5-155

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

7

TXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

SX2

RS

Normal in x at Z2

10

SY2

RS

Normal in y at Z2

11

TXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 004 times End TCODE,7 End SCODE,6 ELTYPE =76 2

Acoustic velocity/pressures in six-sided solid element (CHEXA) UNDEF

ELTYPE =77 2

Acoustic velocity/pressures in five-sided solid element (CPENTA) UNDEF

ELTYPE =78 2 ELTYPE =79

Name

ELTYPE =80 2

None Type

Description

Undef UNDEF

ELTYPE =81 2

None Undef

UNDEF Word

None Acoustic velocity/pressures in four-sided solid element (CTETRA)

UNDEF

2

None

None Undef

UNDEF

None

ELTYPE =82

Quadrilateral plate element (CQUADR)

SCODE,6 =0

Strain

TCODE,7 =0

Real

5-156

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

7

ETXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

EMJRP1

RS

Major Principal at Z1

10

EMNRP1

RS

Minor Principal at Z1

11

ETMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

EX2

RS

Normal in x at Z2

14

EY2

RS

Normal in y at Z2

15

ETXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

EMJRP2

RS

Major Principal at Z2

18

EMNRP2

RS

Minor Principal at Z2

19

ETMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 005 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1R

RS

Normal in x at Z1

6

EX1I

RS

Normal in x at Z1

DMAP Programmer’s Guide

5-157

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

7

EY1R

RS

Normal in y at Z1

8

EY1I

RS

Normal in y at Z1

9

ETXY1R

RS

Shear in xy at Z1

10

ETXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

EX2R

RS

Normal in x at Z2

13

EX2I

RS

Normal in x at Z2

14

EY2R

RS

Normal in y at Z2

15

EY2I

RS

Normal in y at Z2

16

ETXY2R

RS

Shear in xy at Z2

17

ETXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 005 times TCODE,7 =2

Random Response

2

TERM

CHAR4

"CENTER"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

EX1

RS

Normal in x at Z1

6

EY1

RS

Normal in y at Z1

7

ETXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

EX2

RS

Normal in x at Z2

10

EY2

RS

Normal in y at Z2

11

ETXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 005 times End TCODE,7 SCODE,6 =01

5-158

DMAP Programmer’s Guide

Stress

Data Block Descriptions O-V

Name

Word TCODE,7 =0

Type

Description

Real

2

TERM

CHAR4

"CEN"

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

7

TXY1

RS

Shear in xy at Z1

8

A1

RS

Theta (Shear Angle) at Z1

9

MJRP1

RS

Major Principal at Z1

10

MNRP1

RS

Minor Principal at Z1

11

TMAX1

RS

Maximum Shear at Z1

12

FD2

RS

Fiber distance at Z2

13

SX2

RS

Normal in x at Z2

14

SY2

RS

Normal in y at Z2

15

TXY2

RS

Shear in xy at Z2

16

A2

RS

Theta (Shear Angle) at Z2

17

MJRP2

RS

Major Principal at Z2

18

MNRP2

RS

Minor Principal at Z2

19

TMAX2

RS

Maximum Shear at Z2

Words 3 through 19 repeat 005 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1R

RS

Normal in x at Z1

DMAP Programmer’s Guide

5-159

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

6

SX1I

RS

Normal in x at Z1

7

SY1R

RS

Normal in y at Z1

8

SY1I

RS

Normal in y at Z1

9

TXY1R

RS

Shear in xy at Z1

10

TXY1I

RS

Shear in xy at Z1

11

FD2

RS

Fiber distance at Z2

12

SX2R

RS

Normal in x at Z2

13

SX2I

RS

Normal in x at Z2

14

SY2R

RS

Normal in y at Z2

15

SY2I

RS

Normal in y at Z2

16

TXY2R

RS

Shear in xy at Z2

17

TXY2I

RS

Shear in xy at Z2

Words 3 through 17 repeat 005 times TCODE,7 =2

Random Response

2

TERM

CHAR4

3

GRID

I

Number active grids identification number or grid identification number

4

FD1

RS

Fiber distance at Z1

5

SX1

RS

Normal in x at Z1

6

SY1

RS

Normal in y at Z1

7

TXY1

RS

Shear in xy at Z1

8

FD2

RS

Fiber distance at Z2

9

SX2

RS

Normal in x at Z2

10

SY2

RS

Normal in y at Z2

11

TXY2

RS

Shear in xy at Z2

Words 3 through 11 repeat 005 times End TCODE,7

5-160

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

End SCODE,6 ELTYPE =83 2

Acoustic absorber element (CHACAB) UNDEF

ELTYPE =84 2

None Acoustic barrier element (CHACBR)

UNDEF

ELTYPE =85

None TETRA - Nonlinear

2

CTYPE

CHAR4

3

GRID

I

Grid / Gauss

4

SX

RS

Stress in x

5

SY

RS

Stress in y

6

SZ

RS

Stress in z

7

SXY

RS

Stress in xy

8

SYZ

RS

Stress in yz

9

SZX

RS

Stress in zx

10

SE

RS

Equivalent stress

11

EPS

RS

Effective plastic strain

12

ECS

RS

Effective creep strain

13

EX

RS

Strain in x

14

EY

RS

Strain in y

15

EZ

RS

Strain in z

16

EXY

RS

Strain in xy

17

EYZ

RS

Strain in yz

18

EZX

RS

Strain in zx

Words 3 through 18 repeat 005 times ELTYPE =86 2

GAP - Nonlinear CPX

RS

Comp x

DMAP Programmer’s Guide

5-161

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

3

SHY

RS

Shear in y

4

SHZ

RS

Shear in z

5

AU

RS

Axial in u

6

SHV

RS

Shear in v

7

SHW

RS

Shear in w

8

SLV

RS

Slip in v

9

SLP

RS

Slip in w

10

FORM1

CHAR4

No definition

11

FORM2

CHAR4

No definition

ELTYPE =87

Nonlinear tube element (CTUBE)

2

AS

RS

Axial Stress

3

SE

RS

Equivalent Stress

4

TE

RS

Total Strain

5

EPS

RS

Effective Plastic strain

6

ECS

RS

Effective Creep strain

7

LTS

RS

Linear torsional stress

ELTYPE =88

TRIA3 - Nonlinear (Same as QUAD4)

NUMWDE =13 2

FD1

RS

Z1 = Fiber distance

3

SX1

RS

Stress in x at Z1

4

SY1

RS

Stress in y at Z1

5

SZ1

RS

Stress in z at Z1

6

TXY1

RS

Shear stress in xy at Z1

7

ES

RS

Equivalent stress at Z1

8

EPS1

RS

Effective plastic/inelastic strain at Z1

9

ECS1

RS

Effective creep strain at Z1

5-162

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

10

EX1

RS

Strain in x at Z1

11

EY1

RS

Strain in y at Z1

12

EZ1

RS

Strain in z at Z1

13

ETXY1

RS

Shear strain in xy at Z1

NUMWDE =25 2

FD1

RS

Z1 = Fiber distance

3

SX1

RS

Stress in x at Z1

4

SY1

RS

Stress in y at Z1

5

UNDEF

None

Stress in z at Z1

6

TXY1

RS

Shear stress in xy at Z1

7

ES

RS

Equivalent stress at Z1

8

EPS1

RS

Effective plastic/inelastic strain at Z1

9

ECS1

RS

Effective creep strain at Z1

10

EX1

RS

Strain in x at Z1

11

EY1

RS

Strain in y at Z1

12

UNDEF

None

Strain in z at Z1

13

ETXY1

RS

Shear strain in xy at Z1

14

FD2

RS

Z2 = Fiber distance

15

SX2

RS

Stress in x at Z2

16

SY2

RS

Stress in y at Z2

17

UNDEF

None

Stress in z at Z2

18

TXY2

RS

Shear stress in xy at Z2

19

ES

RS

Equivalent stress at Z2

20

EPS2

RS

Effective plastic/inelastic strain at Z2

21

ECS2

RS

Effective creep strain at Z2

22

EX2

RS

Strain in x at Z2

DMAP Programmer’s Guide

5-163

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

23

EY2

RS

Strain in y at Z2

24

UNDEF

None

Strain in z at Z2

25

ETXY2

RS

Shear strain in xy at Z2

End NUMWDE ELTYPE =89

Nonlinear rod element (CROD)

2

AS

RS

Axial Stress

3

SE

RS

Equivalent Stress

4

TE

RS

Total Strain

5

EPS

RS

Effective Plastic strain

6

ECS

RS

Effective Creep strain

7

LTS

RS

Linear torsional stress

Name

Word ELTYPE =90

Type

Description

QUAD4 - Nonlinear

NUMWDE =13 2

FD1

RS

Z1 = Fiber distance

3

SX1

RS

Stress in x at Z1

4

SY1

RS

Stress in y at Z1

5

SZ1

RS

Stress in z at Z1

6

TXY1

RS

Shear stress in xy at Z1

7

ES

RS

Equivalent stress at Z1

8

EPS1

RS

Effective plastic/inelastic strain at Z1

9

ECS1

RS

Effective creep strain at Z1

10

EX1

RS

Strain in x at Z1

11

EY1

RS

Strain in y at Z1

12

EZ1

RS

Strain in z at Z1

13

ETXY1

RS

Shear strain in xy at Z1

5-164

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

NUMWDE =25 2

FD1

RS

Z1 = Fiber distance

3

SX1

RS

Stress in x at Z1

4

SY1

RS

Stress in y at Z1

5

UNDEF

None

Stress in z at Z1

6

TXY1

RS

Shear stress in xy at Z1

7

ES

RS

Equivalent stress at Z1

8

EPS1

RS

Effective plastic/inelastic strain at Z1

9

ECS1

RS

Effective creep strain at Z1

10

EX1

RS

Strain in x at Z1

11

EY1

RS

Strain in y at Z1

12

UNDEF

None

Strain in z at Z1

13

ETXY1

RS

Shear strain in xy at Z1

14

FD2

RS

Z2 = Fiber distance

15

SX2

RS

Stress in x at Z2

16

SY2

RS

Stress in y at Z2

17

UNDEF

None

Stress in z at Z2

18

TXY2

RS

Shear stress in xy at Z2

19

ES

RS

Equivalent stress at Z2

20

EPS2

RS

Effective plastic/inelastic strain at Z2

21

ECS2

RS

Effective creep strain at Z2

22

EX2

RS

Strain in x at Z2

23

EY2

RS

Strain in y at Z2

24

UNDEF

None

Strain in z at Z2

25

ETXY2

RS

Shear strain in xy at Z2

End NUMWDE

DMAP Programmer’s Guide

5-165

Chapter 5

Data Block Descriptions O-V

Name

Word ELTYPE =91

Type

Description

Nonlinear five-sided solid element (CPENTA)

2

CTYPE

CHAR4

Grid or Gauss

3

GRID

I

Extermal Grid identification number; 0 = Center

4

SX

RS

Stress in x

5

SY

RS

Stress in y

6

SZ

RS

Stress in z

7

SXY

RS

Stress in xy

8

SYZ

RS

Stress in yz

9

SZX

RS

Stress in zx

10

SE

RS

Equivalent stress

11

EPS

RS

Equivalent plastic strain

12

ECS

RS

Effective creep strain

13

EX

RS

Strain in x

14

EY

RS

Strain in y

15

EZ

RS

Strain in z

16

EXY

RS

Strain in xy

17

EYZ

RS

Strain in yz

18

EZX

RS

Strain in zx

Words 3 through 18 repeat 007 times ELTYPE =92

Nonlinear rod element connection and property (CONROD)

2

AS

RS

Axial Stress

3

SE

RS

Equivalent Stress

4

TE

RS

Total Strain

5

EPS

RS

Effective Plastic strain

6

ECS

RS

Effective Creep strain

7

LTS

RS

Linear torsional stress

5-166

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word ELTYPE =93

Type

Description

Nonlinear six-sided solid element (CHEXA)

2

CTYPE

CHAR4

Grid or Gauss

3

GRID

I

Extermal Grid identification number; 0 = Center

4

SX

RS

Stress in x

5

SY

RS

Stress in y

6

SZ

RS

Stress in z

7

SXY

RS

Stress in xy

8

SYZ

RS

Stress in yz

9

SZX

RS

Stress in zx

10

SE

RS

Equivalent stress

11

EPS

RS

Equivalent plastic strain

12

ECS

RS

Effective creep strain

13

EX

RS

Strain in x

14

EY

RS

Strain in y

15

EZ

RS

Strain in z

16

EXY

RS

Strain in xy

17

EYZ

RS

Strain in yz

18

EZX

RS

Strain in zx

Words 3 through 18 repeat 009 times ELTYPE =94

Nonlinear beam element (CBEAM)

2

GRIDA

I

External Grid point Id at A

3

LOCCA

CHAR4

’C’ (BCD Value) at A

4

NSXCA

RS

Long. Stress at point C at A

5

NSECA

RS

Equivalent Stress at A

6

TECA

RS

Total Strain at A

7

EPECA

RS

Effective Plastic strain at A

DMAP Programmer’s Guide

5-167

Chapter 5

Word

Data Block Descriptions O-V

Name

Type

Description

8

ECECA

RS

Effective Creep strain at A

9

LOCDA

CHAR4

’D’ (BCD Value) at A

10

NSXDA

RS

Long. Stress at point D at A

11

NSEDA

RS

Equivalent Stress at A

12

TEDA

RS

Total Strain at A

13

EPEDA

RS

Effective Plastic strain at A

14

ECEDA

RS

Effective Creep strain at A

15

LOCEA

CHAR4

’E’ (BCD Value) at A

16

NSXEA

RS

Long. Stress at point E at A

17

NSEEA

RS

Equivalent Stress at A

18

TEEA

RS

Total Strain at A

19

EPEEA

RS

Effective Plastic strain at A

20

ECEEA

RS

Effective Creep strain at A

21

LOCFA

CHAR4

’F’ (BCD Value) at A

22

NSXFA

RS

Long. Stress at point F at A

23

NSEFA

RS

Equivalent Stress at A

24

TEFA

RS

Total Strain at A

25

EPEFA

RS

Effective Plastic strain at A

26

ECEFA

RS

Effective Creep strain at A

27

GRIDB

I

External Grid point identification number at B

28

LOCCB

CHAR4

’C’ (BCD Value) at B

29

NSXCB

RS

Long. Stress at point C at B

30

NSECB

RS

Equivalent Stress at B

31

TECB

RS

Total Strain at B

32

EPECB

RS

Effective Plastic strain at B

33

ECECB

RS

Effective Creep strain at B

5-168

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

34

LOCDB

CHAR4

’D’ (BCD Value) at B

35

NSXDB

RS

Long. Stress at point D at B

36

NSEDB

RS

Equivalent Stress at B

37

TEDB

RS

Total Strain at B

38

EPEDB

RS

Effective Plastic strain at B

39

ECEDB

RS

Effective Creep strain at B

40

LOCEB

CHAR4

’E’ (BCD Value) at B

41

NSXEB

RS

Long. Stress at point E at B

42

NSEEB

RS

Equivalent Stress at B

43

TEEB

RS

Total Strain at B

44

EPEEB

RS

Effective Plastic strain at B

45

ECEEB

RS

Effective Creep strain at B

46

LOCFB

CHAR4

’F’ (BCD Value) at B

47

NSXFB

RS

Long. Stress at point F at B

48

NSEFB

RS

Equivalent Stress at B

49

TEFB

RS

Total Strain at B

50

EPEFB

RS

Effective Plastic strain at B

51

ECEFB

RS

Effective Creep strain at B

ELTYPE =95

QUAD4 composite

SCODE,6 =0

Strain

2

PLY

I

Lamina Number

3

EX1

RS

Normal-1

4

EY1

RS

Normal-2

5

ET1

RS

Shear-12

6

EL1

RS

Shear-1Z

7

EL2

RS

Shear-2Z

DMAP Programmer’s Guide

5-169

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

8

A1

RS

Shear angle

9

EMJRP1

RS

Major Principal

10

EMNRP1

RS

Minor Principal

11

ETMAX1

RS

von Mises or Maximum shear

SCODE,6 =01

Stress

2

PLY

I

Lamina Number

3

SX1

RS

Normal-1

4

SY1

RS

Normal-2

5

T1

RS

Shear-12

6

SL1

RS

Shear-1Z

7

SL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

MJRP1

RS

Major Principal

10

MNRP1

RS

Minor Principal

11

TMAX1

RS

von Mises or Maximum shear

End SCODE,6 ELTYPE =96

QUAD8 composite (Same as QUAD4 composite)

SCODE,6 =0

Strain

2

PLY

I

Lamina Number

3

EX1

RS

Normal-1

4

EY1

RS

Normal-2

5

ET1

RS

Shear-12

6

EL1

RS

Shear-1Z

7

EL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

EMJRP1

RS

Major Principal

5-170

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

10

EMNRP1

RS

Minor Principal

11

ETMAX1

RS

von Mises or Maximum shear

SCODE,6 =01

Stress

2

PLY

I

Lamina Number

3

SX1

RS

Normal-1

4

SY1

RS

Normal-2

5

T1

RS

Shear-12

6

SL1

RS

Shear-1Z

7

SL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

MJRP1

RS

Major Principal

10

MNRP1

RS

Minor Principal

11

TMAX1

RS

von Mises or Maximum shear

End SCODE,6 ELTYPE =97

TRIA3 composite (Same as QUAD4 composite)

SCODE,6 =0

Strain

2

PLY

I

Lamina Number

3

EX1

RS

Normal-1

4

EY1

RS

Normal-2

5

ET1

RS

Shear-12

6

EL1

RS

Shear-1Z

7

EL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

EMJRP1

RS

Major Principal

10

EMNRP1

RS

Minor Principal

11

ETMAX1

RS

von Mises or Maximum shear

DMAP Programmer’s Guide

5-171

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

SCODE,6 =01

Stress

2

PLY

I

Lamina Number

3

SX1

RS

Normal-1

4

SY1

RS

Normal-2

5

T1

RS

Shear-12

6

SL1

RS

Shear-1Z

7

SL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

MJRP1

RS

Major Principal

10

MNRP1

RS

Minor Principal

11

TMAX1

RS

von Mises or Maximum shear

End SCODE,6 ELTYPE =98

TRIA6 composite (Same as QUAD4 composite)

SCODE,6 =0

Strain

2

PLY

I

Lamina Number

3

EX1

RS

Normal-1

4

EY1

RS

Normal-2

5

ET1

RS

Shear-12

6

EL1

RS

Shear-1Z

7

EL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

EMJRP1

RS

Major Principal

10

EMNRP1

RS

Minor Principal

11

ETMAX1

RS

von Mises or Maximum shear

SCODE,6 =01

Stress

2

I

5-172

PLY

DMAP Programmer’s Guide

Lamina Number

Data Block Descriptions O-V

Name

Word

Type

Description

3

SX1

RS

Normal-1

4

SY1

RS

Normal-2

5

T1

RS

Shear-12

6

SL1

RS

Shear-1Z

7

SL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

MJRP1

RS

Major Principal

10

MNRP1

RS

Minor Principal

11

TMAX1

RS

von Mises or Maximum shear

End SCODE,6 ELTYPE =99 2

Undef UNDEF

None

Name

Word

Type

Description

ELTYPE =100

Simple beam element w/stations (CBAR with CBARAO or PLOAD1)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

SD

RS

% along bar for output

3

EXC

RS

Strain at point c

4

EXD

RS

Strain at point d

5

EXE

RS

Strain at point e

6

EXF

RS

Strain at point f

7

AE

RS

Axial strain

8

EMAX

RS

Maximum strain

9

EMIN

RS

Minimum strain

10

MS

RS

Margin of Safety

DMAP Programmer’s Guide

5-173

Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7 =1

Type

Description

Real / Imaginary

2

SD

RS

% along bar for output

3

EXCR

RS

Strain at point c

4

EXDR

RS

Strain at point d

5

EXER

RS

Strain at point e

6

EXFR

RS

Strain at point f

7

AER

RS

Axial strain

8

EMAXR

RS

Maximum strain

9

EMINR

RS

Minimum strain

10

EXCI

RS

Strain at point c

11

EXDI

RS

Strain at point d

12

EXEI

RS

Strain at point e

13

EXFI

RS

Strain at point f

14

AEI

RS

Axial strain

15

EMAXI

RS

Maximum strain

16

EMINI

RS

Minimum strain

TCODE,7 =2

Random Response

2

SD

RS

% along bar for output

3

EXC

RS

Strain at point c

4

EXD

RS

Strain at point d

5

EXE

RS

Strain at point e

6

EXF

RS

Strain at point f

7

AE

RS

Axial strain

8

EMAX

RS

Maximum strain

9

EMIN

RS

Minimum strain

End TCODE,7

5-174

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

SCODE,6 =01

Stress

TCODE,7 =0

Real

Description

2

SD

RS

% along bar for output

3

SXC

RS

Stress at point c

4

SXD

RS

Stress at point d

5

SXE

RS

Stress at point e

6

SXF

RS

Stress at point f

7

AS

RS

Axial stress

8

SMAX

RS

Maximum stress

9

SMIN

RS

Minimum stress

10

MS

RS

Margin of Safety

TCODE,7 =1

Real / Imaginary

2

SD

RS

% along bar for output

3

SXCR

RS

Stress at point c

4

SXDR

RS

Stress at point d

5

SXER

RS

Stress at point e

6

SXFR

RS

Stress at point f

7

ASR

RS

Axial stress

8

SMAXR

RS

Maximum stress

9

SMINR

RS

Minimum stress

10

SXCI

RS

Stress at point c

11

SXDI

RS

Stress at point d

12

SXEI

RS

Stress at point e

13

SXFI

RS

Stress at point f

14

ASI

RS

Axial stress

15

SMAXI

RS

Maximum stress

DMAP Programmer’s Guide

5-175

Data Block Descriptions O-V

Chapter 5

Name

Word 16

SMINI

TCODE,7 =2

Type RS

Description Minimum stress

Random Response

2

SD

RS

% along bar for output

3

SXC

RS

Stress at point c

4

SXD

RS

Stress at point d

5

SXE

RS

Stress at point e

6

SXF

RS

Stress at point f

7

AS

RS

Axial stress

8

SMAX

RS

Maximum stress

9

SMIN

RS

Minimum stress

End TCODE,7 End SCODE,6 ELTYPE =101

Acoustic absorber element with freq. dependence (CAABSF)

TCODE,7 =0 or 2

Real or Random Response

2

IMPED

RS

Impedance

3

ABSORB

RS

Absorption Coefficient

TCODE,7 =1

Real / Imaginary

2

IMPEDR

RS

Impedance

3

IMPEDI

RS

Impedance

4

ABSORB

RS

Absorption Coefficient

End TCODE,7 ELTYPE =102

Generalized spring and damper element (CBUSH)

TCODE,7 =0 or 2

Real or Random Response

2

TX

RS

Translation x

3

TY

RS

Translation y

4

TZ

RS

Translation z

5-176

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

5

RX

RS

Rotation x

6

RY

RS

Rotation y

7

RZ

RS

Rotation z

TCODE,7 =1

Real / Imaginary

2

TXR

RS

Translation x R

3

TYR

RS

Translation y R

4

TZR

RS

Translation z R

5

RXR

RS

Rotation x R

6

RYR

RS

Rotation y R

7

RZR

RS

Rotation z R

8

TXI

RS

Translation x I

9

TYI

RS

Translation y I

10

TZI

RS

Translation z I

11

RXI

RS

Rotation x I

12

RYI

RS

Rotation y I

13

RZI

RS

Rotation z I

End TCODE,7 ELTYPE =103

Quadrilateral shell element (QUADP)

2

None

UNDEF

ELTYPE =104

Triangular shell p-element (TRIAP)

2

None

UNDEF

ELTYPE =105

Beam p-element (BEAMP)

2

None

UNDEF

ELTYPE =106

Scalar damper with material property (CDAMP5)

2

None

UNDEF

ELTYPE =107

Heat transfer boundary condition element - (CHBDYE)

DMAP Programmer’s Guide

5-177

Data Block Descriptions O-V

Chapter 5

Name

Word 2

UNDEF

Type

Description

None

ELTYPE =108

Heat transfer boundary condition element (CHBDYG)

2

None

UNDEF

ELTYPE =109

Heat transfer boundary condition element (CHBDYP)

2

None

UNDEF Name

Word

Type

ELTYPE =110

CONV

2

None

UNDEF

ELTYPE =111

CONVM

2

None

UNDEF

ELTYPE =115

RADBC

2

None

UNDEF

ELTYPE =112

QBDY3

2

None

UNDEF

ELTYPE =113

QVECT

2

None

UNDEF

ELTYPE =114

QVOL

2

None

UNDEF

ELTYPE =115

Radbc

2

None

UNDEF

ELTYPE =116

Slideline contact (SLIF1D)

2

None

UNDEF Word

Name

Type

ELTYPE =127

CQUAD

ELTYPE =128

CQUADX

ELTYPE =129

RELUC

5-178

DMAP Programmer’s Guide

Description

Description

Data Block Descriptions O-V

Name

Word

Type

Description

ELTYPE =130

RES

ELTYPE =131

TETRAE

ELTYPE =132

CTRIA

ELTYPE =133

CTRIAX

ELTYPE =134

LINEOB

ELTYPE =135

LINXOB

ELTYPE =136

QUADOB

ELTYPE =137

TRIAOB

ELTYPE =138

LINEX

ELTYPE =139

Hyperelastic QUAD4FD

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Words 3 through 9 repeat 004 times Name

Word

Type

Description

ELTYPE =140

Hyperelastic 8-noded hexahedron element linear format (HEXAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SXY

RS

Gaus

DMAP Programmer’s Guide

5-179

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

6

PA

RS

7

AX

RS

8

AY

RS

9

AZ

RS

10

PRESSURE

RS

11

SY

RS

12

SYZ

RS

13

PB

RS

14

BX

RS

15

BY

RS

16

BZ

RS

17

SZ

RS

18

SZX

RS

19

PC

RS

20

CX

RS

21

CY

RS

22

CZ

RS

Description

Words 3 through 22 repeat 008 times ELTYPE =141

Six-sided solid p-element (HEXAP)

2

None

UNDEF

ELTYPE =142

Five-sided solid p-element (PENTAP)

2

None

UNDEF

ELTYPE =143

Four-sided solid p-element (TETRAP)

2

None

UNDEF

ELTYPE =144

Quadrilateral plate element for corner stresses (QUAD144)

SCODE,6 =0

Strain

5-180

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word TCODE,7 =0

Type

Description

Real

2

TERM

CHAR4

3

GRID

I

4

FD1

RS

Fiber distance at z1

5

EX1

RS

Normal in x at z1

6

EY1

RS

Normal in y at z1

7

ETXY1

RS

Shear in xy at z1

8

A1

RS

Shear angle at z1

9

EMJRP1

RS

Major Principal at z1

10

EMNRP1

RS

Minor Principal at z1

11

ETMAX1

RS

von Mises or max shear at z1

12

FD2

RS

Fiber distance at z2

13

EX2

RS

Normal in x at z2

14

EY2

RS

Normal in y at z2

15

ETXY2

RS

Shear in xy at z2

16

A2

RS

Shear angle at z2

17

EMJRP2

RS

Major Principal at z2

18

EMNRP2

RS

Minor Principal at z2

19

ETMRP2

RS

von Mises or max shear at z2

Words 3 through 19 repeat 005 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

3

GRID

I

4

FD1

RS

Fiber distance at z1

5

EX1R

RS

Normal in x at z1

6

EX1I

RS

Normal in x at z1

DMAP Programmer’s Guide

5-181

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

7

EY1R

RS

Normal in y at z1

8

EY1I

RS

Normal in y at z1

9

ETXY1R

RS

Shear in xy at z1

10

ETXY1I

RS

Shear in xy at z1

11

FD2

RS

Fiber distance at z2

12

EX2R

RS

Normal in x at z2

13

EX2I

RS

Normal in x at z2

14

EY2R

RS

Normal in y at z2

15

EY2I

RS

Normal in y at z2

16

ETXY2R

RS

Shear in xy at z1

17

ETXY2I

RS

Shear in xy at z1

Words 3 through 17 repeat 005 times TCODE,7 =2

Random Response

2

TERM

CHAR4

3

GRID

I

4

FD1

RS

Fiber distance at z1

5

EX1

RS

Normal in x at z1

6

EY1

RS

Normal in y at z1

7

ETXY1

RS

Shear in xy at z1

8

FD2

RS

Fiber distance at z2

9

EX2

RS

Normal in x at z2

10

EY2

RS

Normal in y at z2

11

ETXY2

RS

Shear in xy at z1

Words 3 through 11 repeat 005 times End TCODE,7 SCODE,6 =01

5-182

DMAP Programmer’s Guide

Stress

Data Block Descriptions O-V

Name

Word TCODE,7 =0

Type

Description

Real

2

TERM

CHAR4

3

GRID

I

4

FD1

RS

Fiber distance at z1

5

SX1

RS

Normal in x at z1

6

SY1

RS

Normal in y at z1

7

TXY1

RS

Shear in xy at z1

8

A1

RS

Shear angle at z1

9

MJRP1

RS

Major Principal at z1

10

MNRP1

RS

Minor Principal at z1

11

TMAX1

RS

von Mises or max shear at z1

12

FD2

RS

Fiber distance at z2

13

SX2

RS

Normal in x at z2

14

SY2

RS

Normal in y at z2

15

TXY2

RS

Shear in xy at z2

16

A2

RS

Shear angle at z2

17

MJRP2

RS

Major Principal at z2

18

MNRP2

RS

Minor Principal at z2

19

TMAX2

RS

von Mises or max shear at z2

Words 3 through 19 repeat 005 times TCODE,7 =1

Real / Imaginary

2

TERM

CHAR4

3

GRID

I

4

FD1

RS

Fiber distance at z1

5

SX1R

RS

Normal in x at z1

6

SX1I

RS

Normal in x at z1

DMAP Programmer’s Guide

5-183

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

7

SY1R

RS

Normal in y at z1

8

SY1I

RS

Normal in y at z1

9

TXY1R

RS

Shear in xy at z1

10

TXY1I

RS

Shear in xy at z1

11

FD2

RS

Fiber distance at z2

12

SX2R

RS

Normal in x at z2

13

SX2I

RS

Normal in x at z2

14

SY2R

RS

Normal in y at z2

15

SY2I

RS

Normal in y at z2

16

TXY2R

RS

Shear in xy at z2

17

TXY2I

RS

Shear in xy at z2

Words 3 through 17 repeat 005 times TCODE,7 =2

Random Response

2

TERM

CHAR4

3

GRID

I

4

FD1

RS

Fiber distance at z1

5

SX1

RS

Normal in x at z1

6

SY1

RS

Normal in y at z1

7

TXY1

RS

Shear in xy at z1

8

FD2

RS

Fiber distance at z2

9

SX2

RS

Normal in x at z2

10

SY2

RS

Normal in y at z2

11

TXY2

RS

Shear in xy at z2

Words 3 through 11 repeat 005 times End TCODE,7 End SCODE,6

5-184

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

ELTYPE =145

Six-sided solid display element (VUHEXA)

2

I

PARENTID

NUMWDE =98

Len=2+ 12 * No. of points

3

GRIDID

I

4

XNORM

RS

5

YNORM

RS

6

ZNORM

RS

7

TXY

RS

8

TYZ

RS

9

TZX

RS

10

PRIN01

RS

11

PRIN02

RS

12

PRIN03

RS

13

MEAN

RS

14

VONOROCT

RS

Words 3 through 14 repeat 008 times NUMWDE =58

Len= 2 + 7 * No. of points

3

GRIDID

I

4

XNORM

RS

5

YNORM

RS

6

ZNORM

RS

7

TXY

RS

8

TYZ

RS

9

TZX

RS

Words 3 through 9 repeat 008 times NUMWDE =106

Len= 2 + 13 * No. of points

DMAP Programmer’s Guide

5-185

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

3

GRIDID

I

4

XNORMR

RS

5

YNORMR

RS

6

ZNORMR

RS

7

TXYR

RS

8

TYZR

RS

9

TZXR

RS

10

XNORMI

RS

11

YNORMI

RS

12

ZNORMI

RS

13

TXYI

RS

14

TYZI

RS

15

TZXI

RS

Description

Words 3 through 15 repeat 008 times End NUMWDE ELTYPE =146

Five-sided solid display element (VUPENTA)

2

I

PARENTID

NUMWDE =74 3

GRIDID

I

4

XNORM

RS

5

YNORM

RS

6

ZNORM

RS

7

TXY

RS

8

TYZ

RS

9

TZX

RS

10

PRIN01

RS

5-186

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

11

PRIN02

RS

12

PRIN03

RS

13

MEAN

RS

14

VONOROCT

RS

Description

Words 3 through 14 repeat 006 times NUMWDE =44 3

GRIDID

I

4

XNORM

RS

5

YNORM

RS

6

ZNORM

RS

7

TXY

RS

8

TYZ

RS

9

TZX

RS

Words 3 through 9 repeat 006 times NUMWDE =80

2 + 6*13

3

GRIDID

I

4

XNORMR

RS

5

YNORMR

RS

6

ZNORMR

RS

7

TXYR

RS

8

TYZR

RS

9

TZXR

RS

10

XNORMI

RS

11

YNORMI

RS

12

ZNORMI

RS

13

TXYI

RS

DMAP Programmer’s Guide

5-187

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

14

TYZI

RS

15

TZXI

RS

Description

Words 3 through 15 repeat 006 times End NUMWDE ELTYPE =147

Four-sided solid display element (VUTETRA)

2

I

PARENTID

NUMWDE =50 3

GRIDID

I

4

XNORM

RS

5

YNORM

RS

6

ZNORM

RS

7

TXY

RS

8

TYZ

RS

9

TZX

RS

10

PRIN01

RS

11

PRIN02

RS

12

PRIN03

RS

13

MEAN

RS

14

VONOROCT

RS

Words 3 through 14 repeat 004 times NUMWDE =30 3

GRIDID

I

4

XNORM

RS

5

YNORM

RS

6

ZNORM

RS

7

TXY

RS

5-188

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

8

TYZ

RS

9

TZX

RS

Description

Words 3 through 9 repeat 004 times NUMWDE =54

2 + 4*13

3

GRIDID

I

4

XNORMR

RS

5

YNORMR

RS

6

ZNORMR

RS

7

TXYR

RS

8

TYZR

RS

9

TZXR

RS

10

XNORMI

RS

11

YNORMI

RS

12

ZNORMI

RS

13

TXYI

RS

14

TYZI

RS

15

TZXI

RS

Words 3 through 15 repeat 004 times End NUMWDE ELTYPE =148

HEXAM

2

None

UNDEF

ELTYPE =149

PENTAM

2

None

UNDEF Name

Word

Type

ELTYPE =150

TETRAM

2

None

UNDEF

Description

DMAP Programmer’s Guide

5-189

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

ELTYPE =151

QUADM

2

None

UNDEF

ELTYPE =152

TRIAM

2

None

UNDEF

ELTYPE =153

QUADXM

2

None

UNDEF

ELTYPE =154

TRIAXM

2

None

UNDEF

ELTYPE =155

QUADPW

2

None

UNDEF

ELTYPE =156

TRIAPW

2

None

UNDEF

ELTYPE =157

LINEPW

2

None

UNDEF

ELTYPE =158

QUADOBM

2

None

UNDEF

ELTYPE =159

TRIAOBM

2

None

UNDEF Name

Word

Description

Type

Description

ELTYPE =160

Hyperelastic 5-sided 6-noded solid element (PENTAFD) Linear form

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SXY

RS

6

PA

RS

5-190

DMAP Programmer’s Guide

Gaus

Data Block Descriptions O-V

Name

Word

Type

7

AX

RS

8

AY

RS

9

AZ

RS

10

PRESSURE

RS

11

SY

RS

12

SYZ

RS

13

PB

RS

14

BX

RS

15

BY

RS

16

BZ

RS

17

SZ

RS

18

SZX

RS

19

PC

RS

20

CX

RS

21

CY

RS

22

CZ

RS

Description

Words 3 through 22 repeat 006 times ELTYPE =161

Linear form for hyperelastic 4 node TETRA

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SXY

RS

6

PA

RS

7

AX

RS

8

AY

RS

9

AZ

RS

Gaus

DMAP Programmer’s Guide

5-191

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

10

PRESSURE

RS

11

SY

RS

12

SYZ

RS

13

PB

RS

14

BX

RS

15

BY

RS

16

BZ

RS

17

SZ

RS

18

SZX

RS

19

PC

RS

20

CX

RS

21

CY

RS

22

CZ

RS

Description

Words 3 through 22 repeat 001 times ELTYPE =162

Linear form for hyperelastic 3 node TRIA (strain)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Words 3 through 9 repeat 001 times ELTYPE =163

Linear form for hyperelastic 20 node HEXAFD

2

TYPE

CHAR4

5-192

DMAP Programmer’s Guide

Gaus

Data Block Descriptions O-V

Name

Word

Type

3

ID

I

4

SX

RS

5

SXY

RS

6

PA

RS

7

AX

RS

8

AY

RS

9

AZ

RS

10

PRESSURE

RS

11

SY

RS

12

SYZ

RS

13

PB

RS

14

BX

RS

15

BY

RS

16

BZ

RS

17

SZ

RS

18

SZX

RS

19

PC

RS

20

CX

RS

21

CY

RS

22

CZ

RS

Description

Words 3 through 22 repeat 027 times ELTYPE =164

Hyperelastic quadrilateral 9-noded element (QUADFD) Linear

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

DMAP Programmer’s Guide

5-193

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Description

Words 3 through 9 repeat 009 times ELTYPE =165

Hyperelastic 5-sided 15-noded solid element (PENTAFD) Linear

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SXY

RS

6

PA

RS

7

AX

RS

8

AY

RS

9

AZ

RS

10

PRESSURE

RS

11

SY

RS

12

SYZ

RS

13

PB

RS

14

BX

RS

15

BY

RS

16

BZ

RS

17

SZ

RS

18

SZX

RS

19

PC

RS

20

CX

RS

21

CY

RS

5-194

DMAP Programmer’s Guide

Gaus

Data Block Descriptions O-V

Name

Word 22

CZ

Type

Description

RS

Words 3 through 22 repeat 021 times ELTYPE =166

Linear form for hyperelastic 10 node TETRA

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SXY

RS

6

PA

RS

7

AX

RS

8

AY

RS

9

AZ

RS

10

PRESSURE

RS

11

SY

RS

12

SYZ

RS

13

PB

RS

14

BX

RS

15

BY

RS

16

BZ

RS

17

SZ

RS

18

SZX

RS

19

PC

RS

20

CX

RS

21

CY

RS

22

CZ

RS

Gaus

Words 3 through 22 repeat 005 times ELTYPE =167

Linear form for hyperelastic 6 node TRIA (plane strain)

DMAP Programmer’s Guide

5-195

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Description

Words 3 through 9 repeat 003 times ELTYPE =168

Linear form for hyperelastic 3 node TRIA (axisymm)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Words 3 through 9 repeat 001 times ELTYPE =169

Linear form for hyperelastic 6 node TRIA (axisymm)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

5-196

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

8

SMJ

RS

9

SMI

RS

Description

Words 3 through 9 repeat 003 times Name

Word

Type

Description

ELTYPE =170

Linear form for hyperelastic 4 node QUAD (axisymm)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Words 3 through 9 repeat 004 times ELTYPE =171

Linear form for hyperelastic 9 node QUAD (axisymm)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SXY

RS

7

ANGLE

RS

8

SMJ

RS

9

SMI

RS

Words 3 through 9 repeat 009 times Word ELTYPE =189

Name

Type

Description

Quadrilateral plate view element (VUQUAD)

DMAP Programmer’s Guide

5-197

Chapter 5

Data Block Descriptions O-V

Name

Word SCODE,6 =0

Type

Description

Strain

2

PARENT

I

Parent p-element identification number

3

COORD

I

CID coordinate system identification number

4

ICORD

CHAR4

ICORD flat/curved and so on

5

THETA

I

THETA angle

6

ITYPE

I

ITYPE strcur =0, fiber=1

TCODE,7 =0

Real

7

VUID

I

VU grid identification number for this corner

8

NONE(2)

I

Nothing

10

MSX

RS

Membrane stain x

11

MSY

RS

Membrane strain y

12

MXY

RS

Membrane strain xy

13

NONE(3)

RS

Nothing

16

BCX

RS

Bending curvature x

17

BCY

RS

Bending curvature y

18

BCXY

RS

Bending curvature xy

19

TYZ

RS

Shear yz

20

TZX

RS

Shear zx

21

UNDEF(3 )

None

Words 7 through 23 repeat 004 times TCODE,7 =1

Real / Imaginary

7

VUID

I

8

UNDEF(2 )

None

10

MSXR

RS

Membrane strain x RM

11

MSYR

RS

Membrane strain y RM

12

MXYR

RS

Membrane strain xy RM

5-198

DMAP Programmer’s Guide

VU grid identification number this corner

Data Block Descriptions O-V

Name

Word

Type

Description

13

UNDEF(3 )

None

16

BCXR

RS

Bending curvature x RM

17

BCYR

RS

Bending curvature y RM

18

BCXYR

RS

Bending curvature xy RM

19

TYZR

RS

Shear yz RM

20

TZXR

RS

Shear zx RM

21

UNDEF

None

22

MSXI

RS

Membrane strain x IP

23

MSYI

RS

Membrane strain y IP

24

MXYI

RS

Membrane strain xy IP

25

UNDEF(3 )

None

28

BCXI

RS

Bending curvature x IP

29

BCYI

RS

Bending curvature y IP

30

BCXYI

RS

Bending curvature xy IP

31

TYZI

RS

Shear yz IP

32

TZXI

RS

Shear zx IP

33

UNDEF

None

Words 7 through 33 repeat 004 times TCODE,7 =2 2

Random Response UNDEF

None

End TCODE,7 SCODE,6 =01

Stress

2

PARENT

I

Parent p-element identification number

3

COORD

I

CID coordinate system identification number

4

ICORD

CHAR4

ICORD flat/curved and so on

5

THETA

I

THETA angle

DMAP Programmer’s Guide

5-199

Data Block Descriptions O-V

Chapter 5

Name

Word 6

ITYPE

TCODE,7 =0

Type I

Description ITYPE strcur =0, fiber=1

Real

7

VUID

I

VU grid identification number for this corner

8

Z1

RS

Z1 fiber distance

9

Z2

RS

Z2 fiber distance

10

NX1

RS

Normal x at Z1

11

NY1

RS

Normal y at Z1

12

TXY1

RS

Shear xy at Z1

13

ANGLE1

RS

Shear Angle at Z1 or n/a

14

MJRP1

RS

Major principal at Z1 or n/a

15

MNRP1

RS

Minor principal at Z1 or n/a

16

MAXSV1

RS

vonMises/Max.Shear at Z1 or n/a

17

NX2

RS

Normal x at Z2

18

NY2

RS

Normal y at Z2

19

TXY2

RS

Shear xy at Z2

20

ANGLE2

RS

Shear Angle at Z2 or n/a

21

MJRP2

RS

Major principal at Z2 or n/a

22

MNRP2

RS

Minor principal at Z2 or n/a

23

MAXSV2

RS

vonMises/Max.Shear at Z2 or n/a

Words 7 through 23 repeat 004 times TCODE,7 =1

Real / Imaginary

7

VUID

I

VU grid identification number for this corner

8

Z1

RS

Z1 fiber distance

9

Z2

RS

Z2 fiber distance

10

NX1R

RS

Normal x rm at Z1

11

NX1I

RS

Normal x ip at Z1

5-200

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

12

NY1R

RS

Normal y rm at Z1

13

NY1I

RS

Normal y ip at Z1

14

TXY1R

RS

Shear xy rm at Z1

15

TXY1I

RS

Shear xy ip at Z1

16

NZ1R

RS

Normal z rm at Z1 or n/a

17

NZ1I

RS

Normal z ip at Z1 or n/a

18

TYZ1R

RS

Shear yz rm at Z1 or n/a

19

TYZ1I

RS

Shear yz ip at Z1 or n/a

20

TZX1R

RS

Shear zx rm at Z1 or n/a

21

TZX1I

RS

Shear zx ip at Z1 or n/a

22

NX2R

RS

Normal x rm at Z2

23

NX2I

RS

Normal x ip at Z2

24

NY2R

RS

Normal y rm at Z2

25

NY2I

RS

Normal y ip at Z2

26

TXY2R

RS

Shear xy rm at Z2

27

TXY2I

RS

Shear xy ip at Z2

28

NZ1R

RS

Normal z rm at Z1 or n/a

29

NZ1I

RS

Normal z ip at Z1 or n/a

30

TYZ1R

RS

Shear yz rm at Z1 or n/a

31

TYZ1I

RS

Shear yz ip at Z1 or n/a

32

TZX1R

RS

Shear zx rm at Z1 or n/a

33

TZX1I

RS

Shear zx ip at Z1 or n/a

Words 7 through 33 repeat 004 times TCODE,7 =2 2

Random Response UNDEF

None

End TCODE,7 End SCODE,6

DMAP Programmer’s Guide

5-201

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ELTYPE =190

Triangular shell view element (VUTRIA)

SCODE,6 =0

Strain

2

PARENT

I

Parent p-element identification number

3

COORD

I

CID coordinate system identification number

4

ICORD

CHAR4

ICORD flat/curved and so on

5

THETA

I

THETA angle

6

ITYPE

I

ITYPE strcur =0, fiber=1

TCODE,7 =0

Real

7

VUID

I

VU grid identification number for this corner

8

NONE(2)

I

Nothing

10

MSX

RS

Membrane stain x

11

MSY

RS

Membrane strain y

12

MXY

RS

Membrane strain xy

13

NONE(3)

RS

Nothing

16

BCX

RS

bending curvature x

17

BCY

RS

Bending curvature y

18

BCXY

RS

Bending curvature xy

19

TYZ

RS

Shear yz

20

TZX

RS

Shear zx

21

NONE(3)

RS

Nothing

Words 7 through 23 repeat 003 times TCODE,7 =1

Real / Imaginary

7

VUID

I

8

UNDEF(2 )

None

10

MSXR

RS

Membrane strain x RM

11

MSYR

RS

Membrane strain y RM

5-202

DMAP Programmer’s Guide

VU grid identification number this corner

Data Block Descriptions O-V

Name

Word

Type

Description

12

MXYR

RS

13

UNDEF(3 )

None

16

BCXR

RS

Bending curvature x RM

17

BCYR

RS

Bending curvature y RM

18

BCXYR

RS

Bending curvature xy RM

19

TYZR

RS

Shear yz RM

20

TZXR

RS

Shear zx RM

21

UNDEF

None

22

MSXI

RS

Membrane strain x IP

23

MSYI

RS

Membrane strain y IP

24

MXYI

RS

Membrane strain xy IP

25

UNDEF(3 )

None

28

BCXI

RS

Bending curvature x IP

29

BCYI

RS

Bending curvature y IP

30

BCXYI

RS

Bending curvature xy IP

31

TYZI

RS

Shear yz IP

32

TZXI

RS

Shear zx IP

33

UNDEF

None

Membrane strain xy RM

Words 7 through 33 repeat 003 times TCODE,7 =2 2

Random Response UNDEF

None

End TCODE,7 SCODE,6 =01

Stress

2

PARENT

I

Parent p-element identification number

3

COORD

I

CID coordinate system identification number

4

ICORD

CHAR4

ICORD flat/curved and so on

DMAP Programmer’s Guide

5-203

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

5

THETA

I

THETA angle

6

ITYPE

I

ITYPE strcur =0, fiber=1

TCODE,7 =0

Real

7

VUID

I

VU grid identification number for this corner

8

Z1

RS

Z1 fiber distance

9

Z2

RS

Z2 fiber distance

10

NX1

RS

Normal x at Z1

11

NY1

RS

Normal y at Z1

12

TXY1

RS

Shear xy at Z1

13

ANGLE1

RS

Shear Angle at Z1 or n/a

14

MJRP1

RS

Major principal at Z1 or n/a

15

MNRP1

RS

Minor principal at Z1 or n/a

16

MAXSV1

RS

vonMises/Max.Shear at Z1 or n/a

17

NX2

RS

Normal x at Z2

18

NY2

RS

Normal y at Z2

19

TXY2

RS

Shear xy at Z2

20

ANGLE2

RS

Shear Angle at Z2 or n/a

21

MJRP2

RS

Major principal at Z2 or n/a

22

MNRP2

RS

Minor principal at Z2 or n/a

23

MAXSV2

RS

vonMises/Max.Shear at Z2 or n/a

Words 7 through 23 repeat 003 times TCODE,7 =1

Real / Imaginary

7

VUID

I

VU grid identification number for this corner

8

Z1

RS

Z1 fiber distance

9

Z2

RS

Z2 fiber distance

10

NX1R

RS

Normal x rm at Z1

5-204

DMAP Programmer’s Guide

Data Block Descriptions O-V

Word

Name

Type

Description

11

NX1I

RS

Normal x ip at Z1

12

NY1R

RS

Normal y rm at Z1

13

NY1I

RS

Normal y ip at Z1

14

TXY1R

RS

Shear xy rm at Z1

15

TXY1I

RS

Shear xy ip at Z1

16

NZ1R

RS

Normal z rm at Z1 or n/a

17

NZ1I

RS

Normal z ip at Z1 or n/a

18

TYZ1R

RS

Shear yz rm at Z1 or n/a

19

TYZ1I

RS

Shear yz ip at Z1 or n/a

20

TZX1R

RS

Shear zx rm at Z1 or n/a

21

TZX1I

RS

Shear zx ip at Z1 or n/a

22

NX2R

RS

Normal x rm at Z2

23

NX2I

RS

Normal x ip at Z2

24

NY2R

RS

Normal y rm at Z2

25

NY2I

RS

Normal y ip at Z2

26

TXY2R

RS

Shear xy rm at Z2

27

TXY2I

RS

Shear xy ip at Z2

28

NZ1R

RS

Normal z rm at Z1 or n/a

29

NZ1I

RS

Normal z ip at Z1 or n/a

30

TYZ1R

RS

Shear yz rm at Z1 or n/a

31

TYZ1I

RS

Shear yz ip at Z1 or n/a

32

TZX1R

RS

Shear zx rm at Z1 or n/a

33

TZX1I

RS

Shear zx ip at Z1 or n/a

Words 7 through 33 repeat 003 times TCODE,7 =2 2

Random Response UNDEF

None

DMAP Programmer’s Guide

5-205

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

End TCODE,7 End SCODE,6 ELTYPE =191

Beam view element (VUBEAM)

2

PARENT

I

Parent p-element identification number

3

COORD

I

CID coordinate system identification number

4

ICORD

CHAR4

ICORD flat/curved and so on

TCODE,7 =0

Real

5

VUGRID

I

VU grid ID for output grid

6

POSIT

RS

x/L position of VU grid identification number

7

POS(3)

RS

Y, Z, W coordinate of output point

10

NX

RS

Normal x

11

TXY

RS

Shear xy

12

TZX

RS

Shear zx

Words 7 through 12 repeat 4 times 13

MAXLONG

RS

Max longitudinal

14

MINLONG

RS

Min longitudinal

Words 5 through 14 repeat 2 times TCODE,7 =1

Real / Imaginary

5

VUGRID

I

VU grid ID for output grid

6

POSIT

RS

x/L position of VU grid identification number

7

POS(3)

RS

Y, Z, W coordinate of output point

10

NXR

RS

Normal x RM

11

NXI

RS

Normal x IP

12

TXYR

RS

Shear xy RM

13

TXYI

RS

Shear xy IP

14

TZXR

RS

Shear zx RM

5-206

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word 15

TZXI

Type RS

Description Shear zx IP

Words 7 through 15 repeat 4 times Words 5 through 15 repeat 2 times TCODE,7 =2 2

Random Response UNDEF

None

End TCODE,7 ELTYPE =192

CVINT

2

None

UNDEF

ELTYPE =193

QUADFR

2

None

UNDEF

ELTYPE =194

TRIAFR

2

None

UNDEF

ELTYPE =195

LINEFR

2

None

UNDEF

ELTYPE =196

LINXFR

2

None

UNDEF

ELTYPE =197

GMINTS

2

None

UNDEF

ELTYPE =198

CNVPEL

2

None

UNDEF

ELTYPE =199

VUHBDY

2

None

UNDEF Name

Word

Type

ELTYPE =200

CWELD

2

None

UNDEF

Description

DMAP Programmer’s Guide

5-207

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ELTYPE =201

Hyperelastic quadrilateral 4-noded, nonlinear format (QUAD4FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GRID

Words 3 through 13 repeat 004 times ELTYPE =202

Hyperelastic hexahedron 8-noded, nonlinear format (HEXA8FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

5-208

DMAP Programmer’s Guide

Grid or Gaus

Data Block Descriptions O-V

Name

Word

Type

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description

Words 3 through 17 repeat 008 times ELTYPE =203

Slideline contact (SLIF1D)

2

REGIONID

I

Contact region identification number

3

MGRID1

I

Master grid 1

4

MGRID2

I

Master grid 2

5

SCOORD

RS

Surface coordinate

6

F

RS

Normal force

7

S

RS

Shear force

8

SIGMA

RS

Normal stress

9

TAU

RS

Shear stress

10

NGAP

RS

Normal gap

11

SLIP

RS

Slip

12

SLIPRAT

RS

Slip ratio

13

SLIPCODE(2)

CHAR4

Slip code

ELTYPE =204

Hyperelastic pentahedron 6-noded, nonlinear format (PENTA6FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

Grid or Gaus

DMAP Programmer’s Guide

5-209

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description

Words 3 through 17 repeat 006 times ELTYPE =205

Hyperelastic tetrahedron 4-noded, nonlinear format (TETRA4FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

5-210

DMAP Programmer’s Guide

GAUS

Data Block Descriptions O-V

Name

Word

Type

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description

Words 3 through 17 repeat 001 times ELTYPE =206

Hyperelastic triangular 3-noded, nonlinear format (TRIA3FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GAUS

Words 3 through 13 repeat 001 times ELTYPE =207

Hyperelastic hexahedron 20-noded, nonlinear format (HEXAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

GAUS

DMAP Programmer’s Guide

5-211

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description

Words 3 through 17 repeat 027 times ELTYPE =208

Hyperelastic quadrilateral 8-noded, nonlinear format (QUADFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GAUS

Words 3 through 13 repeat 009 times ELTYPE =209

5-212

DMAP Programmer’s Guide

Hyperelastic pentahedron 15-noded nonlinear format (PENTAFD)

Data Block Descriptions O-V

Name

Word

Type

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description GAUS

Words 3 through 17 repeat 021 times Name

Word

Type

Description

ELTYPE =210

Hyperelastic tetrahedron 10-noded nonlinear format (TETRAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

GAUS

DMAP Programmer’s Guide

5-213

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description

Words 3 through 17 repeat 005 times ELTYPE =211

Hyperelastic triangular 6-noded, nonlinear format (TRIAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GRID

Words 3 through 13 repeat 003 times ELTYPE =212

5-214

DMAP Programmer’s Guide

Hyperelastic axi. triangular 3-noded nonlinear format (TRIAX3FD)

Data Block Descriptions O-V

Name

Word

Type

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

Description GAUS

Words 3 through 13 repeat 001 times ELTYPE =213

Hyperelastic axi. triangular 6-noded nonlinear format (TRIAXFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GAUS

DMAP Programmer’s Guide

5-215

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

Words 3 through 13 repeat 003 times ELTYPE =214

Hyperelastic axi. quadrilateral 4-noded nonlinear format(QUADX4FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GAUS

Words 3 through 13 repeat 004 times ELTYPE =215

Hyperelastic axi. quadrilateral 8-noded nonlinear format (QUADXFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

5-216

DMAP Programmer’s Guide

GAUS

Data Block Descriptions O-V

Name

Word

Type

11

EY

RS

12

EZ

RS

13

EXY

RS

Description

Words 3 through 13 repeat 009 times ELTYPE =216

Hyperelastic tetrahedron 4-noded nonlinear format (TETRA4FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

GRID

Words 3 through 17 repeat 004 times ELTYPE =217

Hyperelastic triangular 3-noded nonlinear format (TRIA3FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

GRID

DMAP Programmer’s Guide

5-217

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

Description

Words 3 through 13 repeat 003 times ELTYPE =218

Hyperelastic hexahedron 20-noded nonlinear format (HEXAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

5-218

DMAP Programmer’s Guide

GRID

Data Block Descriptions O-V

Name

Word 17

EZX

Type

Description

RS

Words 3 through 17 repeat 008 times ELTYPE =219

Hyperelastic quadrilateral 8-noded nonlinear format (QUADFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GRID

Words 3 through 13 repeat 004 times Name

Word

Type

Description

ELTYPE =220

Hyperelastic pentahedron 15-noded nonlinear format (PENTAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

GRID

DMAP Programmer’s Guide

5-219

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

17

EZX

RS

Description

Words 3 through 17 repeat 006 times ELTYPE =221

Hyperelastic tetrahedron 10-noded nonlinear format (TETRAFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

SYZ

RS

9

SZX

RS

10

PRESSURE

RS

11

VOLSTR

RS

12

EX

RS

13

EY

RS

14

EZ

RS

15

EXY

RS

16

EYZ

RS

5-220

DMAP Programmer’s Guide

GRID

Data Block Descriptions O-V

Name

Word 17

EZX

Type

Description

RS

Words 3 through 17 repeat 004 times ELTYPE =222

Hyperelastic axi. triangular 3-noded nonlinear format (TRIAX3FD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

GRID

Words 3 through 13 repeat 003 times ELTYPE =223

Hyperelastic axi. quadrilateral 8-noded nonlinear format (QUADXFD)

2

TYPE

CHAR4

3

ID

I

4

SX

RS

5

SY

RS

6

SZ

RS

7

SXY

RS

8

PRESSURE

RS

9

VOLSTR

RS

GRID

DMAP Programmer’s Guide

5-221

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

10

EX

RS

11

EY

RS

12

EZ

RS

13

EXY

RS

Description

Words 3 through 13 repeat 004 times ELTYPE =224

Nonlinear ELAS1

2

F

RS

Force

3

S

RS

Stress

ELTYPE =225

Nonlinear ELAS3

2

F

RS

Force

3

S

RS

Stress

ELTYPE =226

Nonlinear BUSH

2

FX

RS

Force X

3

FY

RS

Force Y

4

FZ

RS

Force Z

5

STX

RS

Stress Translational X

6

STY

RS

Stress Translational Y

7

STZ

RS

Stress Translational Z

8

ETX

RS

Strain Rotational X

9

ETY

RS

Strain Rotational Y

10

ETZ

RS

Strain Rotational Z

11

MX

RS

Moment X

12

MY

RS

Moment Y

13

MZ

RS

Moment Z

14

SRX

RS

Stress Rotational X

15

SRY

RS

Stress Rotational Y

5-222

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

16

SRZ

RS

Stress Rotational Z

17

ERX

RS

Strain Rotational X

18

ERY

RS

Strain Rotational Y

19

ERZ

RS

Strain Rotational Z

ELTYPE =227

Triangular shell element (CTRIAR)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5

EXY1

RS

Shear in xy at Z1

6

EA1

RS

Theta ( Shear Angle ) at Z1

7

EMJRP1

RS

Major Principal at Z1

8

EMNRP1

RS

Minor Principal at Z1

9

EMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

EX2

RS

Normal in x at Z2

12

EY2

RS

Normal in y at Z2

13

EXY2

RS

Shear in xy at Z2

14

EA2

RS

Theta (Shear Angle) at Z2

15

EMJRP2

RS

Major Principal at Z2

16

EMNRP2

RS

Minor Principal at Z2

17

EMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

Real / Imaginary

2

FD1

RS

Z1 = Fibre Distance

3

EX1R

RS

Normal in x at Z1

DMAP Programmer’s Guide

5-223

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

4

EX1I

RS

Normal in x at Z1

5

EY1R

RS

Normal in y at Z1

6

EY1I

RS

Normal in y at Z1

7

EXY1R

RS

Shear in xy at Z1

8

EXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

EX2R

RS

Normal in x at Z2

11

EX2I

RS

Normal in x at Z2

12

EY2R

RS

Normal in y at Z2

13

EY2I

RS

Normal in y at Z2

14

EXY2R

RS

Shear in xy at Z2

15

EXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5

EXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

EX2

RS

Normal in x at Z2

8

EY2

RS

Normal in y at Z2

9

EXY2

RS

Shear in xy at Z2

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

5-224

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

SA1

RS

Theta ( Shear Angle ) at Z1

7

SMJRP1

RS

Major Principal at Z1

8

SMNRP1

RS

Minor Principal at Z1

9

SMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

SX2

RS

Normal in x at Z2

12

SY2

RS

Normal in y at Z2

13

TXY2

RS

Shear in xy at Z2

14

SA2

RS

Theta (Shear Angle) at Z2

15

SMJRP2

RS

Major Principal at Z2

16

SMNRP2

RS

Minor Principal at Z2

17

TMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

Real / Imaginary

2

FD1

RS

Z1 = Fibre Distance

3

SX1R

RS

Normal in x at Z1

4

SX1I

RS

Normal in x at Z1

5

SY1R

RS

Normal in y at Z1

6

SY1I

RS

Normal in y at Z1

7

TXY1R

RS

Shear in xy at Z1

8

TXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

SX2R

RS

Normal in x at Z2

11

SX2I

RS

Normal in x at Z2

12

SY2R

RS

Normal in y at Z2

DMAP Programmer’s Guide

5-225

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

13

SY2I

RS

Normal in y at Z2

14

TXY2R

RS

Shear in xy at Z2

15

TXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

SX2

RS

Normal in x at Z2

8

SY2

RS

Normal in y at Z2

9

TXY2

RS

Shear in xy at Z2

End TCODE,7 End SCODE,6 ELTYPE =228

Quadrilateral plate element (CQUADR)

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

5

EXY1

RS

Shear in xy at Z1

6

EA1

RS

Theta ( Shear Angle ) at Z1

7

EMJRP1

RS

Major Principal at Z1

8

EMNRP1

RS

Minor Principal at Z1

9

EMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

5-226

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

11

EX2

RS

Normal in x at Z2

12

EY2

RS

Normal in y at Z2

13

EXY2

RS

Shear in xy at Z2

14

EA2

RS

Theta (Shear Angle) at Z2

15

EMJRP2

RS

Major Principal at Z2

16

EMNRP2

RS

Minor Principal at Z2

17

EMAX2

RS

Maximum Shear at Z2

TCODE,7 =1

Real / Imaginary

2

FD1

RS

Z1 = Fibre Distance

3

EX1R

RS

Normal in x at Z1

4

EX1I

RS

Normal in x at Z1

5

EY1R

RS

Normal in y at Z1

6

EY1I

RS

Normal in y at Z1

7

EXY1R

RS

Shear in xy at Z1

8

EXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

EX2R

RS

Normal in x at Z2

11

EX2I

RS

Normal in x at Z2

12

EY2R

RS

Normal in y at Z2

13

EY2I

RS

Normal in y at Z2

14

EXY2R

RS

Shear in xy at Z2

15

EXY2I

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

EX1

RS

Normal in x at Z1

4

EY1

RS

Normal in y at Z1

DMAP Programmer’s Guide

5-227

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

5

EXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

EX2

RS

Normal in x at Z2

8

EY2

RS

Normal in y at Z2

9

EXY2

RS

Shear in xy at Z2

End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

SA1

RS

Theta ( Shear Angle ) at Z1

7

SMJRP1

RS

Major Principal at Z1

8

SMNRP1

RS

Minor Principal at Z1

9

SMAX1

RS

Maximum Shear at Z1

10

FD2

RS

Z2 = Fibre Distance

11

SX2

RS

Normal in x at Z2

12

SY2

RS

Normal in y at Z2

13

TXY2

RS

Shear in xy at Z2

14

SA2

RS

Theta (Shear Angle) at Z2

15

SMJRP2

RS

Major Principal at Z2

16

SMNRP2

RS

Minor Principal at Z2

17

SMAX2

RS

Maximum Shear at Z2

TCODE,7 =1 2

5-228

Real / Imaginary FD1

DMAP Programmer’s Guide

RS

Z1 = Fibre Distance

Data Block Descriptions O-V

Name

Word

Type

Description

3

SX1R

RS

Normal in x at Z1

4

SX1I

RS

Normal in x at Z1

5

SY1R

RS

Normal in y at Z1

6

SY1I

RS

Normal in y at Z1

7

TXY1R

RS

Shear in xy at Z1

8

TXY1I

RS

Shear in xy at Z1

9

FD2

RS

Z2 = Fibre Distance

10

SX2R

RS

Normal in x at Z2

11

SX2I

RS

Normal in x at Z2

12

SY2R

RS

Normal in y at Z2

13

SY2I

RS

Normal in y at Z2

14

TXY2R

RS

Shear in xy at Z2

TCODE,7 =2

Random Response

2

FD1

RS

Z1 = Fibre Distance

3

SX1

RS

Normal in x at Z1

4

SY1

RS

Normal in y at Z1

5

TXY1

RS

Shear in xy at Z1

6

FD2

RS

Z2 = Fibre Distance

7

SX2

RS

Normal in x at Z2

8

SY2

RS

Normal in y at Z2

9

TXY2

RS

Shear in xy at Z2

End TCODE,7 End SCODE,6 Word

Name

Type

ELTYPE =232

QUADR composite

SCODE,6 =0

Strain

Description

DMAP Programmer’s Guide

5-229

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

PLY

I

Lamina Number

3

EX1

RS

Normal-1

4

EY1

RS

Normal-2

5

ET1

RS

Shear-12

6

EL1

RS

Shear-1Z

7

EL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

EMJRP1

RS

Major Principal

10

EMNRP1

RS

Minor Principal

11

ETMAX1

RS

von Mises or Maximum shear

SCODE,6 =01

Stress

2

PLY

I

Lamina Number

3

SX1

RS

Normal-1

4

SY1

RS

Normal-2

5

T1

RS

Shear-12

6

SL1

RS

Shear-1Z

7

SL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

MJRP1

RS

Major Principal

10

MNRP1

RS

Minor Principal

11

TMAX1

RS

von Mises or Maximum shear

End SCODE,6 ELTYPE =233

TRIAR composite (Same as TRIAR composite)

SCODE,6 =0

Strain

2

PLY

I

Lamina Number

3

EX1

RS

Normal-1

5-230

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

4

EY1

RS

Normal-2

5

ET1

RS

Shear-12

6

EL1

RS

Shear-1Z

7

EL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

EMJRP1

RS

Major Principal

10

EMNRP1

RS

Minor Principal

11

ETMAX1

RS

von Mises or Maximum shear

SCODE,6 =01

Stress

2

PLY

I

Lamina Number

3

SX1

RS

Normal-1

4

SY1

RS

Normal-2

5

T1

RS

Shear-12

6

SL1

RS

Shear-1Z

7

SL2

RS

Shear-2Z

8

A1

RS

Shear angle

9

MJRP1

RS

Major Principal

10

MNRP1

RS

Minor Principal

11

TMAX1

RS

von Mises or Maximum shear

End SCODE,6 Name

Word

Type

Description

ELTYPE =240

CTRIA6 - Nonlinear - Center and corners

2

TERM

CHAR4

“CEN”

3

GRID ID

I

0 for center

4

FD1

RS

Z1 = Fiber distance

5

SX1

RS

Stress in x at Z1

DMAP Programmer’s Guide

5-231

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

6

SY1

RS

Stress in y at Z1

7

SZ1

RS

Stress in z at Z1

8

TXY1

RS

Shear stress in xy at Z1

9

ES

RS

Equivalent stress at Z1

10

EPS1

RS

Effective plastic/inelastic strain at Z1

11

ECS1

RS

Effective creep strain at Z1

12

EX1

RS

Strain in x at Z1

13

EY1

RS

Strain in y at Z1

14

EZ1

None

Strain in z at Z1

15

ETXY1

RS

Shear strain in xy at Z1

16

FD2

RS

Z2 = Fiber distance

17

SX2

RS

Stress in x at Z2

18

SY2

RS

Stress in y at Z2

19

SZ2

None

Stress in z at Z2

20

TXY2

RS

Shear stress in xy at Z2

21

ES2

RS

Equivalent stress at Z2

22

EPS2

RS

Effective plastic/inelastic strain at Z2

23

ECS2

RS

Effective creep strain at Z2

24

EX2

RS

Strain in x at Z2

25

EY2

RS

Strain in y at Z2

26

EZ2

None

Strain in z at Z2

27

ETXY2

RS

Shear strain in xy at Z2

Words 3 through 27 process 4 times Name

Word

Type

Description

ELTYPE =241

CQUAD8 - Nonlinear - Center and corners

2

CHAR4

5-232

TERM

DMAP Programmer’s Guide

“CEN”

Data Block Descriptions O-V

Name

Word

Type

Description

3

GRID ID

I

0 for center

4

FD1

RS

Z1 = Fiber distance

5

SX1

RS

Stress in x at Z1

6

SY1

RS

Stress in y at Z1

7

SZ1

RS

Stress in z at Z1

8

TXY1

RS

Shear stress in xy at Z1

9

ES

RS

Equivalent stress at Z1

10

EPS1

RS

Effective plastic/inelastic strain at Z1

11

ECS1

RS

Effective creep strain at Z1

12

EX1

RS

Strain in x at Z1

13

EY1

RS

Strain in y at Z1

14

EZ1

None

Strain in z at Z1

15

ETXY1

RS

Shear strain in xy at Z1

16

FD2

RS

Z2 = Fiber distance

17

SX2

RS

Stress in x at Z2

18

SY2

RS

Stress in y at Z2

19

SZ2

None

Stress in z at Z2

20

TXY2

RS

Shear stress in xy at Z2

21

ES2

RS

Equivalent stress at Z2

22

EPS2

RS

Effective plastic/inelastic strain at Z2

23

ECS2

RS

Effective creep strain at Z2

24

EX2

RS

Strain in x at Z2

25

EY2

RS

Strain in y at Z2

26

EZ2

None

Strain in z at Z2

27

ETXY2

RS

Shear strain in xy at Z2

Words 3 through 27 process 5 times

DMAP Programmer’s Guide

5-233

Data Block Descriptions O-V

Chapter 5

ELTYPE =242

Axisymmetric triangular element (CTRAX3) – Linear Stress/Strain - Center and corners

TCODE,7 =0

Real

2

CTYPE

CHAR4

Coordinate Type (BCD)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

MAXP

RS

Maximum Principal

9

TMAX

RS

Maximum Shear

10

OCTS

RS

Octahedral

Words 3 through 10 process 4 times TCODE,7 =1

Real / Imaginary

2

CTYPE

CHAR4

Coordinate Type (BCD)

3

LOC

I

Location Code

4

RSR

RS

Radial Stress

5

RSI

RS

Radial Stress

6

AZSR

RS

Azimuthal Stress

7

AZSI

RS

Azimuthal Stress

8

ASR

RS

Axial Stress

9

ASI

RS

Axial Stress

10

SSR

RS

Shear Stress

11

SSI

RS

Shear Stress

Words 3 through 11 process 4 times TCODE,7 =2

Random Response

2

CTYPE

CHAR4

Coordinate Type (BCD)

3

LOC

I

Location Code

5-234

DMAP Programmer’s Guide

Data Block Descriptions O-V

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

Words 3 through 7 process 4 times End TCODE,7 ELTYPE =243

Axisymmetric quad element (CQUADX4) – Linear Stress/Strain - Center and corners

TCODE,7 =0

Real

2

CTYPE

CHAR4

Coordinate Type (BCD)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

MAXP

RS

Maximum Principal

9

TMAX

RS

Maximum Shear

10

OCTS

RS

Octahedral

Words 3 through 10 process 5 times TCODE,7 =1

Real / Imaginary

2

LOC

I

Location Code

3

RSR

RS

Radial Stress

4

RSI

RS

Radial Stress

5

AZSR

RS

Azimuthal Stress

6

AZSI

RS

Azimuthal Stress

7

ASR

RS

Axial Stress

8

ASI

RS

Axial Stress

DMAP Programmer’s Guide

5-235

Data Block Descriptions O-V

Chapter 5

9

SSR

RS

Shear Stress

10

SSI

RS

Shear Stress

Words 2 through 10 process 5 times TCODE,7 =2

Random Response

2

LOC

I

Location Code

3

RS

RS

Radial Stress

4

AZS

RS

Azimuthal Stress

5

AS

RS

Axial Stress

6

SS

RS

Shear Stress

Words 2 through 6 process 5 times End TCODE,7 ELTYPE =244

Axisymmetric triangle element (CTRAX6) – Linear Stress/Strain - Center and corners

TCODE,7 =0

Real

2

CTYPE

CHAR4

Coordinate Type (BCD)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

MAXP

RS

Maximum Principal

9

TMAX

RS

Maximum Shear

10

OCTS

RS

Octahedral

Words 3 through 10 process 4 times TCODE,7 =1

Real / Imaginary

2

LOC

I

Location Code

3

RSR

RS

Radial Stress

5-236

DMAP Programmer’s Guide

Data Block Descriptions O-V

4

RSI

RS

Radial Stress

5

AZSR

RS

Azimuthal Stress

6

AZSI

RS

Azimuthal Stress

7

ASR

RS

Axial Stress

8

ASI

RS

Axial Stress

9

SSR

RS

Shear Stress

10

SSI

RS

Shear Stress

Words 2 through 10 process 4 times TCODE,7 =2

Random Response

2

LOC

I

Location Code

3

RS

RS

Radial Stress

4

AZS

RS

Azimuthal Stress

5

AS

RS

Axial Stress

6

SS

RS

Shear Stress

Words 2 through 6 process 4 times End TCODE,7 ELTYPE =245

Axisymmetric quad element (CQUADX8) – Linear Stress/Strain - Center and corners

TCODE,7 =0

Real

2

CTYPE

CHAR4

Coordinate Type (BCD)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

MAXP

RS

Maximum Principal

9

TMAX

RS

Maximum Shear

DMAP Programmer’s Guide

5-237

Data Block Descriptions O-V

Chapter 5

10

OCTS

RS

Octahedral

Words 3 through 10 process 5 times TCODE,7 =1

Real / Imaginary

2

LOC

I

Location Code

3

RSR

RS

Radial Stress

4

RSI

RS

Radial Stress

5

AZSR

RS

Azimuthal Stress

6

AZSI

RS

Azimuthal Stress

7

ASR

RS

Axial Stress

8

ASI

RS

Axial Stress

9

SSR

RS

Shear Stress

10

SSI

RS

Shear Stress

Words 2 through 10 process 5 times TCODE,7 =2

Random Response

2

LOC

I

Location Code

3

RS

RS

Radial Stress

4

AZS

RS

Azimuthal Stress

5

AS

RS

Axial Stress

6

SS

RS

Shear Stress

Words 2 through 6 process 5 times End TCODE,7 ELTYPE =246

Axisymmetric triangle element (CTRAX3) – Nonlinear Stress/Strain - Center and corners

2

CTYPE

CHAR4

Coordinate Type (GRID)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

5-238

DMAP Programmer’s Guide

Data Block Descriptions O-V

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

ES

RS

Equivalent Stress

9

EPS

RS

Effective Plastic Strain

10

ECS

RS

Effective Creep Strain

11

RE

RS

Radial Strain

12

AZE

RS

Azimuthal Strain

13

AE

RS

Axial Strain

14

SE

RS

Shear Strain

Words 3 through 14 process 4 times ELTYPE =247

Axisymmetric quad element (CQUADX4) – Nonlinear Stress/Strain - Center and corners

2

CTYPE

CHAR4

Coordinate Type (GRID)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

ES

RS

Equivalent Stress

9

EPS

RS

Effective Plastic Strain

10

ECS

RS

Effective Creep Strain

11

RE

RS

Radial Strain

12

AZE

RS

Azimuthal Strain

13

AE

RS

Axial Strain

14

SE

RS

Shear Strain

Words 3 through 14 process 5 times

DMAP Programmer’s Guide

5-239

Data Block Descriptions O-V

Chapter 5

ELTYPE =248

Axisymmetric triangle element (CTRAX6) – Nonlinear Stress/Strain - Center and corners

2

CTYPE

CHAR4

Coordinate Type (GRID)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

ES

RS

Equivalent Stress

9

EPS

RS

Effective Plastic Strain

10

ECS

RS

Effective Creep Strain

11

RE

RS

Radial Strain

12

AZE

RS

Azimuthal Strain

13

AE

RS

Axial Strain

14

SE

RS

Shear Strain

Words 3 through 14 process 4 times ELTYPE =249

Axisymmetric quad element (CQUADX8) – Nonlinear Stress/Strain - Center and corners

2

CTYPE

CHAR4

Coordinate Type (GRID)

3

LOC

I

Location Code

4

RS

RS

Radial Stress

5

AZS

RS

Azimuthal Stress

6

AS

RS

Axial Stress

7

SS

RS

Shear Stress

8

ES

RS

Equivalent Stress

9

EPS

RS

Effective Plastic Strain

10

ECS

RS

Effective Creep Strain

11

RE

RS

Radial Strain

5-240

DMAP Programmer’s Guide

Data Block Descriptions O-V

12

AZE

RS

Azimuthal Strain

13

AE

RS

Axial Strain

14

SE

RS

Shear Strain

Words 3 through 14 process 5 times ELTYPE =250

Axisymmetric triangle element (CTRAX3) – Linear form of hyperelastic – Gauss Location

2

LOC

I

Location Code

3

SX

RS

Radial Stress

4

SZ

RS

Azimuthal Stress

5

SXZ

RS

Axial Stress

6

ANGLE

RS

Shear Stress

7

SMJ

RS

Major Principle

8

SMI

RS

Minor Principle

Words 3 through 8 process 3 times ELTYPE =251

Axisymmetric quad element (CQUADX4) – Linear form of hyperelastic – Gauss Locations

2

LOC

I

Location Code

3

SX

RS

Radial Stress

4

SZ

RS

Azimuthal Stress

5

SXZ

RS

Axial Stress

6

ANGLE

RS

Shear Stress

7

SMJ

RS

Major Principle

8

SMI

RS

Minor Principle

Words 3 through 8 process 4 times ELTYPE =252

Axisymmetric triangle element (CTRAX6) – Linear form of hyperelastic – Gauss Locations

2

I

LOC

Location Code

DMAP Programmer’s Guide

5-241

Data Block Descriptions O-V

Chapter 5

3

SX

RS

Radial Stress

4

SZ

RS

Azimuthal Stress

5

SXZ

RS

Axial Stress

6

ANGLE

RS

Shear Stress

7

SMJ

RS

Major Principle

8

SMI

RS

Minor Principle

Words 3 through 8 process 3 times

ELTYPE =253

Axisymmetric quad element (CQUADX8) – Linear form of hyperelastic – Gauss Locations

2

LOC

I

Location Code

3

SX

RS

Radial Stress

4

SZ

RS

Azimuthal Stress

5

SXZ

RS

Axial Stress

6

ANGLE

RS

Shear Stress

7

SMJ

RS

Major Principle

8

SMI

RS

Minor Principle

Words 3 through 8 process 9 times

Name

Word

Type

Description

ELTYPE =254

CQUAD4 - Nonlinear - Center and corners

2

TERM

CHAR4

“CEN”

3

GRID ID

I

0 for center

4

FD1

RS

Z1 = Fiber distance

5

SX1

RS

Stress in x at Z1

6

SY1

RS

Stress in y at Z1

7

SZ1

RS

Stress in z at Z1

8

TXY1

RS

Shear stress in xy at Z1

9

ES

RS

Equivalent stress at Z1

5-242

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

10

EPS1

RS

Effective plastic/inelastic strain at Z1

11

ECS1

RS

Effective creep strain at Z1

12

EX1

RS

Strain in x at Z1

13

EY1

RS

Strain in y at Z1

14

EZ1

None

Strain in z at Z1

15

ETXY1

RS

Shear strain in xy at Z1

16

FD2

RS

Z2 = Fiber distance

17

SX2

RS

Stress in x at Z2

18

SY2

RS

Stress in y at Z2

19

SZ2

None

Stress in z at Z2

20

TXY2

RS

Shear stress in xy at Z2

21

ES2

RS

Equivalent stress at Z2

22

EPS2

RS

Effective plastic/inelastic strain at Z2

23

ECS2

RS

Effective creep strain at Z2

24

EX2

RS

Strain in x at Z2

25

EY2

RS

Strain in y at Z2

26

EZ2

None

Strain in z at Z2

27

ETXY2

RS

Shear strain in xy at Z2

Words 3 through 27 process 5 times ELTYPE = 255

CPYRAM – Linear Strain/Stress

SCODE,6 =0

Strain

TCODE,7 =0

Real

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid ID (0=center)

DMAP Programmer’s Guide

5-243

Chapter 5

Data Block Descriptions O-V

6

EX

RS

Normal in x

7

ETXY

RS

Shear in xy

8

EP1

RS

First principal strain

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

EPR

RS

Mean pressure

13

EOCT

RS

Octahedral shear strain

14

EY

RS

Normal in y

15

ETYZ

RS

Shear in yz

16

EP2

RS

Second principal strain

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

EZ

RS

Normal in z

21

ETZX

RS

Shear in zx

22

EP3

RS

Third principal strain

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 process 6 times TCODE,7 =1

Real / Imaginary

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid ID (0=center)

6

EXR

RS

Normal in x

5-244

DMAP Programmer’s Guide

Data Block Descriptions O-V

7

EYR

RS

Normal in y

8

EZR

RS

Normal in z

9

ETXYR

RS

Shear in xy

10

ETYZR

RS

Shear in yz

11

ETZXR

RS

Shear in zx

12

EXI

RS

Normal in x

13

EYI

RS

Normal in y

14

EZI

RS

Normal in z

15

ETXYI

RS

Shear in xy

16

ETYZI

RS

Shear in yz

17

ETZXI

RS

Shear in zx

Words 5 through 17 process 6 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid ID (0=center)

6

EX

RS

Normal in x

7

EY

RS

Normal in y

8

EZ

RS

Normal in z

9

ETXY

RS

Shear in xy

10

ETYZ

RS

Shear in yz

11

ETZX

RS

Shear in zx

Words 5 through 11 process 6 times End TCODE,7 SCODE,6 =01

Stress

TCODE,7 =0

Real

DMAP Programmer’s Guide

5-245

Data Block Descriptions O-V

Chapter 5

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

TXY

RS

Shear in xy

8

P1

RS

First principal stress

9

P1X

RS

First principal x cosine

10

P2X

RS

Second principal x cosine

11

P3X

RS

Third principal x cosine

12

PR

RS

Mean pressure

13

OCT

RS

Octahedral shear stress

14

SY

RS

Normal in y

15

TYZ

RS

Shear in yz

16

P2

RS

Second principal stress

17

P1Y

RS

First principal y cosine

18

P2Y

RS

Second principal y cosine

19

P3Y

RS

Third principal y cosine

20

SZ

RS

Normal in z

21

TZX

RS

Shear in zx

22

P3

RS

Third principal stress

23

P1Z

RS

First principal z cosine

24

P2Z

RS

Second principal z cosine

25

P3Z

RS

Third principal z cosine

Words 5 through 25 process 6 times TCODE,7 =1 2

5-246

Real / Imaginary CID

DMAP Programmer’s Guide

I

Stress Coordinate System

Data Block Descriptions O-V

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SXR

RS

Normal in x

7

SYR

RS

Normal in y

8

SZR

RS

Normal in z

9

TXYR

RS

Shear in xy

10

TYZR

RS

Shear in yz

11

TZXR

RS

Shear in zx

12

SXI

RS

Normal in x

13

SYI

RS

Normal in y

14

SZI

RS

Normal in z

15

TXYI

RS

Shear in xy

16

TYZI

RS

Shear in yz

17

TZXI

RS

Shear in zx

Words 5 through 17 process 6 times TCODE,7 =2

Random Response

2

CID

I

Stress Coordinate System

3

CTYPE

CHAR4

Coordinate System Type (BCD)

4

NODEF

I

Number of Active Points

5

GRID

I

External grid identification number (0=center)

6

SX

RS

Normal in x

7

SY

RS

Normal in y

8

SZ

RS

Normal in z

9

TXY

RS

Shear in xy

10

TYZ

RS

Shear in yz

11

TZX

RS

Shear in zx

DMAP Programmer’s Guide

5-247

Data Block Descriptions O-V

Chapter 5

Words 5 through 11 process 6 times End TCODE,7 End SCODE,6

ELTYPE =256

CPYRAM - Nonlinear

2

CTYPE

CHAR4

GRID or GAUSS

3

GRID

I

0 for center

4

SX

RS

Stress in x

5

SY

RS

Stress in y

6

SZ

RS

Stress in z

7

SXY

RS

Stress in xy

8

SYZ

RS

Stress in yz

9

SZX

RS

Stress in zx

10

SE

RS

Equivalent stress

11

EPS

RS

Effective plastic strain

12

ECS

RS

Effective creep strain

13

EX

RS

Strain in x

14

EY

RS

Strain in y

15

EZ

RS

Strain in z

16

EXY

RS

Strain in xy

17

EYZ

RS

Strain in yz

18

EZX

RS

Strain in zx

Words 3 through 18 process 6 times

ELTYPE =257

CPYRAM (linear element, 5 grids) – Hyperelastic nonlinear format

2

CTYPE

CHAR4

GRID

3

ID

I

Grid ID

4

SX

RS

Stress in X

5-248

DMAP Programmer’s Guide

Data Block Descriptions O-V

5

SY

RS

Stress in Y

6

SZ

RS

Stress in Z

7

SXY

RS

Stress in XY

8

SYZ

RS

Stress in YZ

9

SZX

RS

Stress in ZX

10

PRESSURE

RS

Pressure

11

VOLSTR

RS

Volumetric Strain

12

EX

RS

Strain in X

13

EY

RS

Strain in Y

14

EZ

RS

Strain in Z

15

EXY

RS

Strain in XY

16

EYZ

RS

Strain in YZ

17

EZX

RS

Strain in ZX

Words 3 through 17 process 5 times ELTYPE =258

CPYRAM (parabolic element, 13 grids) – Hyperelastic nonlinear format

2

TYPE

CHAR4

GRID

3

ID

I

Grid ID

4

SX

RS

Stress in X

5

SY

RS

Stress in Y

6

SZ

RS

Stress in Z

7

SXY

RS

Stress in XY

8

SYZ

RS

Stress in YZ

9

SZX

RS

Stress in ZX

10

PRESSURE

RS

Pressure

11

VOLSTR

RS

Volumetric Strain

12

EX

RS

Strain in X

DMAP Programmer’s Guide

5-249

Data Block Descriptions O-V

Chapter 5

13

EY

RS

Strain in Y

14

EZ

RS

Strain in Z

15

EXY

RS

Strain in XY

16

EYZ

RS

Strain in YZ

17

EZX

RS

Strain in ZX

Words 3 through 17 process 5 times ELTYPE =259

Reserved for hyperelastic PYRAM 5-noded, linear form.

ELTYPE =260

Reserved for hyperelastic PYRAM 13-noded, linear form.

ELTYPE =261

Axisymmetric triangle element (CTRAX3) – Nonlinear form of hyperelastic

2

TYPE

CHAR4

GAUS or GRID

3

LOC

I

Location Code

4

SX

RS

Radial Stress

5

SY

RS

Azimuthal Stress

6

SZ

RS

Axial Stress

7

SXY

RS

Shear Stress

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volumetric Strain

10

EX

RS

Radial Strain

11

EY

RS

Azimuthal Strain

12

EZ

RS

Axial Strain

13

EXY

RS

Shear Strain

Words 3 through 13 process 3 times ELTYPE =262

Axisymmetric quad element (CQUADX4) – Nonlinear form of hyperelastic

2

TYPE

CHAR4

5-250

DMAP Programmer’s Guide

GAUS or GRID

Data Block Descriptions O-V

3

LOC

I

Location Code

4

SX

RS

Radial Stress

5

SY

RS

Azimuthal Stress

6

SZ

RS

Axial Stress

7

SXY

RS

Shear Stress

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volumetric Strain

10

EX

RS

Radial Strain

11

EY

RS

Azimuthal Strain

12

EZ

RS

Axial Strain

13

EXY

RS

Shear Strain

Words 3 through 13 process 4 times ELTYPE =263

Axisymmetric triangle element (CTRAX6) – Nonlinear form of hyperelastic

2

TYPE

CHAR4

GAUS or GRID

3

LOC

I

Location Code

4

SX

RS

Radial Stress

5

SY

RS

Azimuthal Stress

6

SZ

RS

Axial Stress

7

SXY

RS

Shear Stress

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volumetric Strain

10

EX

RS

Radial Strain

11

EY

RS

Azimuthal Strain

12

EZ

RS

Axial Strain

13

EXY

RS

Shear Strain

Words 3 through 13 process 3 times

DMAP Programmer’s Guide

5-251

Data Block Descriptions O-V

Chapter 5

ELTYPE =264

Axisymmetric quad element (CQUADX8) – Nonlinear form of hyperelastic – Grid Locations

2

TYPE

CHAR4

GRID

3

LOC

I

Location Code

4

SX

RS

Radial Stress

5

SY

RS

Azimuthal Stress

6

SZ

RS

Axial Stress

7

SXY

RS

Shear Stress

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volumetric Strain

10

EX

RS

Radial Strain

11

EY

RS

Azimuthal Strain

12

EZ

RS

Axial Strain

13

EXY

RS

Shear Strain

Words 3 through 13 process 4 times ELTYPE =266

Axisymmetric quad element (CQUADX8) – Nonlinear form of hyperelastic – 9 Gauss Locations

2

TYPE

CHAR4

GAUS

3

LOC

I

Location Code

4

SX

RS

Radial Stress

5

SY

RS

Azimuthal Stress

6

SZ

RS

Axial Stress

7

SXY

RS

Shear Stress

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volumetric Strain

10

EX

RS

Radial Strain

11

EY

RS

Azimuthal Strain

12

EZ

RS

Axial Strain

5-252

DMAP Programmer’s Guide

Data Block Descriptions O-V

13

EXY

RS

Shear Strain

Words 3 through 13 process 9 times ELTYPE =269

Composite HEXA element (CHEXAL) – Center and corners

1

I

PLY

SCODE,6=0

Strain

PLSLOC=0

Center option

Lamina number

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

EX1

RS

Normal strain in the 1-direction

5

EY1

RS

Normal strain in the 2-direction

6

ET1

RS

Shear strain in the 12-plane

7

EZ1

RS

Normal strain in the 3-direction

8

EL1

RS

Shear strain in the 13-plane

9

EL2

RS

Shear strain in the 23-plane

10

ETMAX1

RS

Von Mises strain

PLSLOC=1

Corner option

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

EX1

RS

Normal strain in the 1-direction

5

EY1

RS

Normal strain in the 2-direction

6

ET1

RS

Shear strain in the 12-plane

7

EZ1

RS

Normal strain in the 3-direction

8

EL1

RS

Shear strain in the 13-plane

9

EL2

RS

Shear strain in the 23-plane

10

ETMAX1

RS

Von Mises strain

Words 2 through 10 repeat 5 times SCODE,6=1

Stress

DMAP Programmer’s Guide

5-253

Data Block Descriptions O-V

Chapter 5

PLSLOC=0

Center option

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

SX1

RS

Normal stress in the 1-direction

5

SY1

RS

Normal stress in the 2-direction

6

ST1

RS

Shear stress in the 12-plane

7

SZ1

RS

Normal stress in the 3-direction

8

SL1

RS

Shear stress in the 13-plane

9

SL2

RS

Shear stress in the 23-plane

10

STMAX1

RS

Von Mises stress

PLSLOC=1

Corner option

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

SX1

RS

Normal stress in the 1-direction

5

SY1

RS

Normal stress in the 2-direction

6

ST1

RS

Shear stress in the 12-plane

7

SZ1

RS

Normal stress in the 3-direction

8

SL1

RS

Shear stress in the 13-plane

9

SL2

RS

Shear stress in the 23-plane

10

STMAX1

RS

Von Mises stress

Words 2 through 10 repeat 5 times End SCODE,6 ELTYPE =270

Composite PENTA element (CPENTAL) – Center and corners

1

I

PLY

SCODE,6=0

Strain

PLSLOC=0

Center option

2

FLOC

5-254

DMAP Programmer’s Guide

CHAR4

Lamina number

Fiber location (BOT, MID, TOP)

Data Block Descriptions O-V

3

GRID

I

Edge grid ID (center=0)

4

EX1

RS

Normal strain in the 1-direction

5

EY1

RS

Normal strain in the 2-direction

6

ET1

RS

Shear strain in the 12-plane

7

EZ1

RS

Normal strain in the 3-direction

8

EL1

RS

Shear strain in the 13-plane

9

EL2

RS

Shear strain in the 23-plane

10

ETMAX1

RS

Von Mises strain

PLSLOC=1

Corner option

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

EX1

RS

Normal strain in the 1-direction

5

EY1

RS

Normal strain in the 2-direction

6

ET1

RS

Shear strain in the 12-plane

7

EZ1

RS

Normal strain in the 3-direction

8

EL1

RS

Shear strain in the 13-plane

9

EL2

RS

Shear strain in the 23-plane

10

ETMAX1

RS

Von Mises strain

Words 2 through 10 repeat 4 times SCODE,6=1

Stress

PLSLOC=0

Center option

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

SX1

RS

Normal stress in the 1-direction

5

SY1

RS

Normal stress in the 2-direction

6

ST1

RS

Shear stress in the 12-plane

7

SZ1

RS

Normal stress in the 3-direction

DMAP Programmer’s Guide

5-255

Data Block Descriptions O-V

Chapter 5

8

SL1

RS

Shear stress in the 13-plane

9

SL2

RS

Shear stress in the 23-plane

10

STMAX1

RS

Von Mises stress

PLSLOC=1

Corner option

2

FLOC

CHAR4

Fiber location (BOT, MID, TOP)

3

GRID

I

Edge grid ID (center=0)

4

SX1

RS

Normal stress in the 1-direction

5

SY1

RS

Normal stress in the 2-direction

6

ST1

RS

Shear stress in the 12-plane

7

SZ1

RS

Normal stress in the 3-direction

8

SL1

RS

Shear stress in the 13-plane

9

SL2

RS

Shear stress in the 23-plane

10

STMAX1

RS

Von Mises stress

Words 2 through 10 repeat 4 times End SCODE,6 ELTYPE =271

Triangle plane strain (CPLSTN3) – Center

SCODE,6=0

Strain

TCODE,7=0

Real

2

EX

RS

Normal strain in x

3

EY

RS

Normal strain in y

4

EZ

RS

Normal strain in z

5

EXZ

RS

Shear strain in xz

6

EMAX

RS

Von Mises strain

TCODE,7=1

Real / Imaginary

2

EXR

RS

Normal strain in x – real part

3

EXI

RS

Normal strain in x – imaginary part

4

EYR

RS

Normal strain in y – real part

5-256

DMAP Programmer’s Guide

Data Block Descriptions O-V

5

EYI

RS

Normal strain in y – imaginary part

6

EZR

RS

Normal strain in z – real part

7

EZI

RS

Normal strain in z – imaginary part

8

EXYR

RS

Shear strain in xz – real part

9

EXYI

RS

Shear strain in xz – imaginary part

End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

SX

RS

Normal stress in x

3

SY

RS

Normal stress in y

4

SZ

RS

Normal stress in z

5

SXZ

RS

Shear stress in xz

6

SMAX

RS

Von Mises stress

TCODE,7=1

Real / Imaginary

2

SXR

RS

Normal stress in x – real part

3

SXI

RS

Normal stress in x – imaginary part

4

SYR

RS

Normal stress in y – real part

5

SYI

RS

Normal stress in y – imaginary part

6

SZR

RS

Normal stress in z – real part

7

SZI

RS

Normal stress in z – imaginary part

8

SXYR

RS

Shear stress in xz – real part

9

SXYI

RS

Shear stress in xz – imaginary part

End TCODE,7 End SCODE,6 ELTYPE =272

Quadrilateral plane strain (CPLSTN4) – Center and Corners

SCODE,6=0

Strain

TCODE,7=0

Real

DMAP Programmer’s Guide

5-257

Data Block Descriptions O-V

Chapter 5

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EX

RS

Normal strain in x

5

EY

RS

Normal strain in y

6

EZ

RS

Normal strain in z

7

EXZ

RS

Shear strain in xz

8

EMAX

RS

Von Mises strain

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EXR

RS

Normal strain in x – real part

5

EXI

RS

Normal strain in x – imaginary part

6

EYR

RS

Normal strain in y – real part

7

EYI

RS

Normal strain in y – imaginary part

8

EZR

RS

Normal strain in z – real part

9

EZI

RS

Normal strain in z – imaginary part

10

EXZR

RS

Shear strain in xz – real part

11

EXZI

RS

Shear strain in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

5-258

DMAP Programmer’s Guide

Data Block Descriptions O-V

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

SMAX

RS

Von Mises stress

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SXR

RS

Normal stress in x – real part

5

SXI

RS

Normal stress in x – imaginary part

6

SYR

RS

Normal stress in y – real part

7

SYI

RS

Normal stress in y – imaginary part

8

SZR

RS

Normal stress in z – real part

9

SZI

RS

Normal stress in z – imaginary part

10

SXZR

RS

Shear stress in xz – real part

11

SXZI

RS

Shear stress in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 End SCODE,6 ELTYPE =273

Triangle plane strain (CPLSTN6 ) – Center and Corners

SCODE,6=0

Strain

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EX

RS

Normal strain in x

5

EY

RS

Normal strain in y

6

EZ

RS

Normal strain in z

7

EXZ

RS

Shear strain in xz

DMAP Programmer’s Guide

5-259

Data Block Descriptions O-V

Chapter 5

8

EMAX

RS

Von Mises strain

Words 3 through 8 repeat 4 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EXR

RS

Normal strain in x – real part

5

EXI

RS

Normal strain in x – imaginary part

6

EYR

RS

Normal strain in y – real part

7

EYI

RS

Normal strain in y – imaginary part

8

EZR

RS

Normal strain in z – real part

9

EZI

RS

Normal strain in z – imaginary part

10

EXZR

RS

Shear strain in xz – real part

11

EXZI

RS

Shear strain in xz – imaginary part

Words 3 through 11 repeat 4 times End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

SMAX

RS

Von Mises stress

Words 3 through 8 repeat 4 times TCODE,7=1

Real / Imaginary

2

TERM

5-260

DMAP Programmer’s Guide

CHAR4

“CEN”

Data Block Descriptions O-V

3

GRID

I

Grid identification number; 0 for centroid

4

SXR

RS

Normal stress in x – real part

5

SXI

RS

Normal stress in x – imaginary part

6

SYR

RS

Normal stress in y – real part

7

SYI

RS

Normal stress in y – imaginary part

8

SZR

RS

Normal stress in z – real part

9

SZI

RS

Normal stress in z – imaginary part

10

SXZR

RS

Shear stress in xz – real part

11

SXZI

RS

Shear stress in xz – imaginary part

Words 3 through 11 repeat 4 times End TCODE,7 End SCODE,6 ELTYPE =274

Quadrilateral plane strain (CPLSTN8) – Center and Corners

SCODE,6=0

Strain

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EX

RS

Normal strain in x

5

EY

RS

Normal strain in y

6

EZ

RS

Normal strain in z

7

EXZ

RS

Shear strain in xz

8

EMAX

RS

Von Mises strain

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EXR

RS

Normal strain in x – real part

DMAP Programmer’s Guide

5-261

Data Block Descriptions O-V

Chapter 5

5

EXI

RS

Normal strain in x – imaginary part

6

EYR

RS

Normal strain in y – real part

7

EYI

RS

Normal strain in y – imaginary part

8

EZR

RS

Normal strain in z – real part

9

EZI

RS

Normal strain in z – imaginary part

10

EXZR

RS

Shear strain in xz – real part

11

EXZI

RS

Shear strain in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

SMAX

RS

Von Mises stress

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SXR

RS

Normal stress in x – real part

5

SXI

RS

Normal stress in x – imaginary part

6

SYR

RS

Normal stress in y – real part

7

SYI

RS

Normal stress in y – imaginary part

8

SZR

RS

Normal stress in z – real part

5-262

DMAP Programmer’s Guide

Data Block Descriptions O-V

9

SZI

RS

Normal stress in z – imaginary part

10

SXZR

RS

Shear stress in xz – real part

11

SXZI

RS

Shear stress in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 End SCODE,6 ELTYPE =275

Triangle plane stress (CPLSTS3) – Center

SCODE,6=0

Strain

TCODE,7=0

Real

2

EX

RS

Normal strain in x

3

EY

RS

Normal strain in y

4

EZ

RS

Normal strain in z

5

EXZ

RS

Shear strain in xz

6

EMAX

RS

Von Mises strain

TCODE,7=1

Real / Imaginary

2

EXR

RS

Normal strain in x – real part

3

EXI

RS

Normal strain in x – imaginary part

4

EYR

RS

Normal strain in y – real part

5

EYI

RS

Normal strain in y – imaginary part

6

EZR

RS

Normal strain in z – real part

7

EZI

RS

Normal strain in z – imaginary part

8

EXYR

RS

Shear strain in xz – real part

9

EXYI

RS

Shear strain in xz – imaginary part

End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

SX

RS

Normal stress in x

DMAP Programmer’s Guide

5-263

Data Block Descriptions O-V

Chapter 5

3

SY

RS

Normal stress in y

4

SZ

RS

Normal stress in z

5

SXZ

RS

Shear stress in xz

6

SMAX

RS

Von Mises stress

TCODE,7=1

Real / Imaginary

2

SXR

RS

Normal stress in x – real part

3

SXI

RS

Normal stress in x – imaginary part

4

SYR

RS

Normal stress in y – real part

5

SYI

RS

Normal stress in y – imaginary part

6

SZR

RS

Normal stress in z – real part

7

SZI

RS

Normal stress in z – imaginary part

8

SXYR

RS

Shear stress in xz – real part

9

SXYI

RS

Shear stress in xz – imaginary part

End TCODE,7 End SCODE,6 ELTYPE =276

Quadrilateral plane stress (CPLSTS4) – Center and Corners

SCODE,6=0

Strain

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EX

RS

Normal strain in x

5

EY

RS

Normal strain in y

6

EZ

RS

Normal strain in z

7

EXZ

RS

Shear strain in xz

8

EMAX

RS

Von Mises strain

Words 3 through 8 repeat 5 times TCODE,7=1

5-264

DMAP Programmer’s Guide

Real / Imaginary

Data Block Descriptions O-V

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EXR

RS

Normal strain in x – real part

5

EXI

RS

Normal strain in x – imaginary part

6

EYR

RS

Normal strain in y – real part

7

EYI

RS

Normal strain in y – imaginary part

8

EZR

RS

Normal strain in z – real part

9

EZI

RS

Normal strain in z – imaginary part

10

EXZR

RS

Shear strain in xz – real part

11

EXZI

RS

Shear strain in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

SMAX

RS

Von Mises stress

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SXR

RS

Normal stress in x – real part

5

SXI

RS

Normal stress in x – imaginary part

DMAP Programmer’s Guide

5-265

Data Block Descriptions O-V

Chapter 5

6

SYR

RS

Normal stress in y – real part

7

SYI

RS

Normal stress in y – imaginary part

8

SZR

RS

Normal stress in z – real part

9

SZI

RS

Normal stress in z – imaginary part

10

SXZR

RS

Shear stress in xz – real part

11

SXZI

RS

Shear stress in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 End SCODE,6 ELTYPE =277

Triangle plane stress (CPLSTS6) – Center and Corners

SCODE,6=0

Strain

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EX

RS

Normal strain in x

5

EY

RS

Normal strain in y

6

EZ

RS

Normal strain in z

7

EXZ

RS

Shear strain in xz

8

EMAX

RS

Von Mises strain

Words 3 through 8 repeat 4 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EXR

RS

Normal strain in x – real part

5

EXI

RS

Normal strain in x – imaginary part

6

EYR

RS

Normal strain in y – real part

7

EYI

RS

Normal strain in y – imaginary part

5-266

DMAP Programmer’s Guide

Data Block Descriptions O-V

8

EZR

RS

Normal strain in z – real part

9

EZI

RS

Normal strain in z – imaginary part

10

EXZR

RS

Shear strain in xz – real part

11

EXZI

RS

Shear strain in xz – imaginary part

Words 3 through 11 repeat 4 times End TCODE,7 SCODE,6=1

Stress

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

SMAX

RS

Von Mises stress

Words 3 through 8 repeat 4 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SXR

RS

Normal stress in x – real part

5

SXI

RS

Normal stress in x – imaginary part

6

SYR

RS

Normal stress in y – real part

7

SYI

RS

Normal stress in y – imaginary part

8

SZR

RS

Normal stress in z – real part

9

SZI

RS

Normal stress in z – imaginary part

10

SXZR

RS

Shear stress in xz – real part

11

SXZI

RS

Shear stress in xz – imaginary part

DMAP Programmer’s Guide

5-267

Data Block Descriptions O-V

Chapter 5

Words 3 through 11 repeat 4 times End TCODE,7 End SCODE,6 ELTYPE =278

Quadrilateral plane stress (CPLSTS8) – Center and Corners

SCODE,6=0

Strain

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EX

RS

Normal strain in x

5

EY

RS

Normal strain in y

6

EZ

RS

Normal strain in z

7

EXZ

RS

Shear strain in xz

8

EMAX

RS

Von Mises strain

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

EXR

RS

Normal strain in x – real part

5

EXI

RS

Normal strain in x – imaginary part

6

EYR

RS

Normal strain in y – real part

7

EYI

RS

Normal strain in y – imaginary part

8

EZR

RS

Normal strain in z – real part

9

EZI

RS

Normal strain in z – imaginary part

10

EXZR

RS

Shear strain in xz – real part

11

EXZI

RS

Shear strain in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7

5-268

DMAP Programmer’s Guide

Data Block Descriptions O-V

SCODE,6=1

Stress

TCODE,7=0

Real

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

SMAX

RS

Von Mises stress

Words 3 through 8 repeat 5 times TCODE,7=1

Real / Imaginary

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SXR

RS

Normal stress in x – real part

5

SXI

RS

Normal stress in x – imaginary part

6

SYR

RS

Normal stress in y – real part

7

SYI

RS

Normal stress in y – imaginary part

8

SZR

RS

Normal stress in z – real part

9

SZI

RS

Normal stress in z – imaginary part

10

SXZR

RS

Shear stress in xz – real part

11

SXZI

RS

Shear stress in xz – imaginary part

Words 3 through 11 repeat 5 times End TCODE,7 End SCODE,6 ELTYPE =281

Triangle plane strain (CPLSTN3) – Nonlinear format – Center

2

SX

RS

Normal stress in x

3

SY

RS

Normal stress in y

DMAP Programmer’s Guide

5-269

Data Block Descriptions O-V

Chapter 5

4

SZ

RS

Normal stress in z

5

SXZ

RS

Shear stress in xz

6

ES

RS

Equivalent stress

7

EPS

RS

Effective plastic/inelastic strain

8

ECS

RS

Effective creep strain

9

EX

RS

Strain in x

10

EY

RS

Strain in y

11

EZ

RS

Strain in z

12

ETXZ

RS

Shear strain in xz

ELTYPE =283

Triangle plane strain (CPLSTN6) – Nonlinear format – Center and Corners

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

ES

RS

Equivalent stress

9

EPS

RS

Effective plastic/inelastic strain

10

ECS

RS

Effective creep strain

11

EX

RS

Strain in x

12

EY

RS

Strain in y

13

EZ

RS

Strain in z

14

ETXZ

RS

Shear strain in xz

Words 3 through 14 repeat 4 times ELTYPE =284

5-270

DMAP Programmer’s Guide

Quadrilateral plane strain (CPLSTN8) – Nonlinear format – Center and Corners

Data Block Descriptions O-V

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

ES

RS

Equivalent stress

9

EPS

RS

Effective plastic/inelastic strain

10

ECS

RS

Effective creep strain

11

EX

RS

Strain in x

12

EY

RS

Strain in y

13

EZ

RS

Strain in z

14

ETXZ

RS

Shear strain in xz

Words 3 through 14 repeat 5 times ELTYPE =285

Triangle plane stress (CPLSTS3) – Nonlinear format – Center

2

SX

RS

Normal stress in x

3

SY

RS

Normal stress in y

4

SZ

RS

Normal stress in z

5

SXZ

RS

Shear stress in xz

6

ES

RS

Equivalent stress

7

EPS

RS

Effective plastic/inelastic strain

8

ECS

RS

Effective creep strain

9

EX

RS

Strain in x

10

EY

RS

Strain in y

11

EZ

RS

Strain in z

12

ETXZ

RS

Shear strain in xz

DMAP Programmer’s Guide

5-271

Data Block Descriptions O-V

Chapter 5

ELTYPE =287

Triangle plane stress (CPLSTS6) – Nonlinear format – Center and Corners

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

ES

RS

Equivalent stress

9

EPS

RS

Effective plastic/inelastic strain

10

ECS

RS

Effective creep strain

11

EX

RS

Strain in x

12

EY

RS

Strain in y

13

EZ

RS

Strain in z

14

ETXZ

RS

Shear strain in xz

Words 3 through 14 repeat 4 times ELTYPE =288

Quadrilateral plane stress (CPLSTS8) – Nonlinear format – Center and Corners

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

ES

RS

Equivalent stress

9

EPS

RS

Effective plastic/inelastic strain

10

ECS

RS

Effective creep strain

11

EX

RS

Strain in x

5-272

DMAP Programmer’s Guide

Data Block Descriptions O-V

12

EY

RS

Strain in y

13

EZ

RS

Strain in z

14

ETXZ

RS

Shear strain in xz

Words 3 through 14 repeat 5 times ELTYPE =289

Quadrilateral plane strain (CPLSTN4) – Nonlinear format – Center and Corners

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

ES

RS

Equivalent stress

9

EPS

RS

Effective plastic/inelastic strain

10

ECS

RS

Effective creep strain

11

EX

RS

Strain in x

12

EY

RS

Strain in y

13

EZ

RS

Strain in z

14

ETXZ

RS

Shear strain in xz

Words 3 through 14 repeat 5 times ELTYPE =290

Quadrilateral plane stress (CPLSTS4) – Nonlinear format – Center and Corners

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

DMAP Programmer’s Guide

5-273

Data Block Descriptions O-V

Chapter 5

7

SXZ

RS

Shear stress in xz

8

ES

RS

Equivalent stress

9

EPS

RS

Effective plastic/inelastic strain

10

ECS

RS

Effective creep strain

11

EX

RS

Strain in x

12

EY

RS

Strain in y

13

EZ

RS

Strain in z

14

ETXZ

RS

Shear strain in xz

Words 3 through 14 repeat 5 times ELTYPE =291

Triangle plane strain (CPLSTN3) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 3 times ELTYPE =292

Quadrilateral plane strain (CPLSTN4) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

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4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 4 times ELTYPE =293

Triangle plane strain (CPLSTN6) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 3 times

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Chapter 5

ELTYPE =294

Quadrilateral plane strain (CPLSTN8) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 4 times ELTYPE =295

Triangle plane stress (CPLSTS3) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

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13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 3 times ELTYPE =296

Quadrilateral plane stress (CPLSTS4) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 4 times ELTYPE =297

Triangle plane stress (CPLSTS6) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

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Chapter 5

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 3 times ELTYPE =298

Quadrilateral plane stress (CPLSTS8) – Hyperelastic - Grid

2

TERM

CHAR4

“GRID”

3

ID

I

Point ID

4

SX

RS

Normal stress in x

5

SY

RS

Normal stress in y

6

SZ

RS

Normal stress in z

7

SXZ

RS

Shear stress in xz

8

PRESSURE

RS

Pressure

9

VOLSTR

RS

Volume strain

10

EX

RS

Strain in x

11

EY

RS

Strain in y

12

EZ

RS

Strain in z

13

ETXZ

RS

Shear strain in xz

Words 3 through 13 repeat 4 times Name

Word

Type

Description

Type

Description

End ELTYPE

Record - TRAILER Word 1

5-278

Name UNDEF(6 )

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None

Data Block Descriptions O-V

Notes: 1.

For CBEAM (2) Item codes are given for end A. Addition of the quantity (K-1) 10 to the item code points to the same information for other stations, where K is the station number. K=11 for end B and 2-10 for intermediate stations.

2. For CTRIA6 (53) The stresses are repeated for each of the stress points within each element. For CHEX8 there are 9 stress points for each element. For CHEX20 there are 9 plus (the number of nondeleted mid-side nodes) stress points for each element. 3. For QUAD8 (64) For corner grids, real , add 17I to items 3 through 19, where I = 1,2,3,4 (87 total words). For corner grids, real/imaginary add 15I to items 3 through 19, where I = 1,2,3,4 (77 total words).

5.10 OESMC Table of modal contributions of element stresses. For all analysis types (real and complex), and SORT1 and SORT2 formats.

Record 0 - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

MCODE

I

Modal contributions code: 1=absolute, 2=normalized

4

SUBCASE

I

Subcase number

5

EICODE

I

Element item code (1000*element ID + item code)

TCODE,1 =1

Sort 1

ACODE,4 = 05

Frequency

6

RS

FREQ

Frequency (Hz)

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Chapter 5

Name

Word 7

UNDEF

Type

Description

None

ACODE,4 =06

Transient

6

TIME

RS

7

UNDEF

None

Time step

ACODE,4 =09

Complex Eigenvalues

6

EIGR

RS

Eigenvalue – real part

7

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 TCODE,1 =02

Sort 2

6

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

7

MFREQ

RS

Modal frequency (Hz)

End TCODE,1

8

UNDEF

None

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 - DATA Name

Word

Type

Description

TCODE,1 =01

Sort 1

1

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

2

MFREQ

RS

Modal frequency (Hz)

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Name

Word TCODE,1 =02

Type

Description

Sort 2

ACODE,4 =05 1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

ACODE,4 =06 1

TIME

RS

2

UNDEF

None

Time step

ACODE,4 =09 1

EIGR

RS

Eigenvalue – real part

2

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 End TCODE,1 TCODE,7 = 0 or 2

Real

3

RS

MC

TCODE,7 =1

Modal contribution

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

End TCODE,7

Record 3 - TRAILER Word

Name

Type

1

NREC

I

2

UNDEF(5 )

None

Description Number of records

5.11 OGF Table of grid point forces

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Chapter 5

Record 0 - HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Block Name

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code; always 19

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

UNDEF

None

Not defined

ACODE,4=0 5

ACODE,4=01

Statics

5

None

UNDEF

See word 8

ACODE,4=02

Real Eigenvalues

5

I

MODE

Mode Number

ACODE,4=03

Differential Stiffness 0

5

None

UNDEF

See word 8

ACODE,4=04

Differential Stiffness 1

5

None

UNDEF

ACODE,4=05

Frequency

5

RS

FREQ

ACODE,4=06

Transient

5

RS

TIME

See word 8

Frequency

Time step

ACODE,4=07

Buckling 0 (Pre-buckling)

5

None

UNDEF

See word 8

ACODE,4=08

Buckling 1 (Post-buckling)

5

I

5-282

MODE

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Mode number

Data Block Descriptions O-V

Name

Word

Type

Description

ACODE,4=09

Complex Eigenvalues

5

I

MODE

Mode number

ACODE,4=10

Nonlinear Statics (Sol 106)

5

RS

LOADFAC

Load factor

ACODE,4=11

Geometric Nonlinear Statics

5

None

UNDEF

ACODE,4=12

CONTRAN

5

RS

TIME

See word 8

Time step

End ACODE,4 6

UNDEF(2)

None

8

LOADSET

I

Load set or zero

9

FCODE

I

Format Code

10

NUMWDE(C)

I

Number of words per entry in DATA record

11

UNDEF(2)

None

13

SETID

I

Set identification number

14

EIGENR

RS

Natural eigenvalue – real part

15

EIGENI

RS

Natural eigenvalue – imaginary part

16

FREQ

RS

Natural frequency

17

UNDEF(34)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 - DATA Word

Name

TCODE,1 =1 1

Type

Description

Sort 1 EKEY

I

Device code + 10* Point identification number

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Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,1 =02

Type

Description

Sort 2 - Swap with word 5 of IDENT

ACODE,4 =0 1

UNDEF

None

Not defined

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

RS

Frequency

RS

Time step

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

RS

Frequency or Time step

I

Device code + 10* Point identification number

ACODE,4 =01 1

EKEY

ACODE,4 =02 1

EKEY

ACODE,4 =03 1

EKEY

ACODE,4 =04 1

EKEY

ACODE,4 =05 1

FREQ

ACODE,4 =06 1

TIME

ACODE,4 =07 1

EKEY

ACODE,4 =08 1

EKEY

ACODE,4 =09 1

EKEY

ACODE,4 =10 1

FQTS

ACODE,4 =11 1

EKEY

ACODE,4 =12

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Name

Word 1

EKEY

Type

Description

I

Device code + 10* Point ID

Element identification number if element force; otherwise zero

End ACODE,4 End TCODE,1 2

EID

I

3

ELNAME(2)

CHAR4

NUMWDE =10

real

5

F1

RS

Force in displacement coordinate system direction 1

6

F2

RS

Force in displacement coordinate system direction 2

7

F3

RS

Force in displacement coordinate system direction 3

8

M1

RS

Moment in displacement coordinate system direction 1

9

M2

RS

Moment in displacement coordinate system direction 2

10

M3

RS

Moment in displacement coordinate system direction 3

NUMWDE =16

complex

5

F1R

RS

6

F2R

RS

7

F3R

RS

8

M1R

RS

9

M2R

RS

10

M3R

RS

11

F1I

RS

12

F2I

RS

13

F3I

RS

14

M1I

RS

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Data Block Descriptions O-V

Chapter 5

Name

Word 15

M2I

RS

16

M3I

RS

Type

Description

Type

Description

End NUMWDE

Record 3 - TRAILER Name

Word 1

WORD1

I

2

UNDEF(5 )

None

Number of output line entries

Notes: 1. Records repeat for each subcase having any output requests. 2. Device code: 1 = print 2 = plot 4 = punch 5 = print, and punch, and so on 3. Approach code: 1 = statics 2 = reigen 3 = ds0 4 = ds1 5 = freq 6 = bkl0 7 = bkl1 8 = ceigen 9 = pla

5.12 OGK Output gasket element results For SOL 601,106 and SOL 601,129.

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Data Block Descriptions O-V

Record - HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data Block Name, for example, OGK1

Record - IDENT Name

Word

Type

Description

1

ACODE

I

Device code + 10*Approach code

2

TCODE

I

Table code; 61

3

ELTYPE

I

Element Type (for example, linear hexa=67, linear penta=68, nonlinear penta=91, hexa=93, ....)

4

SUBCASE

I

5

TIME

RS

6-7

UNDEF

None

8

LOADSET

I

Load Set or Zero

9

FCODE

I

1

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF

None

12

PID

I

11-50

UNDEF

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Time Step

Physical Property ID

Record - DATA Name

Word

Type

Description

1

EKEY

I

Device code + 10* Element identification number

2

GP

RS

Gasket pressure

3

GC

RS

Gasket closure

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

4

GPC

RS

Gasket plastic closure

5

YS

RS

Gasket yield stress

6

GS

I

Gasket status. See Remark 2.

Repeat word 1-6 for each element.

Record – TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

Notes: 1. Gasket element results are elemental based results. 2. Gasket status is assigned to the following integer values: Integer – Status 1 – Open 2 – Closed 3 – Sealed 4 – Leaked 5 – Crushed

5.13 OGS Table of grid point stresses/strains or discontinuities SORT1, SORT2, and real formats only.

Record 0 - HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

Month, day, year, 0, 1

Word 3 repeats until End of Record

Record 1 - IDENT Word 1

5-288

Name ACODE(C)

DMAP Programmer’s Guide

Type I

Description Device code + 10*Approach code

Data Block Descriptions O-V

Name

Word

Type

Description

2

TCODE(C)

I

Table type code

3

ID

I

Surface or volume identification number

4

SUBCASE

I

Subcase or mode identification number

ACODE =01

Statics

5

LSDVMN

I

6

UNDEF

None

ACODE =02

Load set number

Real Eigenvalues

5

MODE

I

Mode Number

6

EIGN

RS

Eigenvalue

Transient

ACODE =06 5

TIME

RS

6

UNDEF

None

ACODE =10

Time Step

Nonlinear Statics

5

LOADSTEP

RS

6

UNDEF

None

7

UNDEF

None

8

REFID

I

Reference coordinate system identification number

9

FCODE

I

Format code

10

NUMWDE

I

Number of words per entry in DATA record

11

SCODE

I

Stress/Strain code

12

OCOORD

I

Output coordinate system code

13

AXIS

I

Axis specification code

14

NORMAL

I

Normal Specification code

15

UNDEF(36 )

None

51

TITLE(32)

CHAR4

Load Step

End ACODE

Title

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Chapter 5

Name

Word

Type

Description

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 – DATA Name

Word TCODE =26

Type

Description

Surface

1

EKEY

I

10*Grid point identification number + Device code

2

ID

I

Element identification number

3

FIBRE

CHAR4

Fibre

4

NX

RS

Normal in x

5

NY

RS

Normal in y

6

TXY

RS

Shear in xy

7

A

RS

Angle

8

MJRP

RS

Major principal

9

MNRP

RS

Minor principal

10

TMAX

RS

Maximum shear

11

HVM

RS

Hency-von Mises

TCODE =27

Volume with direct

1

EKEY

I

10*Grid point identification number + Device Code

2

NX

RS

Normal in x

3

NY

RS

Normal in y

4

NZ

RS

Normal in z

5

TXY

RS

Shear in xy

6

TYZ

RS

Shear in yz

7

TZX

RS

Shear in zx

8

PR

RS

Mean pressure

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Data Block Descriptions O-V

Name

Word 9

HVM

TCODE =28

Type RS

Description Hencky-von Mises or Octahedral

Volume with principal

1

EKEY

I

10*Grid point identification number + Device code

2

LXA

RS

Direction cosine from x to a

3

LXB

RS

Direction cosine from x to b

4

LXC

RS

Direction cosine from x to c

5

LYA

RS

Direction cosine from y to a

6

LYB

RS

Direction cosine from y to b

7

LYC

RS

Direction cosine from y to c

8

LZA

RS

Direction cosine from z to a

9

LZB

RS

Direction cosine from z to b

10

LZC

RS

Direction cosine from z to c

11

SA

RS

Principal in a

12

SB

RS

Principal in b

13

SC

RS

Principal in c

14

EPR

RS

Mean pressure

15

EHVM

RS

Hencky-von Mises or Octahedral

TCODE =29

Element discontinuities for surface

1

EKEY

I

10*Grid point identification number + Device code

2

ELTYPE(2)

CHAR4

Element type

4

FIBRE

CHAR4

Fibre

5

NX

RS

Normal in x

6

NY

RS

Normal in y

7

TXY

RS

Shear in xy

8

MJPR

RS

Major principal

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Chapter 5

Data Block Descriptions O-V

Name

Word

Type

Description

9

MNPR

RS

Minor principal

10

TMAX

RS

Maximum shear

11

HVM

RS

Hencky-von Mises

12

ERR

RS

Error estimate

Name

Word TCODE =30

Type

Description

Element discontinuities for volumes with direct

1

EKEY

I

10*Element identification number + Device code

2

ELTYPE(2)

CHAR4

Element type

4

NX

RS

Normal in x

5

NY

RS

Normal in y

6

NZ

RS

Normal in z

7

SXY

RS

Shear in xy

8

SYZ

RS

Shear in yz

9

SZX

RS

Shear in zx

10

PR

RS

Mean pressure

11

HVM

RS

Hencky-von Mises

12

ERR

RS

Error estimate

TCODE =31

Element discontinuities for volumes with principal

1

EKEY

I

10*Element identification number + Device code

2

ELTYPE(2)

CHAR4

Element type

4

SA

RS

Principal in a

5

SB

RS

Principal in b

6

SC

RS

Principal in c

7

MP

RS

Mean pressure

8

HVM

RS

Hencky-von Mises or Octahedral

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Data Block Descriptions O-V

Name

Word 9

ERR

TCODE =32

Type RS

Description Error estimate

Grid point discontinuities for surface

1

EKEY

I

10*Grid point identification number + Device code

2

FIBRE

CHAR4

Fibre

3

NX

RS

Normal in x

4

NY

RS

Normal in y

5

NXY

RS

Shear in xy

6

MJPR

RS

Major principal

7

MNPR

RS

Minor principal

8

TMAX

RS

Maximum shear

9

HVM

RS

Hencky-von Mises

10

ERR

RS

Error estimate

TCODE =33

Grid point discontinuities for volumes with direct

1

EKEY

I

10*Grid point identification number + Device Code

2

NX

RS

Normal in x

3

NY

RS

Normal in y

4

NZ

RS

Normal in z

5

TXY

RS

Shear in xy

6

TYZ

RS

Shear in yz

7

TZX

RS

Shear in zx

8

PR

RS

Mean pressure

9

HVM

RS

Hencky-von Mises or Octahedral

10

ERR

RS

Error estimate

TCODE =34 1

Grid point discontinuities for volumes with principal EKEY

I

10*Grid point identification number + Device Code

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

SA

RS

Principal in a

3

SB

RS

Principal in b

4

SC

RS

Principal in c

5

PR

RS

Mean pressure

6

HVM

RS

Hencky-von Mises or Octahedral

7

ERR

RS

Error estimate

TCODE =35

Grid point stresses for surfaces with plane strain

1

EKEY

I

10*Grid point identification number and Grid Code

2

NX

RS

Normal in x

3

NY

RS

Normal in y

4

NZ

RS

Normal in z (always -1)

5

TXY

RS

Shear in xy

6

PR

RS

Mean pressure (always -1)

End TCODE,2 End TABLE

Record 3 – TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

Notes: 1. Records repeat for each surface or volume. 2. Record 2 is the same format for stress (SCODE=0) or strain (SCODE=1). 3. Format Code ’1’ implies real. 4. Output coordinate system code 1 = Surface or CID for 3D 2 = Element 3 = Basic (3D only)

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5. Axis specification code (for surfaces only) 1 = X Axis 2 = Y Axis 3 = Z Axis 6. Normal Specification code (for surfaces only ) 1 = Radius vector 2 = X Axis 3 = Y Axis 4 = Z Axis 5 = –X Axis 6 = –Y Axis 7 = –Z Axis 8 = –Radius vector

5.14 OMECON Table of constant total modal energies.

Record 0 - HEADER Word

Name

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

6

UNDEF(2)

None

Description Block Name

Record 1 - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

5

MODE/FREQ

I/RS

6

UNDEF(3)

None

9

FORM

I

Description Device code + 10*Mode number (SORT1) / Frequency in Hz (SORT2)

Form of data: =1 For real/imaginary =3 For magnitude/phase

10

NUMWDE(C)

I

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Length of entries in RECORD=DATA

Record 2 - DATA Name

Word

Type

Description

TCODE=1042

Sort 1

1

FREQ

RS

Frequency in Hz.

2

TYPE

I

Always 4 for ‘modal’.

3

REAL or MAG

RS

Real part of energy value (FORM=1) or magnitude of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

TCODE=3042

Sort 2

1

EKEY

I

Device code + 10*mode number

2

TYPE

I

Always 4 for ‘modal’

3

REAL or MAG

RS

Real part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

5-296

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Data Block Descriptions O-V

Record 3 - TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of output line entries

Notes: 1. Four words of data in record 2 repeats for each mode (SORT2) or each frequency (SORT1). 2. Records 1 and 2 repeat for each frequency (SORT2) or each mode (SORT1). 3. Device code: 1 = print 4 = punch 5 = print and punch 4. Approach code: 5= freq 5. Table code: 1042 = SORT1 complex 3042 = SORT2 complex Mode number = 0 implies summation results (summation of all modal energy values for a frequency)

5.15 OMEOSC Table of oscillating total modal energies.

Record 0 - HEADER Word

Name

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

6

UNDEF(2)

None

Description Block Name

DMAP Programmer’s Guide

5-297

Data Block Descriptions O-V

Chapter 5

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

5

MODE/FREQ

I/RS

Device code + 10*Mode number (SORT1) / Frequency in Hz (SORT2)

6

UNDEF(3)

None

9

FORM

I

Form of data: =1 For real/imaginary =3 For magnitude/phase

10

NUMWDE(C)

I

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Length of entries in RECORD=DATA

Record 2 - DATA Name

Word

Type

Description

TCODE=1043

Sort 1

1

FREQ

RS

Frequency in Hz.

2

TYPE

I

Always 4 for ‘modal’.

3

REAL or MAG

RS

Real part of energy value (FORM=1) or magnitude of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

TCODE=3043

Sort 2

1

I

5-298

EKEY

DMAP Programmer’s Guide

Device code + 10*mode number

Data Block Descriptions O-V

Name

Word

Type

Description

2

TYPE

I

Always 4 for ‘modal’

3

REAL or MAG

RS

Real part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

Record 3 - TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of output line entries

Notes: 1. Four words of data in record 2 repeats for each mode (SORT2) or each frequency (SORT1). 2. Records 1 and 2 repeat for each frequency (SORT2) or each mode (SORT1). 3. Device code: 1 = print 4 = punch 5 = print and punch 4. Approach code: 5= freq 5. Table code: 1043 = SORT1 complex 3043 = SORT2 complex Mode number = 0 implies summation results (summation of all modal energy values for a frequency)

5.16 OMKEC Table of constant modal kinetic energies.

DMAP Programmer’s Guide

5-299

Data Block Descriptions O-V

Chapter 5

Record 0 - HEADER Name

Word

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

6

UNDEF(2)

None

Description Block Name

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

5

MODE/FREQ

I/RS

Device code + 10*Mode number (SORT1) / Frequency in Hz (SORT2)

6

UNDEF(3)

None

9

FORM

I

Form of data: =1 For real/imaginary =3 For magnitude/phase

10

NUMWDE(C)

I

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Length of entries in RECORD=DATA

Record 2 - DATA Word

Name

TCODE=1040

5-300

DMAP Programmer’s Guide

Type Sort 1

Description

Data Block Descriptions O-V

Name

Word

Type

Description

1

FREQ

RS

Frequency in Hz.

2

TYPE

I

Always 4 for ‘modal’.

3

REAL or MAG

RS

Real part of energy value (FORM=1) or magnitude of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

TCODE=3040

Sort 2

1

EKEY

I

Device code + 10*mode number

2

TYPE

I

Always 4 for ‘modal’

3

REAL or MAG

RS

Real part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

Record 3 - TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of output line entries

Notes: 1. Four words of data in record 2 repeats for each mode (SORT2) or each frequency (SORT1). 2. Records 1 and 2 repeat for each frequency (SORT2) or each mode (SORT1). 3. Device code: 1 = print 4 = punch 5 = print and punch 4. Approach code: 5= freq 5. Table code: 1040 = SORT1 complex 3040 = SORT2 complex

DMAP Programmer’s Guide

5-301

Chapter 5

Data Block Descriptions O-V

Mode number = 0 implies summation results (summation of all modal energy values for a frequency)

5.17 OMKEO Table of oscillating modal kinetic energies.

Record 0 - HEADER Word

Name

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

6

UNDEF(2)

None

Description Block Name

Record 1 - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

5

MODE/FREQ

I/RS

Device code + 10*Mode number (SORT1) / Frequency in Hz (SORT2)

6

UNDEF(3)

None

9

FORM

I

Form of data: =1 For real/imaginary =3 For magnitude/phase

10

NUMWDE(C)

I

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

5-302

DMAP Programmer’s Guide

Length of entries in RECORD=DATA

Data Block Descriptions O-V

Name

Word 115

Type CHAR4

LABEL(32)

Description Label

Record 2 - DATA Name

Word

Type

Description

TCODE=1041

Sort 1

1

FREQ

RS

Frequency in Hz.

2

TYPE

I

Always 4 for ‘modal’.

3

REAL or MAG

RS

Real part of energy value (FORM=1) or magnitude of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

TCODE=3041

Sort 2

1

EKEY

I

Device code + 10*mode number

2

TYPE

I

Always 4 for ‘modal’

3

REAL or MAG

RS

Real part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

Record 3 - TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of output line entries

Notes: 1. Four words of data in record 2 repeats for each mode (SORT2) or each frequency (SORT1). 2. Records 1 and 2 repeat for each frequency (SORT2) or each mode (SORT1). 3. Device code: 1 = print 4 = punch

DMAP Programmer’s Guide

5-303

Data Block Descriptions O-V

Chapter 5

5 = print and punch 4. Approach code: 5= freq 5. Table code: 1041 = SORT1 complex 3041 = SORT2 complex Mode number = 0 implies summation results (summation of all modal energy values for a frequency)

5.18 OMSEC Table of constant modal strain energies.

Record 0 - HEADER Word

Name

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

6

UNDEF(2)

None

Description Block Name

Record 1 - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

5

MODE/FREQ

I/RS

Device code + 10*Mode number (SORT1) / Frequency in Hz (SORT2)

6

UNDEF(3)

None

5-304

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word 9

Type I

FORM

Description Form of data: =1 For real/imaginary =3 For magnitude/phase

10

NUMWDE(C)

I

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Length of entries in RECORD=DATA

Record 2 - DATA Name

Word

Type

Description

TCODE=1038

Sort 1

1

FREQ

RS

Frequency in Hz.

2

TYPE

I

Always 4 for ‘modal’.

3

REAL or MAG

RS

Real part of energy value (FORM=1) or magnitude of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

TCODE=3038

Sort 2

1

EKEY

I

Device code + 10*mode number

2

TYPE

I

Always 4 for ‘modal’

3

REAL or MAG

RS

Real part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

Record 3 - TRAILER Word 1

Name WORD1

Type I

Description Number of output line entries

DMAP Programmer’s Guide

5-305

Data Block Descriptions O-V

Chapter 5

Name

Word 2

UNDEF(5 )

Type

Description

None

Notes: 1. Four words of data in record 2 repeats for each mode (SORT2) or each frequency (SORT1). 2. Records 1 and 2 repeat for each frequency (SORT2) or each mode (SORT1). 3. Device code: 1 = print 4 = punch 5 = print and punch 4. Approach code: 5= freq 5. Table code: 1038 = SORT1 complex 3038 = SORT2 complex 6. Mode number = 0 implies summation results (summation of all modal energy values for a frequency)

5.19 OMSEO Table of oscillating modal strain energies.

Record 0 - HEADER Word

Name

Type

1

NAME(2)

CHAR4

3

MONTH

I

4

DAY

I

5

YEAR

I

6

UNDEF(2)

None

5-306

DMAP Programmer’s Guide

Description Block Name

Data Block Descriptions O-V

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach code

2

TCODE(C)

I

Table code

3

UNDEF

None

4

SUBCASE

I

Subcase identification number

5

MODE/FREQ

I/RS

Device code + 10*Mode number (SORT1) / Frequency in Hz (SORT2)

6

UNDEF(3)

None

9

FORM

I

Form of data: =1 For real/imaginary =3 For magnitude/phase

10

NUMWDE(C)

I

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Length of entries in RECORD=DATA

Record 2 - DATA Name

Word

Type

Description

TCODE=1039

Sort 1

1

FREQ

RS

Frequency in Hz.

2

TYPE

I

Always 4 for ‘modal’.

3

REAL or MAG

RS

Real part of energy value (FORM=1) or magnitude of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

TCODE=3039

Sort 2

1

I

EKEY

Device code + 10*mode number

DMAP Programmer’s Guide

5-307

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

2

TYPE

I

Always 4 for ‘modal’

3

REAL or MAG

RS

Real part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

4

IMAG or PHASE

RS

Imaginary part of energy value (FORM=1) or phase (degrees) of energy value (FORM=3)

Record 3 - TRAILER Name

Word

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of output line entries

Notes: 1. Four words of data in record 2 repeats for each mode (SORT2) or each frequency (SORT1). 2. Records 1 and 2 repeat for each frequency (SORT2) or each mode (SORT1). 3. Device code: 1 = print 4 = punch 5 = print and punch 4. Approach code: 5= freq 5. Table code: 1039 = SORT1 complex 3039 = SORT2 complex 6. Mode number = 0 implies summation results (summation of all modal energy values for a frequency)

5.20 OPG Table of applied loads For all analysis types (real and complex), and SORT1 and SORT2 formats.

5-308

DMAP Programmer’s Guide

Data Block Descriptions O-V

Record – HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record – IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

UNDEF

None

4

SUBCASE

I

TCODE =1

Sort 1

ACODE =01

Statics

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE =02

Subcase or Random identification number

Load set number

Real Eigenvalues

5

MODE

I

Mode Number

6

EIGN

RS

Eigenvalue

7

MODECYCL

RS

Mode or Cycle

ACODE =03

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE =04

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

Load set number

Frequency

ACODE =05 5

Load set number

FREQ

RS

Frequency

DMAP Programmer’s Guide

5-309

Chapter 5

Data Block Descriptions O-V

Name

Word

Type

6

UNDEF

None

7

RANDOM ID

I

Description

Random identification number

Transient

ACODE =06 5

TIME

RS

6

UNDEF(2 )

None

ACODE =07

Time Step

Buckling Phase 0 (Pre-buckling)

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE =08

Load set

Buckling Phase 1 (Post-buckling)

5

LSDVMN

I

Mode Number

6

EIGR

RS

Eigenvalue

7

RANDOM ID

I

Random identification number

ACODE =09

Complex Eigenvalues

5

MODE

I

Mode

6

EIGR

RS

Eigenvalue (real)

7

EIGI

RS

Eigenvalue (imaginary)

ACODE =10

Nonlinear statics

5

LFTSFQ

RS

6

UNDEF(2 )

None

ACODE =11

Old geometric nonlinear statics

5

LSDVMN

I

6

UNDEF

None

7

RANDOM ID

I

ACODE =12

Load set

Random identification number

CONTRAN ? (Can appear as ACODE=6)

5

TIME

RS

6

UNDEF(2 )

None

5-310

Load step

DMAP Programmer’s Guide

Time

Data Block Descriptions O-V

Name

Word

Type

Description

End ACODE TCODE =02

Sort 2

5

LSDVMN

I

6

UNDEF(2 )

None

Load set, Mode Number

End TCODE 8

RCODE

I

Random code ID number.

9

FCODE(C)

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(12 )

None

23

THERMAL

I

24

UNDEF(27 )

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

1 for heat transfer and 0 otherwise

Record – DATA Word

Name

TCODE =1 1

Type

Description

Sort 1 EKEY

TCODE =02

I

Device code + 10* Point identification number

Sort 2 - Swap with word 5 of IDENT

ACODE =01 1

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

ACODE =02 1 ACODE =03 1 ACODE =04

DMAP Programmer’s Guide

5-311

Data Block Descriptions O-V

Chapter 5

Name

Word 1

Type

Description

EKEY

I

Device code + 10* Point identification number

FREQ

RS

Frequency

TIME

RS

Time step

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

FQTS

RS

Frequency or Time step

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

TYPE

I

Point type: G for grid and S for scalar

ACODE =05 1 ACODE =06 1 ACODE =07 1 ACODE =08 1 ACODE =09 1 ACODE =10 1 ACODE =11 1 ACODE =12 1 End ACODE End TCODE 2

FCODE =0 or 2

Real or Random Response

3

F1

RS

Applied force in direction 1

4

F2

RS

Applied force in direction 2

5

F3

RS

Applied force in direction 3

6

M1

RS

Applied moment in direction 1

7

M2

RS

Applied moment in direction 2

5-312

DMAP Programmer’s Guide

Data Block Descriptions O-V

Word 8

Name M3

Type RS

FCODE =1

Description Applied moment in direction 3

Real/Imaginary

3

F1R

RS

Applied force in direction 1 – Real

4

F2R

RS

Applied force in direction 2 – Real

5

F3R

RS

Applied force in direction 3 – Real

6

M1R

RS

Applied moment in direction 1 – Real

7

M2R

RS

Applied moment in direction 2 – Real

8

M3R

RS

Applied moment in direction 3 – Real

9

F1I

RS

Applied force in direction 1 – Imaginary

10

F2I

RS

Applied force in direction 2 – Imaginary

11

F3I

RS

Applied force in direction 3 – Imaginary

12

M1I

RS

Applied moment in direction 1 – Imaginary

13

M2I

RS

Applied moment in direction 2 – Imaginary

14

M3I

RS

Applied moment in direction 3 – Imaginary

End FCODE

Record – TRAILER Word 1

Name UNDEF(6 )

Type

Description

None

5.21 OPTPRM Table of optimization parameters

Record - HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name

DMAP Programmer’s Guide

5-313

Data Block Descriptions O-V

Chapter 5

Record - PARAMS Name

Word

Type

Description

The PARAMS record of the OPTPRM data block is identical to the DOPTPRM record of the EDOM data block.

Record - TRAILER Name

Word 1

UNDEF(6)

Type

Description

None

5.22 OQG Table of single or multipoint constraint forces. Also contact force results from SOL 101, SOL 601,106, SOL 601,129 and SOL 701. For all analysis types (real and complex), and SORT1 and SORT2 formats. Contact force results are real only.

Record – HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record – IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

UNDEF

None

4

SUBCASE

I

TCODE =1

Sort 1

ACODE =01

Statics

5

5-314

LSDVMN

DMAP Programmer’s Guide

I

Subcase or Random identification number

Load set number

Data Block Descriptions O-V

Word 6

Name UNDEF(2 )

ACODE =02

Type

Description

None Real Eigenvalues

5

MODE

I

Mode Number

6

EIGN

RS

Eigenvalue

7

MODECYCL

RS

Mode or Cycle

ACODE =03

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE =04

Load set number

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

Load set number

Frequency

ACODE =05 5

FREQ

RS

6

UNDEF

None

7

RANDOM ID

I

Frequency

Random identification number

Transient

ACODE =06 5

TIME

RS

6

UNDEF(2 )

None

ACODE =07

Time Step

Buckling Phase 0 (Pre-buckling)

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE =08

Load set

Buckling Phase 1 (Post-buckling)

5

LSDVMN

I

Mode Number

6

EIGR

RS

Eigenvalue

7

RANDID

I

Random ID number

ACODE =09

Complex Eigenvalues

DMAP Programmer’s Guide

5-315

Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

5

MODE

I

Mode

6

EIGR

RS

Eigenvalue (real)

7

EIGI

RS

Eigenvalue (imaginary)

ACODE =10

Nonlinear statics

5

LFTSFQ

RS

6

UNDEF(2 )

None

ACODE =11

Load step or time step

Old geometric nonlinear statics

5

LSDVMN

I

6

UNDEF

None

7

RANDID

I

ACODE =12

Load set

Random ID number

CONTRAN (Can appear as ACODE=6)

5

TIME

RS

6

UNDEF(2 )

None

Time

End ACODE TCODE =02

Sort 2

5

LSDVMN

I

6

UNDEF(2 )

None

Load set, Mode Number

End TCODE 8

RCODE

I

Load set or Random code ID number

9

FCODE(C)

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

MPCFORCE

I

1 for MPCforce output and 0 for SPCforce output

12

UNDEF(11 )

None

23

THERMAL

I

24

UNDEF(27 )

None

51

TITLE(32)

CHAR4

5-316

DMAP Programmer’s Guide

=1 for heat transfer and 0 otherwise

Title

Data Block Descriptions O-V

Name

Word

Type

Description

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record - DATA Word

Name

TCODE =1 1

Type

Description

Sort 1 EKEY

TCODE =02

I

Device code + 10* Point identification number

Sort 2 - Swap with word 5 of IDENT

ACODE =01 1

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

FREQ

RS

Frequency

TIME

RS

Time step

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

ACODE =02 1 ACODE =03 1 ACODE =04 1 ACODE =05 1 ACODE =06 1 ACODE =07 1 ACODE =08 1 ACODE =09 1 ACODE =10

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Chapter 5

Name

Word 1

Type

Description

FQTS

RS

Frequency or Time step

EKEY

I

Device code + 10* Point identification number

EKEY

I

Device code + 10* Point identification number

TYPE

I

Point type: G for grid and S for scalar

ACODE =11 1 ACODE =12 1 End ACODE End TCODE 2

FCODE =0 or 2

Real or Random Response

3

QF1

RS

Constraint force in direction 1

4

QF2

RS

Constraint force in direction 2

5

QF3

RS

Constraint force in direction 3

6

QM1

RS

Constraint moment in direction 1

7

QM2

RS

Constraint moment in direction 2

8

QM3

RS

Constraint moment in direction 3

FCODE =1

Real/Imaginary

3

QF1R

RS

Constraint force in direction 1 – Real

4

QF2R

RS

Constraint force in direction 2 – Real

5

QF3R

RS

Constraint force in direction 3 – Real

6

QM1R

RS

Constraint moment in direction 1 – Real

7

QM2R

RS

Constraint moment in direction 2 – Real

8

QM3R

RS

Constraint moment in direction 3 – Real

9

QF1I

RS

Constraint force in direction 1 – Imaginary

10

QF2I

RS

Constraint force in direction 2 – Imaginary

11

QF3I

RS

Constraint force in direction 3 – Imaginary

12

QM1I

RS

Constraint moment in direction 1 – Imaginary

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Data Block Descriptions O-V

Word

Name

Type

Description

13

QM2I

RS

Constraint moment in direction 2 – Imaginary

14

QM3I

RS

Constraint moment in direction 3 – Imaginary

End FCODE

Data Format when Table Code = 63 (OQG contact force results) 1

EKEY

I

Device code + 10*Point identification number

2

TYPE

I

Point type, Grid or Scalar (always Grid for contact force)

3

QF1

RS

Contact force in direction X (Base C.S.)

4

QF2

RS

Contact force in direction Y (Base C.S.)

5

QF3

RS

Contact force in direction Z (Base C.S.)

6

QM1

RS

Not used

7

QM2

RS

Not used

8

QM2

RS

Not used

Repeat word 1-8 for each grid point.

Data Format when Table Code = 67 (OQG glue force results for SOL 101 (ACODE=1) and SOLs 103 and 105 (ACODE=2)) 1

EKEY

I

Device code + 10*Point identification number

2

TYPE

I

Point type, Grid or Scalar (always Grid for glue force)

3

QF1

RS

Glue force in direction X (Base C.S.)

4

QF2

RS

Glue force in direction Y (Base C.S.)

5

QF3

RS

Glue force in direction Z (Base C.S.)

6

QM1

RS

Not used

7

QM2

RS

Not used

8

QM2

RS

Not used

Repeat word 1-8 for each grid point.

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Record – TRAILER Name

Word 1

Type

Description

None

UNDEF(6 )

5.23 OQGMC Table of modal contributions of single point constraint forces. For all analysis types (real and complex), and SORT1 and SORT2 formats.

Record 0 - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record 1 - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

MCODE

I

Modal contributions code: 1=absolute, 2=normalized

4

SUBCASE

I

Subcase number

5

DCODE

I

Dof code (10*grid ID + direction)

TCODE,1 =1

Sort 1

ACODE,4 = 05

Frequency

6

FREQ

RS

7

UNDEF

None

ACODE,4 =06

Transient

6

TIME

RS

7

UNDEF

None

5-320

DMAP Programmer’s Guide

Frequency (Hz)

Time step

Data Block Descriptions O-V

Name

Word

Type

Description

ACODE,4 =09

Complex Eigenvalues

6

EIGR

RS

Eigenvalue – real part

7

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 TCODE,1 =02

Sort 2

6

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

7

MFREQ

RS

Modal frequency (Hz)

End TCODE,1

8

UNDEF

None

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record 2 - DATA Name

Word

Type

Description

TCODE,1 =01

Sort 1

1

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

2

MFREQ

RS

Modal frequency (Hz)

TCODE,1 =02

Sort 2

ACODE,4 =05 1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ACODE,4 =06 1

TIME

RS

2

UNDEF

None

Time step

ACODE,4 =09 1

EIGR

RS

Eigenvalue – real part

2

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 End TCODE,1 TCODE,7 = 0 or 2

Real

3

RS

MC

TCODE,7 =1

Modal contribution

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

End TCODE,7

Record 3 - TRAILER Word

Name

Type

1

NREC

I

2

UNDEF(5 )

None

Description Number of records

5.24 OSDISP2 Table of Modal Contributions

Record 0 – HEADER Word 1

5-322

Name NAME(2)

DMAP Programmer’s Guide

Type CHAR4

Description Data block Name

Data Block Descriptions O-V

Record 1 – OSINT Name

Word

Type

1–10

OSDNUM

I

11–50

UNDEF (40)

None

51,52

SOLNM1(2)

Char4

53,54

SOLNM2(2)

Char4

55–144

UNDEF(90)

None

145

INUM

I

146

UNDEF

None

Description

Record 2 - OSNUM Name

Word 1

ISTART

I

2

IVAL

I

3

AVAL

RS

Type

Description

Type

Description

Record 3- Trailer Name

Word 1

UNDEF(6 )

none

Notes: 1. Records 1 and 2 may repeat in order for n number of times followed by the trailer.

5.25 OSHT Output shell element thickness results For SOLs 601/701, Sort 1 only.

Record – HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block Name, e.g. OSHT1

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Data Block Descriptions O-V

Chapter 5

Record – IDENT Name

Word

Type

Description

2

TCODE

I

Table Code, 60

3

ELTYPE

I

Element Type

11–50

UNDEF

None

Record - DATA Word

Name

ELTYPE=88

Type

Description

TRIA3 - Nonlinear

1

EKEY

I

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

THICK

RS

Thickness

Words 3 through 4 repeat 004 times

ELTYPE=90

QUAD4 - Nonlinear

1

EKEY

I

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

THICK

RS

Thickness

Words 3 through 4 repeat 005 times

ELTYPE=240

TRIA6 - Nonlinear

1

EKEY

I

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

THICK

RS

Thickness

Words 3 through 4 repeat 004 times

5-324

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word ELTYPE=241

Type

Description

QUAD8 - Nonlinear

1

EKEY

I

2

TERM

CHAR4

“CEN”

3

GRID

I

Grid identification number; 0 for centroid

4

THICK

RS

Thickness

Words 3 through 4 repeat 005 times

Record – TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

5.26 OSPDS Output contact separation distance results. When SORT1 data is requested, OSPDSI1 stores the initial separation distance, and OSPDS1 stores the final. When SORT2 data is requested, OSPDSI2 and OSPDS2 are written. The separation distance data is output during the statics portion of a solution. For example, a STATSUB being used when running a normal modes solution (SOL 103).

Record - HEADER Name

Word

Type

Description

1-2

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Word 1

Name ACODE(C)

Type I

Description Device code + 10*Approach Code

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word 2

TCODE(C)

Type I

Description Table Code 64 for Initial Separation Distance 65 for Deformed Separation Distance

3

UNDEF

None

4

SUBCASE

I

Subcase

TCODE,1 =1

Sort 1

ACODE,4=01

SOL 101 Linear Statics

5

LSDVMN

I

6

UNDEF(2)

None

Load set number

End ACODE TCODE,1=02 5

Sort 2 EKEY

I

6

UNDEF(2 )

None

8

LSDVMN

I

Load set number

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(1)

None

12

PID

I

13

UNDEF(38)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITLE(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Device code + 10*point identification number

End TCODE

Physical Property ID

Record - DATA Word

Name

TCODE,1 =01

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DMAP Programmer’s Guide

Type Sort 1

Description

Data Block Descriptions O-V

Name

Word 1

Type

EKEY

Description

I

TCODE,1 =02

Device code + 10* Point identification number

Sort 2 - Swap with word 5 of IDENT

ACODE,4 =01 1

EKEY

I

Device code + 10* Point identification number

ACODE,4 =10

601/701 Nonlinear

1

RS

Time step

RS

Contact separation distance

TIME

End ACODE,4 End TCODE,1 2

SDIS

Record - TRAILER Word 1

Name

Type

Description

None

UNDEF(6)

5.27 OSTRMC Table of modal contributions of element strains. For all analysis types (real and complex), and SORT1 and SORT2 formats.

Record 0 - HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record 1 - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

DMAP Programmer’s Guide

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Chapter 5

Name

Word

Type

Description

3

MCODE

I

Modal contributions code: 1=absolute, 2=normalized

4

SUBCASE

I

Subcase number

5

EICODE

I

Element item code (1000*element ID + item code)

TCODE,1 =1

Sort 1

ACODE,4 = 05

Frequency

6

FREQ

RS

7

UNDEF

None

ACODE,4 =06

Transient

6

TIME

RS

7

UNDEF

None

Frequency (Hz)

Time step

ACODE,4 =09

Complex Eigenvalues

6

EIGR

RS

Eigenvalue – real part

7

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 TCODE,1 =02

Sort 2

6

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

7

MFREQ

RS

Modal frequency (Hz)

End TCODE,1

8

UNDEF

None

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

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Data Block Descriptions O-V

Name

Word 115

LABEL(32)

Type CHAR4

Description Label

Record 2 - DATA Name

Word

Type

Description

TCODE,1 =01

Sort 1

1

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

2

MFREQ

RS

Modal frequency (Hz)

TCODE,1 =02

Sort 2

ACODE,4 =05 1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

ACODE,4 =06 1

TIME

RS

2

UNDEF

None

Time step

ACODE,4 =09 1

EIGR

RS

Eigenvalue – real part

2

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 End TCODE,1 TCODE,7 = 0 or 2

Real

3

RS

MC

TCODE,7 =1

Modal contribution

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

End TCODE,7

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Chapter 5

Record 3 - TRAILER Name

Word

Type

1

NREC

I

2

UNDEF(5 )

None

Description Number of records

5.28 OUG Table of displacements, velocities, accelerations Also, temperatures for heat transfer and sound pressure levels for acoustic analyses. For all analysis types (real and complex), and SORT1 and SORT2 formats.

Record - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

DATCOD

I

Data code: 0 = rigid body motion included 1 = rigid body motion excluded

4

SUBCASE

I

Subcase or Random identification number

TCODE,1 =1

Sort 1

ACODE,4 =01

Statics

5

LSDVMN

I

6

UNDEF(2 )

None

Load set number

ACODE,4 =02

Real Eigenvalues

5

I

5-330

MODE

DMAP Programmer’s Guide

Mode Number

Data Block Descriptions O-V

Name

Word

Type

Description

6

EIGN

RS

Eigenvalue

7

MODECYCL

RS

Mode or Cycle

ACODE,4 =03

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

Load set number

ACODE,4 =04

Differential Stiffness

5

LSDVMN

I

6

UNDEF(2 )

None

ACODE,4 =05

Frequency

5

FREQ

RS

6

UNDEF

None

7

RANDOM ID

I

ACODE,4 =06

Transient

5

TIME

RS

6

UNDEF(2 )

None

Load set number

Frequency

Random identification number

Time Step

ACODE,4 =07

Buckling Phase 0 (Pre-buckling)

5

LSDVMN

I

6

UNDEF(2 )

None

Load set

ACODE,4 =08

Buckling Phase 1 (Post-buckling)

5

LSDVMN

I

Mode Number

6

EIGR

RS

Eigenvalue

7

RANDID

I

Random ID number

ACODE,4 =09

Complex Eigenvalues

5

MODE

I

Mode

6

EIGR

RS

Eigenvalue (real)

7

EIGI

RS

Eigenvalue (imaginary)

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ACODE,4 =10

Nonlinear statics

5

LFTSFQ

RS

6

UNDEF(2 )

None

Load step

ACODE,4 =11

Old geometric nonlinear statics

5

LSDVMN

I

6

UNDEF

None

7

RANDID

I

Load set

Random ID number

ACODE,4 =12

CONTRAN ? ( Can appear as ACODE=6 )

5

TIME

RS

6

UNDEF(2 )

None

Time

End ACODE,4 TCODE,1 =02

Sort 2

5

LSDVMN

I

6

UNDEF(2 )

None

Load set, Mode Number

End TCODE,1 8

RCODE

I

Random code ID number

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(2)

None

13

ACFLAG(C)

I

14

UNDEF(9 )

None

23

THERMAL

I

24

UNDEF(27 )

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

5-332

DMAP Programmer’s Guide

Acoustic presure flag

1 for heat transfer and 0 otherwise

Data Block Descriptions O-V

Record - DATA Name

Word

Type

TCODE,1 =01

Sort 1

1

I

EKEY

TCODE,1 =02

Description

Device code + 10* Point identification number

Sort 2 - Swap with word 5 of IDENT

ACODE,4 =01 1

EKEY

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

RS

Frequency

RS

Time step

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

I

Device code + 10* Point identification number

RS

Frequency or Time step

I

Device code + 10* Point identification number

ACODE,4 =02 1

EKEY

ACODE,4 =03 1

EKEY

ACODE,4 =04 1

EKEY

ACODE,4 =05 1

FREQ

ACODE,4 =06 1

TIME

ACODE,4 =07 1

EKEY

ACODE,4 =08 1

EKEY

ACODE,4 =09 1

EKEY

ACODE,4 =10 1

FQTS

ACODE,4 =11 1

EKEY

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ACODE,4 =12 Word

Name

Type

Description

1

EKEY

I

Device code + 10* Point identification number

I

Point type: G for grid and S for scalar

End ACODE,4 End TCODE,1 2

TYPE

TABLCODE=01

Displacement - TablCode=MOD(TCODE,1000)

TCODE,2 =01 ACFLAG =0

Real

TCODE,7 =0 or 2

Real or Random Response

3

DT1

RS

Translation in direction 1

4

DT2

RS

Translation in direction 2

5

DT3

RS

Translation in direction 3

6

DR1

RS

Rotation in direction 1

7

DR2

RS

Rotation in direction 2

8

DR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

DT1R

RS

Translation in direction 1

4

DT2R

RS

Translation in direction 2

5

DT3R

RS

Translation in direction 3

6

DR1R

RS

Rotation in direction 1

7

DR2R

RS

Rotation in direction 2

8

DR3R

RS

Rotation in direction 3

9

DT1I

RS

Translation in direction 1 - imaginary

10

DT2I

RS

Translation in direction 2 - imaginary

11

DT3I

RS

Translation in direction 3 - imaginary

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Data Block Descriptions O-V

Name

Word

Type

Description

12

DR1I

RS

Rotation in direction 1 - imaginary

13

DR2I

RS

Rotation in direction 2 - imaginary

14

DR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

ACFLAG =2

Acoustic Pressure

TCODE,7 =0 or 2

Real or Random Response

3

P

RS

Sound pressure level

4

PRMS

RS

RMS Sound pressure level

5

DB

RS

Sound pressure level in dB

6

DBA

RS

Sound pressure level in dBA

7

UNDEF(2 )

None

TCODE,7 =1

Real/ Imaginary

3

PR

RS

Sound pressure level

4

PRMSR

RS

RMS Sound pressure level

5

DBR

RS

Sound pressure level in dB

6

DBAR

RS

Sound pressure level in dBA

7

PI

RS

Sound pressure level - imaginary

8

PRMSI

RS

RMS Sound pressure level - imaginary

9

DBI

RS

Sound pressure level in dB - imaginary

10

DBAI

RS

Sound pressure level in dBA - imaginary

11

UNDEF(4 )

None

End TCODE,7 End ACFLAG Word TCODE,2 =07

Name

Type

Description

Eigenvector Displacement

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

TCODE,7 =0 or 2

Real or Random Response

3

DT1

RS

Translation in direction 1

4

DT2

RS

Translation in direction 2

5

DT3

RS

Translation in direction 3

6

DR1

RS

Rotation in direction 1

7

DR2

RS

Rotation in direction 2

8

DR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

DT1R

RS

Translation in direction 1

4

DT2R

RS

Translation in direction 2

5

DT3R

RS

Translation in direction 3

6

DR1R

RS

Rotation in direction 1

7

DR2R

RS

Rotation in direction 2

8

DR3R

RS

Rotation in direction 3

9

DT1I

RS

Translation in direction 1 - imaginary

10

DT2I

RS

Translation in direction 2 - imaginary

11

DT3I

RS

Translation in direction 3 - imaginary

12

DR1I

RS

Rotation in direction 1 - imaginary

13

DR2I

RS

Rotation in direction 2 - imaginary

14

DR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

TCODE,2 =10

Velocity

TCODE,7 =0 or 2

Real or Random Response

3

VT1

RS

Translation in direction 1

4

VT2

RS

Translation in direction 2

5-336

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

5

VT3

RS

Translation in direction 3

6

VR1

RS

Rotation in direction 1

7

VR2

RS

Rotation in direction 2

8

VR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

VT1R

RS

Translation in direction 1

4

VT2R

RS

Translation in direction 2

5

VT3R

RS

Translation in direction 3

6

VR1R

RS

Rotation in direction 1

7

VR2R

RS

Rotation in direction 2

8

VR3R

RS

Rotation in direction 3

9

VT1I

RS

Translation in direction 1 - imaginary

10

VT2I

RS

Translation in direction 2 - imaginary

11

VT3I

RS

Translation in direction 3 - imaginary

12

VR1I

RS

Rotation in direction 1 - imaginary

13

VR2I

RS

Rotation in direction 2 - imaginary

14

VR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

TCODE,2 =11

Acceleration

TCODE,7 =0 or 2

Real or Random Response

3

AT1

RS

Translation in direction 1

4

AT2

RS

Translation in direction 2

5

AT3

RS

Translation in direction 3

6

AR1

RS

Rotation in direction 1

7

AR2

RS

Rotation in direction 2

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word 8

AR3

Type RS

TCODE,7 =1

Description Rotation in direction 3

Real/ Imaginary

3

AT1R

RS

Translation in direction 1

4

AT2R

RS

Translation in direction 2

5

AT3R

RS

Translation in direction 3

6

AR1R

RS

Rotation in direction 1

7

AR2R

RS

Rotation in direction 2

8

AR3R

RS

Rotation in direction 3

9

AT1I

RS

Translation in direction 1 - imaginary

10

AT2I

RS

Translation in direction 2 - imaginary

11

AT3I

RS

Translation in direction 3 - imaginary

12

AR1I

RS

Rotation in direction 1 - imaginary

13

AR2I

RS

Rotation in direction 2 - imaginary

14

AR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

TCODE,2 =14

Eigenvector Displacement (Solution Set)

TCODE,7 =0 or 2

Real or Random Response

3

DT1

RS

Translation in direction 1

4

DT2

RS

Translation in direction 2

5

DT3

RS

Translation in direction 3

6

DR1

RS

Rotation in direction 1

7

DR2

RS

Rotation in direction 2

8

DR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

DT1R

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RS

Translation in direction 1

Data Block Descriptions O-V

Name

Word

Type

Description

4

DT2R

RS

Translation in direction 2

5

DT3R

RS

Translation in direction 3

6

DR1R

RS

Rotation in direction 1

7

DR2R

RS

Rotation in direction 2

8

DR3R

RS

Rotation in direction 3

9

DT1I

RS

Translation in direction 1 - imaginary

10

DT2I

RS

Translation in direction 2 - imaginary

11

DT3I

RS

Translation in direction 3 - imaginary

12

DR1I

RS

Rotation in direction 1 - imaginary

13

DR2I

RS

Rotation in direction 2 - imaginary

14

DR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

TCODE,2 =15

Displacement (Solution Set)

TCODE,7 =0 or 2

Real or Random Response

3

DT1

RS

Translation in direction 1

4

DT2

RS

Translation in direction 2

5

DT3

RS

Translation in direction 3

6

DR1

RS

Rotation in direction 1

7

DR2

RS

Rotation in direction 2

8

DR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

DT1R

RS

Translation in direction 1

4

DT2R

RS

Translation in direction 2

5

DT3R

RS

Translation in direction 3

6

DR1R

RS

Rotation in direction 1

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Chapter 5

Name

Word

Type

Description

7

DR2R

RS

Rotation in direction 2

8

DR3R

RS

Rotation in direction 3

9

DT1I

RS

Translation in direction 1 - imaginary

10

DT2I

RS

Translation in direction 2 - imaginary

11

DT3I

RS

Translation in direction 3 - imaginary

12

DR1I

RS

Rotation in direction 1 - imaginary

13

DR2I

RS

Rotation in direction 2 - imaginary

14

DR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

TCODE,2 =16

Velocity (Solution Set)

TCODE,7 =0 or 2

Real or Random Response

3

VT1

RS

Translation in direction 1

4

VT2

RS

Translation in direction 2

5

VT3

RS

Translation in direction 3

6

VR1

RS

Rotation in direction 1

7

VR2

RS

Rotation in direction 2

8

VR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

VT1R

RS

Translation in direction 1

4

VT2R

RS

Translation in direction 2

5

VT3R

RS

Translation in direction 3

6

VR1R

RS

Rotation in direction 1

7

VR2R

RS

Rotation in direction 2

8

VR3R

RS

Rotation in direction 3

9

VT1I

RS

Translation in direction 1 - imaginary

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Data Block Descriptions O-V

Name

Word

Type

Description

10

VT2I

RS

Translation in direction 2 - imaginary

11

VT3I

RS

Translation in direction 3 - imaginary

12

VR1I

RS

Rotation in direction 1 - imaginary

13

VR2I

RS

Rotation in direction 2 - imaginary

14

VR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 Name

Word

Type

Description

TCODE,2 =17

Acceleration (Solution Set)

TCODE,7 =0 or 2

Real or Random Response

3

AT1

RS

Translation in direction 1

4

AT2

RS

Translation in direction 2

5

AT3

RS

Translation in direction 3

6

AR1

RS

Rotation in direction 1

7

AR2

RS

Rotation in direction 2

8

AR3

RS

Rotation in direction 3

TCODE,7 =1

Real/ Imaginary

3

AT1R

RS

Translation in direction 1

4

AT2R

RS

Translation in direction 2

5

AT3R

RS

Translation in direction 3

6

AR1R

RS

Rotation in direction 1

7

AR2R

RS

Rotation in direction 2

8

AR3R

RS

Rotation in direction 3

9

AT1I

RS

Translation in direction 1 - imaginary

10

AT2I

RS

Translation in direction 2 - imaginary

11

AT3I

RS

Translation in direction 3 - imaginary

12

AR1I

RS

Rotation in direction 1 - imaginary

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Chapter 5

Name

Word

Type

Description

13

AR2I

RS

Rotation in direction 2 - imaginary

14

AR3I

RS

Rotation in direction 3 - imaginary

End TCODE,7 End TCODE,2

Record - TRAILER Name

Word 1

UNDEF(6 )

Type

Description

None

5.29 OUGGC Table of grid contributions. For frequency analysis types (complex), and SORT1 and SORT2 formats.

Record - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

GCODE

I

Grid contributions code: 1=absolute (modal), 2=normalized (modal), -1=absolute (direct), -2=normalized (direct)

4

SUBCASE

I

Subcase number

5

DCODE

I

Acoustic dof code (10*grid ID + direction)

TCODE,1=01

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Sort 1

Data Block Descriptions O-V

Name

Word

Type

ACODE,4=05

Frequency

6

FREQ

RS

7

UNDEF

None

Description

Frequency (Hz)

End ACODE,4 TCODE,1=02

Sort 2

6

GID

I

7

UNDEF

None

Grid ID (0 for TOTAL)

End TCODE,1 8

DATTYP

I

Data Type (1=pressure, 2=first derivative, 3=second derivative)

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record - DATA Name

Word TCODE,1=01

Type

Description

Sort 1

1

GID

I

2

UNDEF

None

TCODE,1=02

Grid ID (0 for TOTAL)

Sort 2

1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

End TCODE,1 TCODE,2=01

Pressure

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word TCODE,7=01

Type

Description

Real/Imaginary

3

GCR

RS

Grid contribution – real part

4

GCI

RS

Grid contribution – imaginary part

End TCODE,7 Name

Word

Type

Description

TCODE,2=10

First derivative of pressure

TCODE,7=01

Real/Imaginary

3

GCR

RS

Grid contribution – real part

4

GCI

RS

Grid contribution – imaginary part

End TCODE,7 Name

Word

Type

Description

TCODE,2=11

Second derivative of pressure

TCODE,7=01

Real/Imaginary

3

GCR

RS

Grid contribution – real part

4

GCI

RS

Grid contribution – imaginary part

End TCODE,7

Record - TRAILER Word

Name

Type

1

NREC

I

2

UNDEF(5 )

None

Description Number of records

5.30 OUGMC Table of modal contributions for displacements, velocities, accelerations. For all analysis types (real and complex), and SORT1 and SORT2 formats.

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Data Block Descriptions O-V

Record - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code (TCODE,2 = 1 for displacement; TCODE,2 = 10 for velocity; TCODE,2 = 11 for acceleration)

3

MCODE

I

Modal contributions code: 1=absolute, 2=normalized

4

SUBCASE

I

Subcase number

5

DCODE

I

DOF code (10*grid ID + direction)

TCODE,1 = 1

Sort 1

ACODE,4 = 05

Frequency

6

FREQ

RS

7

UNDEF

None

ACODE,4 =06

Transient

6

TIME

RS

7

UNDEF

None

Frequency (Hz)

Time step

ACODE,4 =09

Complex Eigenvalues

6

EIGR

RS

Eigenvalue – real part

7

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 TCODE,1 =02

Sort 2

PANFLG = 1

Panel data

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word 6

PNAME(2)

PANFLG = 0

Type CHAR4

Description Panel name

Not panel data

6

MODE

I

Mode number (0 for TOTAL; -1 for constraint modes)

7

MFREQ

RS

Modal frequency (Hz)

End PANFLG End TCODE,1 8

DATTYP

I

Data Type (1=displacement, 2=velocity, 3=acceleration)

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

NOMC(C)

I

Number of modal contribution data sets

12

NUMPAN(C)

I

Number of panels

13

PANFLG

I

Panel flag (1 = panel data; 0 = mode data)

14

UNDEF(37)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record - DATA Name

Word

Type

Description

TCODE,1 = 01

Sort 1

1

MODE

I

Mode number (0 for TOTAL)

2

MFREQ

RS

Modal frequency (Hz)

TCODE,7 = 0 or 2

Real

3

MC

RS

Modal contribution

4

MODE

I

Mode number (-1 for constraint modes)

5

MFREQ

RS

Modal frequency (Hz)

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Data Block Descriptions O-V

Name

Word 6

MC

Type RS

Description Modal contribution

Words 4–6 repeat NOMC times End TCODE,7 = 0 or 2 TCODE,7 = 1

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

5

MODE

I

Mode number (-1 for constraint modes)

6

MFREQ

RS

Modal frequency (Hz)

7

MCR

RS

Modal contribution – real part

8

MCI

RS

Modal contribution – imaginary part

Words 5–8 repeat NOMC times The remaining definitions only exist if NUMPAN > 0 9

MODE

I

Mode number (-1 for constraint modes)

10

MFREQ

RS

Modal frequency (Hz)

11

MCR

RS

Modal contribution - real part

12

MCI

RS

Modal contribution - imaginary part

13

PNAME(2)

CHAR4

Panel name

15

PCR

RS

Panel contribution – real part

16

PCI

RS

Panel contribution – imaginary part

Words 13–16 repeat NUMPAN times Words 9–16 repeat NOMC times End TCODE,7 = 1 TCODE,1 = 02

Sort 2

ACODE,4 =05

Frequency response

1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

ACODE,4 = 06

Transient response

1

TIME

RS

2

UNDEF

None

Time step

ACODE,4 = 09

Complex eigenvalues

1

EIGR

RS

Eigenvalue – real part

2

EIGI

RS

Eigenvalue – imaginary part

End ACODE,4 TCODE,7 =0 or 2

Real

3

RS

MC

TCODE,7 =1

Modal contribution

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

End TCODE,7 Name

Word

Type

TCODE,2 = 10

Velocity

TCODE,7 = 0 or 2

Real

3

RS

MC

Description

Modal contribution

TCODE,7 = 1

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

End TCODE,7 Name

Word

Type

TCODE,2 = 11

Acceleration

TCODE,7 = 0 or 2

Real

3

RS

5-348

MC

DMAP Programmer’s Guide

Description

Modal contribution

Data Block Descriptions O-V

Name

Word

Type

Description

TCODE,7 = 1

Real/ Imaginary

3

MCR

RS

Modal contribution – real part

4

MCI

RS

Modal contribution – imaginary part

End TCODE,7

Record - TRAILER Name

Word

Type

1

NREC

I

2

UNDEF(5)

None

Description Number of records

5.31 OUGPC Table of panel contributions. For frequency analysis types (complex), and SORT1 and SORT2 formats.

Record - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Word

Name

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

PCODE

I

Panel contributions code: 1=absolute (modal), 2=normalized (modal), -1=absolute (direct), -2=normalized (direct)

4

SUBCASE

I

Subcase number

5

DCODE

I

Acoustic dof code (10*grid ID + direction)

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

TCODE,1=01

Sort 1

ACODE,4=05

Frequency

6

FREQ

RS

7

UNDEF

None

Description

Frequency (Hz)

End ACODE,4 TCODE,1=02 6

Sort 2 PNAME(2)

CHAR4

Panel name (0 for TOTAL)

End TCODE,1 8

DATTYP

I

Data Type (1=pressure, 2=first derivative, 3=second derivative)

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

Title

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record - DATA Name

Word TCODE,1=01 1

Type

Description

Sort 1 PNAME(2)

TCODE,1=02

CHAR4

Panel name (0 for TOTAL)

Sort 2

1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

End TCODE,1 TCODE,2=01

Pressure

TCODE,7=01

Real/Imaginary

5-350

DMAP Programmer’s Guide

Data Block Descriptions O-V

Name

Word

Type

Description

3

PCR

RS

Panel contribution – real part

4

PCI

RS

Panel contribution – imaginary part

End TCODE,7 Name

Word

Type

Description

TCODE,2=10

First derivative of pressure

TCODE,7=01

Real/Imaginary

3

PCR

RS

Panel contribution – real part

4

PCI

RS

Panel contribution – imaginary part

End TCODE,7 Name

Word

Type

Description

TCODE,2=11

Second derivative of pressure

TCODE,7=01

Real/Imaginary

3

PCR

RS

Panel contribution – real part

4

PCI

RS

Panel contribution – imaginary part

End TCODE,7

Record - TRAILER Word

Name

Type

1

NREC

I

2

UNDEF(5 )

None

Description Number of records

5.32 OUGRC Table of reciprocal panel contributions. For frequency analysis types (complex), and SORT1 and SORT2 formats.

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Record - HEADER Name

Word

Type

Description

1

NAME(2)

CHAR4

Data block name

3

WORD

I

No Def or Month, Year, One, One

Word 3 repeats until End of Record

Record - IDENT Name

Word

Type

Description

1

ACODE(C)

I

Device code + 10*Approach Code

2

TCODE(C)

I

Table Code

3

PCODE

I

Reciprocal panel contributions code: 1=absolute (modal), 2=normalized (modal), -1=absolute (direct), -2=normalized (direct)

4

SUBCASE

I

Subcase number

5

DCODE

I

Acoustic dof code (10*grid ID + direction)

TCODE,1=01

Sort 1

ACODE,4=05

Frequency

6

FREQ

RS

7

UNDEF

None

Frequency (Hz)

End ACODE,4 TCODE,1=02 6

Sort 2 PNAME(2)

CHAR4

Panel name (0 for TOTAL)

End TCODE,1 8

DATTYP

I

Data Type (1=displacement, 2=velocity, 3=acceleration)

9

FCODE

I

Format Code

10

NUMWDE

I

Number of words per entry in DATA record

11

UNDEF(40)

None

51

TITLE(32)

CHAR4

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DMAP Programmer’s Guide

Title

Data Block Descriptions O-V

Name

Word

Type

Description

83

SUBTITL(32)

CHAR4

Subtitle

115

LABEL(32)

CHAR4

Label

Record - DATA Name

Word TCODE,1=01 1

Type

Description

Sort 1 PNAME(2)

TCODE,1=02

CHAR4

Panel name (0 for TOTAL)

Sort 2

1

FREQ

RS

2

UNDEF

None

Frequency (Hz)

End TCODE,1 TCODE,2=01

Displacement

TCODE,7=01

Real/Imaginary

3

PCR

RS

Reciprocal panel contribution – real part

4

PCI

RS

Reciprocal panel contribution – imaginary part

End TCODE,7 Name

Word

Type

Description

TCODE,2=02

Velocity

TCODE,7=01

Real/Imaginary

3

PCR

RS

Reciprocal panel contribution – real part

4

PCI

RS

Reciprocal panel contribution – imaginary part

End TCODE,7 Word

Name

Type

TCODE,2=03

Acceleration

TCODE,7=01

Real/Imaginary

Description

DMAP Programmer’s Guide

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Data Block Descriptions O-V

Chapter 5

Name

Word

Type

Description

3

PCR

RS

Reciprocal panel contribution – real part

4

PCI

RS

Reciprocal panel contribution – imaginary part

End TCODE,7

Record - TRAILER Name

Word

Type

1

NREC

I

2

UNDEF(5)

None

Description Number of records

5.33 R1MAP Table of mapping from original first level (Direct) Retained Responses

Record 0 – HEADER Word 1

Name

Type CHAR4

NAME(2)

Description Data block name

Record 1 – RESPONSE Word 1

Name IRID

Type I

Description Internal response identification number

Word 1 repeats until End of Record

Record 2 – TRAILER Word

Name

Type

1

WORD1

I

2

UNDEF(5 )

None

5-354

DMAP Programmer’s Guide

Description Number of responses

Data Block Descriptions O-V

5.34 R1TAB Table of type one response attributes

Record 0 - HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record 1 - Repeat Name

Word

Type

Description

1

IRID

I

Internal response identification number

2

RID

I

External response identification number

3

TYPE(C)

I

Response type

4

LABEL(2)

CHAR4

Label

6

REGION

I

Region identifier

7

SCID

I

Subcase identification number

Word

Name

TYPE =1

Type

Description

WEIGHT

8

ATTA

I

Weight DRESP1 ATTA entry or default=3

9

ATTB

I

Weight DRESP1 ATTB entry or default=3

10

SEID

I

Superelement identification number or ALL

11

UNDEF(2 )

None

TYPE =2

VOLUME

8

UNDEF(2 )

None

10

SEID

I

11

UNDEF(2 )

None

TYPE =3

Superelement identification number or ALL

LAMA

8

MODE

I

Mode number

9

APRX

I

Approximation code

DMAP Programmer’s Guide

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Chapter 5

Word 10

Data Block Descriptions O-V

Name UNDEF(3 )

TYPE =4

Type

Description

None EIGN or FREQ

8

MODE

I

Mode number

9

APRX

I

Approximation code

10

UNDEF(3 )

None

TYPE =5

DISP

8

COMP

I

9

UNDEF

None

10

GRID

I

11

UNDEF(2 )

None

TYPE =6

Grid identification number

STRESS

8

ICODE

I

9

UNDEF

None

10

ELID

I

11

UNDEF(2 )

None

TYPE =7

Stress item code

Element identification number

STRAIN

8

ICODE

I

9

UNDEF

None

10

ELID

I

11

UNDEF(2 )

None

TYPE =8

Strain item code

Element identification number

FORCE

8

ICODE

I

9

UNDEF

None

10

ELID

I

11

UNDEF(2 )

None

TYPE =9

5-356

Displacement component

DMAP Programmer’s Guide

CFAILURE

Force item code

Element identification number

Data Block Descriptions O-V

Name

Word

Type

Description

8

ICODE

I

Failure criterion item code

9

PLY

I

Lamina number

10

ELID

I

Element identification number

11

UNDEF(2 )

None

TYPE =10

CSTRESS

8

ICODE

I

Stress item code

9

PLY

I

Lamina number

10

ELID

I

Element identification number

11

UNDEF(2 )

None

TYPE =11

CSTRAIN

8

ICODE

I

Strain item code

9

PLY

I

Lamina number

10

ELID

I

Element identification number

11

UNDEF(2 )

None

TYPE =13

SPCFORCE

8

ICODE

I

9

UNDEF

None

10

GRID

I

11

UNDEF(2 )

None

TYPE =14

Grid identification number

ESE

8

ICODE

I

9

UNDEF

None

10

ELID

I

11

UNDEF(2)

None

TYPE =15 8

SPC force component

Strain energy item code

Element identification number

CEIG MODE

I

Mode number

DMAP Programmer’s Guide

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Chapter 5

Word

Data Block Descriptions O-V

Name

Type

9

ICODE

I

10

UNDEF(3)

None

Word

Name

TYPE =20

Description 1: Real component or 2: Imaginary component

Type

Description

FRDISP or PRES

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =21

Displacement or Acoustic pressure component

FRVELO

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =22

Velocity component

FRACCL

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =23

Acceleration Component

FRSPCF

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

5-358

DMAP Programmer’s Guide

SPCForce Component

Data Block Descriptions O-V

Word 12

Name UNDEF

TYPE =24

Type

Description

None FRSTRE

8

ICODE

I

9

UNDEF

None

10

ELID

I

Element identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =25

Stress item code

FRFORC

8

ICODE

I

9

UNDEF

None

10

ELID

I

Element identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =26

Force item code

RMSDISP

8

COMP

I

RMS Displacement component

9

RANDPS

I

RANDPS entry identification number

10

GRID

I

Grid identification number

11

DMFREQ

RS

Dummy frequency for internal use

12

UNDEF

None

TYPE =27

RMSVELO

8

COMP

I

RMS Velocity component

9

RANDPS

I

RANDPS entry identification number

10

GRID

I

Grid identification number

11

DMFREQ

RS

Dummy frequency for internal use

12

UNDEF

None

TYPE =28

RMSACCL

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Chapter 5

Word

Data Block Descriptions O-V

Name

Type

Description

8

COMP

I

RMS Acceleration component

9

RANDPS

I

RANDPS entry identification number

10

GRID

I

Grid identification number

11

DMFREQ

RS

Dummy frequency for internal use

12

UNDEF

None

TYPE =29

PSDDISP

8

COMP

I

PSD of Displacement component

9

RANDPS

I

RANDPS entry identification number

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =30

PSDVELO

8

COMP

I

PSD of Velocity component

9

RANDPS

I

RANDPS entry identification number

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

12

UNDEF

None

TYPE =31

PSDACCL

8

COMP

I

PSD of Acceleration component

9

RANDPS

I

RANDPS entry identification number

10

GRID

I

Grid identification number

11

FREQ

RS

Frequency

12

UNDEF

None

Word

Name

TYPE =60 8

5-360

Type

Description

TDISP COMP

DMAP Programmer’s Guide

I

Displacement component

Data Block Descriptions O-V

Word

Name

Type

Description

9

UNDEF

None

10

GRID

I

Grid identification number

11

TIME

RS

Time step

12

UNDEF

None

TYPE =61

TVELO

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

TIME

RS

Time step

12

UNDEF

None

TYPE =62

Velocity component

TACCL

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

TIME

RS

Time step

12

UNDEF

None

TYPE =63

Acceleration component

TSPCF

8

COMP

I

9

UNDEF

None

10

GRID

I

Grid identification number

11

TIME

RS

Time step

12

UNDEF

None

TYPE =64

SPCForce component

TSTRE

8

ICODE

I

9

UNDEF

None

10

ELID

I

Stress item code

Element identification number

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Data Block Descriptions O-V

Name

Word

Type

11

TIME

RS

12

UNDEF

None

TYPE =65

Description Time step

TFORCE

8

ICODE

I

9

UNDEF

None

10

ELID

I

Element identification number

11

TIME

RS

Time step

12

UNDEF

None

Name

Word TYPE =81

Force item code

Type

Description

DIVERG

8

ROOT

I

9

UNDEF(2 )

None

11

MACH

RS

Mach number

12

DIVERG

I

DIVERG identification number

TYPE =82

Root number

TRIM

8

XID

I

9

UNDEF(3 )

None

12

TRIM

I

TYPE =83

AESTAT or AESURF identification number

TRIM identification number

STABDER

8

XID

I

AESTAT or AESURF identification number

9

COMP

I

Component

10

RESFLG

I

Restraint flag

11

UNDEF

None

12

TRIM

I

TYPE =84 8

5-362

TRIM identification number

FLUTTER MODE

DMAP Programmer’s Guide

I

Mode number

Data Block Descriptions O-V

Name

Word

Type

Description

9

MACH

RS

Mach numbers

10

VELOC

RS

Velocity

11

DENSITY

RS

Density

12

FLUTTER

I

Flutter identification number

13

UNDEF

None

14

TYFLG

I

Flag to indicate how response is referenced

15

SEID

I

Superelement identification number

End TYPE

Record 2 - TRAILER Name

Word

Type

1

NR1

I

2

UNDEF(5 )

None

Description Number of type one responses (number of records in table)

Notes: 1. 2.

Table is in IRID order and is in the order in which responses are to be generated. TYFLG currently has no meaning. The intent was to use this attribute to identify responses that should always be retained in DSAD. However, this option is not currently supported.

5.35 RESP3 Table of second level (synthetic) responses computed by an external user-supplied program.

Record 0 - HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name

Record 1 - Repeat - for each Type 3 response Word 1

Name IR3ID

Type I

Description Internal response identification number

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Name

Word

Type

Description

2

R3ID

I

External response identification number

3

SUBID

I

Subcase identification number

4

LABEL(2)

CHAR4

Label

6

GROUP(2)

CHAR4

Group defined on an FMS CONNECT statement

8

TYPE(2)

CHAR4

User-created response calculation type in the external user-supplied program

10

REG

I

Region identification number

11

ND(C)

I

Number of design variables

12

NC(C)

I

Number of constants from constant table (Data block DTB)

13

NR(C)

I

Number of type one responses

14

NCORD(C)

I

Number of coordinates

15

NPROP1(C)

I

Number of type one properties

16

NCONP1(C)

I

Number of type one connectivity properties

17

NMATP1(C)

I

Number of type one material properties

18

NPROP2(C)

I

Number of type two properties

19

NCONP2(C)

I

Number of type two connectivity properties

20

NMATP2(C)

I

Number of type two material properties

21

NRR2(C)

I

Number of referenced type two responses

22

NSTR(C)

I

Number of CHAR4 words of USRDATA (rounded to an even number)

23

IDV

I

Internal design variable identification number

RS

Table constant

I

Type one response identification number

Word 23 repeats ND times 24

CVLT1

Word 24 repeats NC times 25

IR1ID

Word 25 repeats NR times

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Data Block Descriptions O-V

Name

Word

Type

Description

26

NODE

I

Node number

27

DIR

I

Direction

Words 26 through 27 repeat NCORD times 28

PROP1ID

I

Type one property identification number

Word 28 repeats NPROP1 times 29

CONP1ID

I

Type one connectivity property identification number

Word 29 repeats NCONP1 times 30

MATP1ID

I

Type one material property identification number

Word 30 repeats NMATP1 times 31

PROP2ID

I

Type two property identification number

Word 31 repeats NPROP2 times 32

CONP2ID

I

Type two connectivity property identification number

Word 32 repeats NCONP2 times 33

MATP2ID

I

Type two material property identification number

Word 33 repeats NMATP2 times 34

IR2ID

I

Type two response identification number

CHAR4

User input data

Word 34 repeats NRR2 times 35

USRDATA

Word 35 repeats NSTR times

Record 2 - TRAILER Word

Name

Type

Description

1

NRP3

I

Number of records (type 3 responses) in the table

2

MAXL

I

Maximum record length

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Word 3

Data Block Descriptions O-V

Name UNDEF(4)

Type

Description

None

5.36 RESP12 Table of second level (synthetic) responses

Record 0 - HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name

Record 1 - Repeat - for each Type 2 response Word

Name

Type

Description

1

IR2ID

I

Internal response identification number

2

R2ID

I

External response identification number

3

SUBID

I

Subcase identification number

4

LABEL(2)

CHAR4

Label

6

EQID

I

Equation identification number, or mathematical function flag when negative

7

REG

I

Region identification number

8

ND(C)

I

Number of design variables

9

NC(C)

I

Number of constants from constant table (Data block DTB)

10

NR(C)

I

Number of type one responses

11

NCORD(C)

I

Number of coordinates

12

NPROP1(C)

I

Number of type one properties

13

NCONP1(C)

I

Number of type one connectivity properties

14

NMATP1(C)

I

Number of type one material properties

15

NPROP2(C)

I

Number of type two properties

16

NCONP2(C)

I

Number of type two connectivity properties

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Data Block Descriptions O-V

Name

Word

Type

Description

17

NMATP2(C)

I

Number of type two material properties

18

NRR2(C)

I

Number of referenced type two responses

19

ARGDSP

I

Number of discrepancy on arguments

20

NCEQ(C)

I

Number of constants from equation table (Data block DEQATN)

21

IDV

I

Internal design variable identification number

RS

Table constant

I

Type one response identification number

Word 21 repeats ND times 22

CVLT1

Word 22 repeats NC times 23

IR1ID

Word 23 repeats NR times 24

NODE

I

Node number

25

DIR

I

Direction

Words 24 through 25 repeat NCORD times 26

PROP1ID

I

Type one property identification number

Word 26 repeats NPROP1 times 27

CONP1ID

I

Type one connectivity property identification number

Word 27 repeats NCONP1 times 28

MATP1ID

I

Type one material property identification number

Word 28 repeats NMATP1 times 29

PROP2ID

I

Type two property identification number

Word 29 repeats NPROP2 times 30

CONP2ID

I

Type two connectivity property identification number

Word 30 repeats NCONP2 times 31

MATP2ID

I

Type two material property identification number

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Chapter 5

Name

Word

Type

Description

Word 31 repeats NMATP2 times 32

IR2ID

I

Type two response identification number

RS

Equation constant

Word 32 repeats NRR2 times 33

CVLQ

Word 33 repeats NCEQ times 34

RC

I

Record count

35

ARGS

I

Number of arguments

36

OSCAR

I

Oscar type; always 13

37

DEQA

CHAR4

"DEQA"

38

RECNUM

I

Record number

39

BIT

I

DEQATN identification number number bitwise-or-ed with bit 32

40

TLC(C)

I

Temporary VPS location count

41

TEMPVPS

I

Temporary VPS locations

Word 41 repeats TLC times 42

IC(C)

I

Instruction word count

43

INST

CHAR4

Instruction character word

44

INSTI(3)

I

Instruction integer words

Words 43 through 46 repeat IC/4 times 47

DATATYP

I

DATATYP =1

Integer input

48

I

INT

DATATYP =2

Real input

48

RS

REAL

Temporary VPS value section

Integer

Real

DATATYP =3

Character input

48

CHAR4

CHARS(2)

End DATATYP

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Character

Data Block Descriptions O-V

Name

Word

Type

Description

Words 47 through max repeat until End of Record

Record 2 - TRAILER Name

Word

Type

Description

1

NRP2

I

Number of records (type 2 responses) in the table

2

MAXL

I

Maximum record length

3

MAXEQ

I

Maximum value of EQPOS - 1 for all the records

4

UNDEF(3 )

None

Notes: 1. EQPOS = 12 + ND + NC + NR + 2*NCORD + NPROP + NCEQ 1.NCC is equal to 2*NCRD. 2. Pointer FRT1 is equal to ND+NCT+12, pointer FRCD is equal to FRT1+NCEQ, pointer FRCEQ is equal to FRCD + 2 * NCRD, pointer EQPOS is equal to FRCEQ + NCEQ.

5.37 SEMAP Superelement Definition Table (Map) Provides geometry and connection information for a problem formulated in terms of superelements.

Record 0 - HEADER Word 1

Name NAME(2)

Type CHAR4

Description Data block name

Record 1 - DEFINE Repeated for each superelement according to process order Word

Name

Type

Description

1

SEID

I

Super element identification number

2

INTIDX

I

Internal index of superelement

3

ORDER

I

Processing order

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Name

Word

Type

Description

4

SEDN

I

Downstream superelement identification number

5

SEDWNIDX

I

Internal index of downstream superelement

6

PEID

I

Primary superelement identification number

7

TYPEBIT

I

Superelement type bit map (See note 3)

8

NODNCNCT

I

Number of downstream connections

9

BITINFO

I

On bits correspond to connected downstream SE’s

Word 9 repeats LENTRY-1 times Words 8 through 9 repeat NBRSE times 10

NLBL

I

Number of SELABEL entries

11

NWLBL(C)

I

Number of words in label

12

SEID

I

Super element identification number

13

LABELI

CHAR4

Four characters in the label

Word 13 repeats NWLBL times Words 10 through 13 repeat NLBL times

Record 2 - MAP Repeated for each superelement according to process order and contains LENTRY words per grid point Word

Name

Type

Description

1

GRIDID

I

Grid point identification number

2

GRIDBIT

I

Grid point bit map

Word 2 repeats LENTRY-1 times

Record 3 - INFO Repeated for each superelement according to process order Word

Name

1

SEID

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DMAP Programmer’s Guide

Type I

Description Superelement identification number

Data Block Descriptions O-V

Word

Name

Type

Description

2

BITNO

I

Bit number for superelement

3

NG(C)

I

Number of exterior grid points

4

NE(C)

I

Number of elements NE=NBR of simple+genel+rigid

5

PEID

I

Primary superelement identification number

6

SEBITS

I

Superelement type bit map (See Note 3)

7

SEDWN

I

Downstream superelement identification number

8

BITDWN

I

Bit number of downstream superelement

9

EXTGRD

I

Sorted list of exterior (boundary) grid point identification numbers

I

Sorted list of element identification numbers

I

List of primary superelement exterior grids

Word 9 repeats NG times 10

ELIDS

Word 10 repeats NE times 11

PGRID

Word 11 repeats until End of Record

Record 4 - TRAILER Word

Name

Type

Description

1

NBRSE

I

Number of superelements including residual (NBRSE+1)

2

NBRGP

I

Total number of grid and scalar points in structure

3

NBRSCL

I

Number of scalar points

4

LENTRY

I

Number of words per entry in RECORD=MAP

5

NBRSEC

I

Number of secondary superelements

6

NWDDEF

I

Number of words per entry in RECORD=DEFINE

Notes: 1. SEID=0 implies residual.

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Chapter 5

2. This table is UNSTRUCTURED. The reason is that each of the records repeat for each superelement. 3. The low order (right to left) 10 bits in TYPEBIT are set as follows: Bit Position: Meaning 0 9 8 7 6 5 4 3 2 1 ------------------0 0 0 0 0 0 0 0 0 0 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1 . . . . . . . . . . 1

------Primary Partitioned Reflect Z Reflect Y Reflect X Repeated Collector External Mirror Identical Apply mapping transform

4. The BITINFO in ENTRY=DWNCNCT indicates the downstream superelement(s?). Bit Number

Downstream superelement is:

0

The residual structure

1 through NBRSE-1

The superelement(s) corresponding to the INTIDX-th bit(s)

5. In ENTRY=GRIDMAP, bits are numbered left to right beginning with zero and span LENTRY-1 words. Bit number

Meaning

0

Grid is connected to the residual structure

1 through NBRSE-1

Grid is connected to the superelement(s) corresponding to the INTIDX-th bit(s)

NBRSE

Grid is a scalar point

NBRSE+1

Grid is an incongruent boundary point

MAXBIT-IDBITS through MAXBIT

Internal superelement index (INTIDX) to which grid is interior

6. where MAXBIT = NBPW*(LENTRY-1)-1, NBPW is the number of bits per word, and "incongruent" indicates inconsistent coordinate systems on the boundary point. 7. In RECORD=INFO the primary superelement exterior grid points are sorted in the order of the secondary exterior grid points. Only if SEQSEP is specified. 8. SELABEL is created by SEP1X only. 9. LENTRY is computed from IDBITS: 10. IDBITS is the minimum number of bits required to represent NBRSE.

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Data Block Descriptions O-V

IDBITS = int (

ln ( max (NBRSE,1))

+ 1.01)

ln 2 ln 2 11. where ln is the natural logarithm and int is the integer function. 12. LENTRY is number of words in the grid point map. NBRSE + IDBITS + 1

LENTRY = int (

+ 2)

NBPW NBPW 13. For example, if NBRSE=50 and NBPW=32, IDBITS=6 and LENTRY=3. 14. The structure of RECORD=MAP is the same for SEP1 and SEP1X, but the content is different. For SEP1X, GRIDID in RECORD=MAP identifies only boundary grid points and GRIDBIT delineates to which superelement the point connects. For SEP1 the bits are not really clear in meaning. However some rules tend to indicate when the exterior grid becomes interior. 15. RECORD=INFO is the same between both systems, although modules SEP1X and SEP2X do not use ENTRY=ELIDS. 16. ENTRY=PGRID exists only for secondary superelements with resequencing, that is, bit 1 is on in TYPE, and lists the relative primary grid points in the same order as ENTRY=EXTGRD.

5.38 SET Table of combined sets

Record 0 – HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 – (*) Name

Word

Type

Description

1

ID

I

Set identification number

2

TYPE

I

Set type

3

SETORIG

I

Origin of set

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Data Block Descriptions O-V

Name

Word

Type

Description

4

SETLEN

I

Length of set

5

SETMEM

I

Set members

Word 5 repeats SETLEN times

Record 2 – TRAILER Name

Word

Type

Description

1

WORD1

I

Number of sets

2

WORD2

I

Number of members in largest set

3

UNDEF(4 )

None

Notes: 1. TYPE: 0=unknown, 1=grid, 2=element, 3=grid pairs 2. SETORIG: 1=Case Control section, 2=plot section, 3=SET1 Bulk Data entries, 4=MSGMESH input

5.39 SETMC Table of SETMC case control commands.

Record 0 - HEADER Name

Word 1

NAME(2)

Type CHAR4

Description Data block name

Record 1 - IDENT Name

Word

Type

Description

1

SID

I

Subcase identification number

2

SETID

I

Set identification number

3

SETLEN(C)

I

Length of this set

4

SETMEM

I

Set member identification number

Word 4 repeats SETLEN times

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Data Block Descriptions O-V

Name

Word

Type

Description

Words 2 through 4 repeat NSETS times

Record N - TRAILER Name

Word

Type

Description

1

WORD1

I

Number of records

2

WORD2

I

Maximum record length

3

UNDEF(4)

None

5.40 SIL Scalar index list.

Record – HEADER Name

Word 1

Type

NAME(2)

CHAR4

Name

Type

Description Data block name

Record – SIL Word

Description

GRID = scalar point 1

SIL

I

Scalar index list item

I

Scalar index list item

GRID = heat transfer 1

SIL

GRID = grid point 1

SIL1

I

Scalar index list item

2

SIL2

I

Scalar index list item

3

SIL3

I

Scalar index list item

4

SIL4

I

Scalar index list item

5

SIL5

I

Scalar index list item

6

SIL6

I

Scalar index list item

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Data Block Descriptions O-V

Record – TRAILER Word

Name

Type

Description

1

WORD1

I

Number of grid points plus scalar points

2

WORD2

I

Number of degrees-of-freedom in the g-displacement set

3

WORD3

I

0

4

WORD4

I

0

5

WORD5

I

0

6

WORD6

I

0

5.41 TOL Transient response time step output list

Record 0 – HEADER Word

Name

Type

Description

1

NAME(2)

CHAR4

Data block name

3

TIME

RS

Time step

Word 3 repeats until End of Record

Record 1 – TRAILER Word

Name

Type

1

WORD1

I

2

UNDEF(5 )

None

Description Number of time steps

5.42 VIEWTB View information table Contains the relationship between each p-element and its view-elements and view-grids.

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Data Block Descriptions O-V

Record 0 - HEADER Name

Word 1

Type CHAR4

NAME(2)

Description Data block name

Record 1 - BEAMP(10500,105,14) Name

Word

Type

Description

1

EID

I

Element identification number

2

CID

I

Coordinate system identification number - from CID field

3

NX

I

View mesh subdivision - from VIEW field

4

NY

I

View mesh subdivision - from VIEW field

5

NZ

I

View mesh subdivision - from VIEW field

6

MTH

CHAR4

Method – ’DIRE’ means direct

7

MINEID

I

Mininum VUHEXA identification number for this element

8

MAXEID

I

Maximum VUHEXA identification number for this element

9

MINGID

I

Minimum Grid identification number for this element

10

MAXGID

I

Maximum Grid identification number for this element

11

G(2)

I

Corner Grid identification numbers

12

ICORD

CHAR4

Flags for convective coordinate system – from PROJ and NORMAL fields

13

UNDEF

Record 2 - HEXAP(14100,141,18) Name

Word

Type

Description

1

EID

I

Element identification number

2

CID

I

Coordinate system identification number - from CID field

3

NX

I

View mesh subdivision - from VIEW field

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Data Block Descriptions O-V

Name

Word

Type

Description

4

NY

I

View mesh subdivision - from VIEW field

5

NZ

I

View mesh subdivision - from VIEW field

6

MTH

CHAR4

Method – ’DIRE’ means direct

7

MINEID

I

Mininum VUHEXA identification number for this element

8

MAXEID

I

Maximum VUHEXA identification number for this element

9

MINGID

I

Minimum Grid identification number for this element

10

MAXGID

I

Maximum Grid identification number for this element

11

G(8)

I

Corner Grid identification numbers

Record 3 – PENTAP(14200,142,16) Name

Word

Type

Description

1

EID

I

Element identification number

2

CID

I

Coordinate system identification number - from CID field

3

NX

I

View mesh subdivision – from VIEW field

4

NY

I

View mesh subdivision – from VIEW field

5

NZ

I

View mesh subdivision – from VIEW field

6

MTH

CHAR4

Method – ’DIRE’ means direct

7

MINEID

I

Mininum VUPENTA IDENTIFICATION NUMBER for this element

8

MAXEID

I

Maximum VUPENTA IDENTIFICATION NUMBER for this element

9

MINGID

I

Minimum Grid identification number for this element

10

MAXGID

I

Maximum Grid identification number for this element

11

G(6)

I

Corner Grid identification numbers

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Data Block Descriptions O-V

Record 4 - QUADP(10300,103,16) Name

Word

Type

Description

1

EID

I

Element identification number

2

CID

I

Coordinate system identification number - from CID field

3

NX

I

View mesh subdivision - from VIEW field

4

NY

I

View mesh subdivision - from VIEW field

5

NZ

I

View mesh subdivision - from VIEW field

6

MTH

CHAR4

Method – ’DIRE’ means direct

7

MINEID

I

Mininum VUHEXA identification number for this element

8

MAXEID

I

Maximum VUHEXA identification number for this element

9

MINGID

I

Minimum Grid identification number for this element

10

MAXGID

I

Maximum Grid identification number for this element

11

G(4)

I

Corner Grid identification numbers

12

ICORD

CHAR4

Flags for convective coordinate system – from PROJ and NORMAL fields

13

THETA

RS

Rotation of convective system

Record 5 – TETRAP(14300,143,14) Name

Word

Type

Description

1

EID

I

Element identification number

2

CID

I

Coordinate system identification number – from CID field

3

NX

I

View mesh subdivision – from VIEW field

4

NY

I

View mesh subdivision – from VIEW field

5

NZ

I

View mesh subdivision – from VIEW field

6

MTH

CHAR4

Method – ’DIRE’ means direct

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Data Block Descriptions O-V

Name

Word

Type

Description

7

MINEID

I

Mininum VUTETRA identification number for this element

8

MAXEID

I

Maximum VUTETRA identification number for this element

9

MINGID

I

Minimum Grid identification number for this element

10

MAXGID

I

Maximum Grid identification number for this element

11

G(4)

I

Corner Grid identification numbers

Record 6 - TRIAP(10400,104,15) Name

Word

Type

Description

1

EID

I

Element identification number

2

CID

I

Coordinate system identification number - from CID field

3

NX

I

View mesh subdivision - from VIEW field

4

NY

I

View mesh subdivision - from VIEW field

5

NZ

I

View mesh subdivision - from VIEW field

6

MTH

CHAR4

Method – ’DIRE’ means direct

7

MINEID

I

Mininum VUHEXA identification number for this element

8

MAXEID

I

Maximum VUHEXA identification number for this element

9

MINGID

I

Minimum Grid identification number for this element

10

MAXGID

I

Maximum Grid identification number for this element

11

G(3)

I

Corner Grid identification numbers

12

ICORD

CHAR4

Flags for convective coordinate system – from PROJ and NORMAL fields

13

THETA

RS

Rotation of convective system

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Record 7 – TRAILER Word 1

Name UNDEF(6 )

Type

Description

None

Notes: 1. For each of the three word headers: The first number is element type * 100; the second number is element type; and the third number is the number of words per element. 2. Items indicated as from field ’XXX’ refer to the OUTRCV Bulk Data entry.

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6

Glossaries

•

Data Block Glossary

•

Parameter Glossary

6.1 Data Block Glossary The Data Block Glossary lists the names and a brief description of all data blocks shown in the module descriptions in “Descriptions of DMAP Modules and Statements” . Naming conventions appear at the end of the glossary. Data Block Name

Parent Data Block Format

Description

A

Square matrix to be decomposed by DCMP, DECOMP, SOLVE, and SOLVIT. Rectangular matrix to be processed by the DIAGONAL and SCALAR modules. Rectangular matrix formed from partitions. Output by MERGE, UMERGE, and UMERGE1. Rectangular matrix to be used in MPYAD and SMPYAD module product. Rectangular matrix to be used in NORM module.

A2GG

Matrix defined on DMIG Bulk Data entries and referenced by the A2GG Case Control command. Output by MTRXIN.

ABESF*

Family of a-set size panel area matrices.

ACGRIDS

Column vector containing the grid IDs of the grids which are a part of the acoustic coupling; the grid IDs are represented as real values.

ACPT

Aerodynamic connection and property table. Output by APD.

ADBINDX

Table of the aerodynamic database contents. (one entry for each of the NV instances created). Output by ADG.

ADELX

Matrix of adjoint sensitivities. Output by DSADJ.

ADJG

Adjoint sensitivity displacement matrix in the g-set or p-set.

AEBGPDT*

BGPDT

Family of aerodynamic basic grid point definition tables. Output by APD.

AEBGPDTI

Basic grid point definition table for the aerodynamic js-set interference degrees-of-freedom.

AEBGPDTI*

Family of basic grid point definition tables for the interference js-set aerodynamic degrees-of-freedom.

AEBGPDTJ

Basic grid point definition table for the aerodynamic js-set degrees-of-freedom.

AEBGPDTJ*

Family of basic grid point definition tables for the js-set aerodynamic degrees-of-freedom.

AEBGPDTK

Basic grid point definition table for the aerodynamic ks-set degrees-of-freedom.

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

AEBGPDTK*

Family of basic grid point definition tables for the ks-set aerodynamic degrees-of-freedom.

AECMPOLD

Previously generated AECOMP.

AECOMP

Aerodynamic component definition table. Output by APD.

AECSTMHG

Table of aerodynamic coordinate system transformation matrices that only contains the hinge moment referenced coordinates systems if not null. Output by MKCNTRL.

AECTRL

Table of aerodynamic model’s control definition. Output by ADG.

AEDBIDX

Index table consisting of the triples. Output by MAKAEFS.

AEDBINDX

Aeroelastic database index for monitor point data.

AEDBUXV

Matrix of vehicle states.

AEDW

Matrix of downwash vectors contained on DMIJ Bulk Data entries referenced by the AEDW entries. Ouptut by MAKAEFA.

AEDWIDX

Index to the AEDW tables. Ouptut by MAKAEFA.

AEECT*

GEOM2

Family of aerodynamic element connection tables. Output by APD.

AEFIDX

Index to the AEFORCE tables. Ouptut by MAKAEFA.

AEFRC

Matrix of force vectors contained on DMIK Bulk data entries referenced by the AEFORCE entries. Ouptut by MAKAEFA.

AEGRID

BGPDT

Basic grid point definition tables for the aerodynamic model. Output by APD as BGPDT with qualifier MODLTYPE=’AEROMESH’.

AEIDW

Matrix of interference downwash vectors contained on DMIJ Bulk Data entries referenced by the AEDW entries. Ouptut by MAKAEFA.

AEIPRE

Matrix of interference pressure vectors contained on DMIJ Bulk data entries referenced by the AEPRESS entries. Ouptut by MAKAEFA.

AEMONOLD

Table of HM monitor points.

AEMONPT

Aerodynamic monitor point table. Output by MAKAEMON and MAKMON.

AEPRE

Matrix of pressure vectors contained on DMIJ Bulk data entries referenced by the AEPRESS entries. Ouptut by MAKAEFA.

AEPRSIDX

Index to the AEPRESS tables. Ouptut by MAKAEFA.

AERO

Table of control information for aerodynamic analysis. Output by APD.

AEROCOMP

Table of aerodynamic components when MESH=’AERO’. Output by MAKCOMP.

AEUSET*

USET

Family of aerodynamic USET tables. Output by APD.

AG0MAX

Column matrix of maximum values in each row of the AG0 matrix (usually derived using MATMOD option 6).

AGG

Fluid/structure coupling matrix at all points or for a structural panel. Output by GP5.

AGX

Gravity/thermal load matrix due to volumetric changes for the central, forward, or backward perturbed configuration. Output by SSG1.

AH

Signed global modally reduced area matrix

Aij

Matrix partitions. Output by PARTN and UPARTN.

6-2

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

AJJT

Aerodynamic influence matrix. Output by AMG.

ALBULK

Family of data blocks for bulk files for the original analysis/design model as well as for all auxiliary models, if any.

AM2

Damping matrix in the d-set for linear elements multiplied by the negative of the time step delta

AM3

Combined mass and damping matrix multiplied the square of the reciprocal of the time step delta and the reciprocal of twice the time step delta, respectively.

AMAT

State-space [A] matrix for superelement.

AMLIST

List of auxiliary model identification numbers. Output by AXMPR1.

AMSPLINE

Table of aerodynamic splines for display. Converted from forces and pressures computed on AEBGPDT grid points, (box centroidal points) to AEGRID grid points (box corner points). Output by APD.

ANORM

Normalized matrix. Output by NORM.

APART

Partitioning vector for panel coupling matrix when PNLPTV=TRUE.

APC

Absolute panel contributions results matrix.

APL

Lower triangular factor of null space A matrix.

APU

Upper triangular factor of null space A matrix.

AUG1

Displacement matrix in g-set for aerostatic analysis. Output by DSAD.

AUTO

Autocorrelation function table. Output by RANDOM.

AUXTAB

Table of aerodynamic extra point identification numbers, displacements, labels, type, status, position and hinge moments for all subcases.

AXIC

Table of Bulk Data entry images related to conical shell, hydro elastic, and acoustic cavity analysis. Output by IFP.

Data Block Name

Parent Data Block Format

Description

B

Output matrix from the DIAGONAL module. Right hand side of a system of equations input to the FBS, SOLVE, and SOLVIT modules. Rectangular matrix to be used in MPYAD and SMPYAD module product.

B2DD

Total damping matrix from viscous damping elements and the B2PP Case Control command and reduced to the d-set. In transient response analysis, B2DD may also include structural damping effects.

B2GG

Matrix defined on DMIG Bulk Data entries and referenced by the B2GG Case Control command. Output by MTRXIN.

B2PP

Matrix defined on DMIG Bulk Data entries and referenced by the B2PP Case Control command. Output by MTRXIN.

BAA

Viscous damping matrix in a-set or d-set.

BACK

Transformation matrix from cyclic to physical components. Required in static and pre-buckling analysis only. Output by CYCLIC1.

BASVEC

Auxiliary displacement matrix.

BASVEC0

Auxiliary displacement matrix. Optional user input.

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Data Block Name

Glossaries

Parent Data Block Format

Description

BCON0

Table of constant terms in the beam section constraint relationship. Output by DOPR1.

BCONXI

Matrix relating beam library constraints to the independent design variables. Output by DOPR1.

BCONXT

Matrix transpose of BCONXI.

BD3X3

3x3 diagonal strip for boundary degrees-of-freedom from KGG for parallel domain decomposition. Output by GPSP.

BDD

Damping (or heat capacitance) matrix for the d-set for linear elements only.

BDIAG

Diagonal matrix of buckling divided by buckling generalized differential stiffness matrix. Output by DSAH.

BDPOOL

Hydroelastic boundary matrices in DMIG Bulk Data entry format. Output by BMG.

BDICT

KDICT

BELM dictionary table. Output by EMG.

BELM

KELM

Table of element damping or heat capacity matrices. Output by EMG.

BFHH

Fluid partition of modal damping matrix BHH.

BGPDT*

BGPDT

Family of basic grid point definition tables for all superelements.

BGPDT

BGPDT

Basic grid point definition table. Output by GP1.

BGPDTD

BGPDT

Basic grid point definition table for a downstream superelement.

BGPDTM

BGPDT

Basic grid point definition table and updated for the current p-level. Output by GP1 with GEOM1M and GEOM2M as inputs.

BGPDTN

BGPDT

New BGPDT table based on displaced grid locations. Output by MATMOD option 11.

BGPDTS

BGPDT

Basic grid point definition table for a superelement. Output by GP1.

BGPDTX

BGPDT

BGPDT assembled for superelements defined on the SEPLOT or SEUPPLOT command. Output by SEPLOT.

BGPDVB

BGPDT

Basic grid point definition table for the backward perturbed configuration. Output by DSAM.

BGPDVP

BGPDT

Basic grid point definition table for the forward (or central) perturbed configuration. Output by DSAM.

BGPDVX

BGPDT

Basic grid point definition table for the central, forward, or backward perturbed configuration. Output by DSAM.

BGPECT

GEOM2

Boundary grid point element connection table. Output by BGP.

BHH

Generalized (modal) damping matrix

BHH1

Modified generalized (modal) damping matrix. Output by FA1.

BIN

Results from bolt preload phase.

BKDICT

KDICT

BKK

BKELM dictionary table. Viscous damping matrix in cyclic components. Output by CYCLIC3.

BLAMA

LAMA

Buckling eigenvalue summary table. Output by READ.

BLAMA*

LAMA

Family of buckling eigenvalue summary tables.

BMAT

6-4

State-space [B] matrix for superelement.

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

BNDFIL

Table containing the local and global boundary grids in the order given by extreme for domain decomposition. Output by SEQP.

BNFDAT

Bolt element grid point force data.

BOLTFOR

List of element numbers and bolt force for SDRX.

BOUT

Results from bolt preload phase.

BP

Null space B matrix.

BRDD

Damping matrix in the d-set for linear elements only or heat capacitance matrix for both linear and nonlinear elements in the d-set.

BTOPO

Contact regions topological information table. Output by BGP.

BTOPOCNV

Updated contact regions input information table. Output by NLITER and NLTRD2.

BTOPOSTF

Updated contact regions topological information table. Output by NLITER and NLTRD2.

BXX

Viscous damping matrix in any set. Usually h-set or d-set in CEAD, FRRD1, FRRD2, TRD1, and TRD2.

BUG*

Family of buckling eigenvector matrices in the g-set

BUX

Matrix of damping multiplied by displacement or eigenvectors.

BULK

Table of all Bulk Data entries. Output by XSORT.

BULK*

Family of auxiliary model or superelement Bulk Data sections.

BULKOLD

BULK table from a prior run.

Data Block Name

Parent Data Block Format

Description Rectangular matrix to be used in MPYAD module addition and SMPYAD module product.

C CASADJ

CASECC

Case Control table associated with adjoint method. Output by DSAD.

CASDSN

CASECC

Case Control table with unneeded analysis subcase(s) deleted, excluding static aeroelastic subcases. Output by DSAD.

CASDSX

CASECC

Case Control table with unneeded analysis subcase deleted

CASE

CASECC

Table of Case Control commands for the current analysis type and superelement.

CASEA

CASECC

A single record (subcase) of CASECC for aerodynamic analysis. Output by AELOOP.

CASEBK

CASECC

Case Control table for cyclic data recovery. One record for every column in BACK. Required in static and pre-buckling analysis only. Output by CYCLIC1.

CASEBUCK

CASECC

Case Control table for buckling analysis and based on ANALYSIS=BUCK. Output by MDCASE.

CASECC

CASECC

Table of Case Control command images. Output by IFP1.

CASECC*

CASECC

Family of auxiliary model Case Control tables.

CASECC1

CASECC

Primary model Case Control table appended with extra subcases to account for the boundary shapes. Output by SHPCAS.

CASECCBO

CASECC

Updated CASECC for contact region data recovery operations. Output by BGCASO.

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Glossaries

Data Block Name

Parent Data Block Format

Description

CASECCR

CASECC

Table of Case Control command images for data recovery. Output by TOLAPP. Case Control table for modal or direct complex eigenvalue analysis and based on ANALYSIS=MCEIG or DCEIG. Output by MDCASE.

CASECEIG

CASEDR

CASECC

Table of Case Control command images for the superelement (identification number equal to output value of SEID). Output by SEDR.

CASEDS

CASECC

Case control table for the data recovery of design responses. Output by DOPR3 and DSTA.

CASEDSF

CASECC

Case Control table for all load cases and all design variables for the perturbed configuration. Output by DSAH.

CASEDVRG

CASECC

Case Control table for aerostatic divergence analysis and based on ANALYSIS=DIVERG. Output by MDCASE.

CASEFLUT

CASECC

Case Control table for flutter and based on ANALYSIS=FLUTTER. Output by MDCASE.

CASEFR

CASECC

Updated Case Control table for static loads generation and solution in cyclic symmetry analysis. One record for every distinct load set identification number. Output by CYCLIC1.

CASEFREQ

CASECC

Case Control table for modal or direct frequency response analysis and based on ANALYSIS=MFREQ or DFREQ. Output by MDCASE.

CASEG

CASECC

Table of Case Control command images for current subcase.

CASEHEAT

CASECC

Case Control table for heat transfer analysis and based on ANALYSIS=HEAT. Output by MDCASE.

CASEMODE

CASECC

Case Control table for normal modes analysis and based on ANALYSIS=MODES. Output by MDCASE.

CASEMTRN

CASECC

Case Control table for modal transient analysis and based on ANALYSIS=MTRAN. Output by MDCASE.

CASEP

CASECC

Residual superelement Case Control table for plotting basis vectors. Output by DOPR2. Case Control table with number of basis vectors in the DESVEC as the number of Case Control records. Output by DSAJ.

CASERS

CASECC

Case Control table for the residual structure and a given analysis type.

CASES

CASECC

Table of Case Control command images for the current superelement (identification number equal to output value of SEID). Output by SEP2CT.

CASESADV

CASECC

Combined Case Control table which includes CASESAER or CASEDVRG. Output by MDCASE.

CASESAER

CASECC

Case Control table for aerostatic analysis and based on ANALYSIS=SAERO. Output by MDCASE.

CASESMEM

CASECC

Case Control table for electromagnetic analysis and based on ANALYSIS=ELEC. Output by MDCASE.

CASESMST

CASECC

Case Control table for structural analysis and based on ANALYSIS=STRU. Output by MDCASE.

CASESNMB

CASECC

Combined Case Control table which includes CASESTAT, CASEMODE, CASEBUCK, CASESAER, CASEDVRG, and CASEFLUT. Output by MDCASE.

CASESTAT

CASECC

Case Control table for static analysis and based on ANALYSIS=STATICS. Output by MDCASE.

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

CASESX

CASECC

Expanded Case Control table. Output by LCGEN.

CASEXX

CASECC

Case Control table intended for Phase 1 matrix generation, assembly and reduction. Output by MDCASE.

CASEUPSE

CASECC

Case Control table for upstream superelements only. Output by MDCASE.

CASEVEC

CASECC

Table of Case Control command images with the PARTN command referencing all of auxiliary model’s grid identification numbers. Output by AXMPR2.

CASEXX

CASECC

Subset of CASECC for current loop. Output by CASE.

CASEYY

CASECC

Appended Case Control table in flutter analysis. Output by FA2.

CDELB

Triple matrix product for flutter damping sensitivity

CDELK

Triple matrix product for flutter stiffness sensitivity

CDELM

Triple matrix product for flutter mass sensitivity

CFSAB

Matrix of spectral densities–weighting factors for RMS calculations. Output by DOPRAN.

CIDATA

Miscellaneous data for controlled increment method. Output by NLITER.

CLAMA

LAMA

Complex eigenvalue summary table. Output by CEAD.

CLAMA1

LAMA

Complex eigenvalue summary table in flutter analysis. Output by CEAD.

CLAMA2

LAMA

Appended complex eigenvalue summary table in flutter analysis. Output by FA2.

CLAMMAT

Diagonal matrix with complex eigenvalues on the diagonal. Output by CEAD, LAMX, and UEIGL.

CMAT

State-space [C] matrix for superelement.

CNELM

Contact element definition table.

CNTABR

CONTAB

Table of retained constraint attributes. Output by DSAD.

CNTABRG

CONTAB

Table of retained constraint attributes.

CNVTST

Convergence test matrix.

COELEM

Correlation table between idcid/eid/component for element responses. Output by DSAH.

COGRID

Correlation table between idcid/gid component for displacement responses. Output by DSAH.

COMP

Merged table of components. Output by MRGCOMP.

COMPEST

Composite solid element summary table.

COMPi

Table of aerodynamic or structural components

CON

Matrix of constants that relates design variables and design coordinates. Output by DOPR2.

CONS1T

Matrix transpose of relationship between dependent and independent design variables. Output by DOPR1.

CONSBL

Matrix of constant property values. Output by DOPR1.

CONSBL*

Family of matrices of constant property values. Output by DOPR1.

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Chapter 6

Glossaries

Data Block Name

Parent Data Block Format

Description

CONTAB

CONTAB

Table of constraint attributes. Output by DOPR3.

CONTACT

Table of Bulk Data entries related to contact regions. Output by IFP.

CONTROL

Table of editing directives for the TABEDIT module.

COORD

Matrix of initial or final designed coordinate values, COORDO or COORDN.

COORDN

Updated (optimized) COORDO. Output by DOM11.

COORDO

Matrix of initial designed coordinate values at the beginning of each design cycle. Output by DOPR2.

CP

Column partitioning vector. Output by VEC and MATMOD option 17.

CPH1

Complex eigenvector matrix for h-set in flutter analysis. Output by CEAD.

CPH2

Appended complex eigenvector matrix for h-set in flutter analysis. Output by FA2.

CPHFL

Left flutter eigenvector - h-set. Output by DSFLTE.

CPHP

Complex eigenvector matrix in the p-set.

CPHFR

Left flutter eigenvector - h-set. Output by DSFLTE.

CPHX

Complex eigenvector matrix in the d-set or h-set. Output by CEAD.

CPHL

Complex eigenvector matrix in the l-set. Output by CEAD.

CSNMB

CASECC

Case Control table for a given superelement and all analysis types.

CSTM

CSTM

Table of coordinate system transformation matrices. Output by GP1.

CSTMi

CSTM

Tables of coordinate system transformation matrices; either aerodynamic or structural.

CSTM0

CSTM

Table of coordinate system transformation matrices for the residual structure.

CSTMA

CSTM

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points. Output by APD.

CSTMD

CSTM

Table of coordinate system transformation matrices for a downstream superelement.

CSTMM

CSTM

Merged table of coordinate system transformation matrices. Output by MKCSTMA.

CSTMS

CSTM

Table of coordinate system transformation matrices for a superelement.

CVAL

Matrix of constraint values, CVALO or CVALRG.

CVALO

Matrix of final (optimized) constraint values. Output by DOM9.

CVAL

Matrix of retained constraint values. Output by DSAD.

CVALR

Matrix of retained constraint values. Output by DSAD.

CVALRG

Matrix of initial constraint values.

CVEC

Partitioning vector for separating the primary model solutions from boundary shape induced solutions. Output by SHPCAS.

CVECT

Load combination factor matrix. Output by PCOMB.

CYCD

Table of constraints in harmonic components. Output by CYCLIC2.

6-8

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

D

Rectangular matrix to be used in SMPYAD module product. Diagonal matrix extracted from LD. Output by MATMOD option 21.

D1JE

Real part of downwash matrix due to extra points.

D1JK

Real part of downwash matrix. Output by AMG.

D2JE

Imaginary part of downwash matrix due to extra points.

D2JK

Imaginary part of downwash matrix. Output by AMG.

DAR

Rigid body transformation matrix for the r-set to the a-set. Formed from the merge of DM and an l-set size identity matrix.

DBCOPT

DBCOPT

Design optimization history table for post-processing. Output by DOM12.

DB

Data block.

DBi

Data block to be processed by the DBC, INPUTT2, and OUTPUT2 modules. Data blocks to be compared in the RESTART module. Data block declared on the FILE statement. Data block to be purged by PURGEX module.

DBMLIB

Table of designed beam library data. Output by DOPR1.

DBMLIBU

Modified DBMLIB data block updated for current values of designed PBARL/PBEAML dimensions.

DBNAME

Data block for ’NAME’ option of PARAML module. Output by PARAML.

DBP

Primary data block.

DBS

Secondary data block. Output by EQUIVX.

DBUG

Buckling eigenvector matrix in the g-set associated with designed (active) eigenvalues. Output by DSAH.

DCLDXT

Matrix of coefficients in the grid to design variable relationship. Output by DOPR2.

DCPHL

Complex eigenvectors associated with the divergence eigenvalues extracted from the real part of eigenvectors associated with the divergence eigenvalues. Output by CEAD.

DEFUSET

Table of DEFUSET Bulk Data entry images. Output by IFP.

DELB1

Matrix of delta buckling load factor for all design variables.

DELBSH

Matrix of finite difference shape step sizes.

DELBSX

Updated DELBSH where the numerical zero terms are replaced by a prescribed small value. Output by DOPR5.

DELCE

Matrix of delta complex eigenvalue for all design variables

DELDV

Matrix of divergence sensitivity. Output by DSDVRG.

DELF1

Matrix of delta eigenvalue for all design variables.

DELFL

Matrix of delta flutter responses for all design variables. Output by DSFLTF.

DELS

Matrix of delta stability derivative responses for all design variables.

DELS1

Matrix of delta stability derivative responses for all design variables for a single trim subcase. Output by DSARSN.

DELTGM

Multipoint constraint transformation matrix for the perturbed configuration. Output by DSVGP4.

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

DELVS

Matrix of delta volume for all design variables. Output by DSAW.

DELWS

Matrix of delta weight for all design variables. Output by DSAW.

DELX

Matrix of delta trim variable responses for all design variables.

DELX1

Matrix of delta trim variable responses for all design variables for a single trim subcase. Output by DSARSN.

DEQATN

Table of DEQATN Bulk Data entry images. Output by IFP.

DEQIND

Index table to DEQATN data block. Output by IFP.

DESELM

Table of designed elements. Output by DOPR3.

DESGID

Table of designed grid coordinate attributes. Output by DOPR2.

DESNEW

Update table of design variable attributes. Output by DOM12.

DESTAB

DESTAB

Table of design variable attributes. Output by DOPR1.

DESVCP

Global shape basis vector matrix with incorporation of DLINK relations with extra columns for property/dummy variables. Output by DOPR2.

DESVEC

Basis vector matrix which consists of basis vectors generated from DVGRID Bulk Data entries and from columns of BASVEC0 matrix. Its components are defined in the basic coordinate system.

DESVECP

Basis vector matrix which consists of basis vectors generated from DVGRID bulk data entries and from columns of BASVEC0 matrix its components are expressed in the global coordinate system.

DFFDNF

Table containing the derivatives of forcing frequencies with respect to natural frequencies. Output by FRLGEN.

DFRFNC

Table of frequency functions records (see bulk data input DTI,DFRFNC).

DGEOM2

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points for the perturbed configuration. Output by DSAH.

DGEOM3

GEOM3

Table of Bulk Data entry images related to static loads for the perturbed configuration. Output by DSAH.

DGTAB

Table relating DTOS4 records and designed grid data. Correlation table of internal grid sequence for the baseline and perturbed configuration. Output by DOPR6.

DISTAB

Table of discrete optimization value sets. Output by DOPR1.

DIT

DIT

Table of TABLEij Bulk Data entry images. Output by IFP.

DITID

Table of identification numbers in DIT. Output by TA1.

DITN

Direct input tables with modified TABLEDi for updated values of designed frequency dependent properties.

DIVDAT

Table of divergence data. Output by DIVERG.

DIVTAB

Table of aerostatic divergence data for all subcases.

DJX

Downwash matrix. Downwash at the j-point due to the x aerodynamic extra point. Output by ADG.

DLCPHL

Left-handed complex eigenvectors associated with the divergence eigenvalues extracted from the real part of left-handed eigenvectors associated with the divergence eigenvalues. Output by DIVERG.

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

DLSTIN

List of data blocks and their paths. Output in a previous execution of RESTART.

DLSTOUT

List of data blocks and their paths. Output by RESTART.

DLT

Table of dynamic loads. Output by DPD.

DLT1

Table of dynamic loads updated for nonlinear analysis. Output by NLCOMB.

DLTH

Table of dynamic loads updated for heat transfer analysis. Output by TRLG.

DM

Rigid body transformation matrix for the r-set to the l-set. Output by RBMG3.

DMATCK

Table of designed material consistency check. Output by DOPR1.

DMI

Table of all matrices specified on DMI Bulk Data entries. Output by IFP.

DMIi

Matrix data blocks created from DMI. Output by DMIIN.

DMINDX

Index into DMI. Output by IFP.

DNODEL

Table of designed and non-designed locations. Output by DOPR2.

DPHG

Normal modes eigenvector matrix in the g-set associated with designed (active) eigenvalues. Output by DSAH.

DPLDXI

Matrix of coefficients in the property to independent design variable relationship. Output by DOPR1.

DPLDXI*

Family of matrices of coefficients in the property to independent design variable relationship. Output by DOPR1.

DPLDXT

Matrix transpose of DPLDXI.

DRDUG

Matrix of adjoint loads for the g-set. Output by DSAD.

DRDUTB

Table of adjoint load attributes. Output by DSAD.

DRLIST

Superelement processing list for data recovery. Output by SEP4.

DRMSVL

Table of the RMS response values with respect to the design variables. Output by DSAMRG.

DRSTBL

Table containing the number of retained responses for each subcase for each of the response types. Output by DSAD.

DRSTBLG

Table containing the number of retained responses for each subcase for each of the response types.

DSCM

Design sensitivity coefficient matrix. Output by DSAL.

DSCM2

Normalized design sensitivity coefficient matrix. Output by DOM6.

DSCMCOL

DCSMCOL

Correlation table for normalized design sensitivity coefficient matrix. Output by DSTAP2.

DSCMG

Unnormalized design sensitivity matrix.

DSCMR

Old combined design sensitivity/constraint matrix. Output by DSMA.

DSCOLL

Table of design sensitivity column labels for design sensitivity matrix, DSCMR. Output by DSTA.

DSCREN

Table of constants from the DSCREEN Bulk Data entry. Output by DOPR1.

DSDIV

Matrix of delta divergence speed for all design variables.

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

DSEDV

Partitioning vector for retained divergence responses. Output by DSAH.

DSEGM

Old design sensitivity eigenvalue gradient matrix.

DSESM

Design sensitivity eigenvector selection matrix - Boolean operator to select eigenvectors which are referenced by constraints (buckling and normal modes only). Output by DSTA.

DSIDLBL

Table of design response labels. Output by DSTAP2.

DSLIST

Superelement processing list to direct the pseudo-load and response sensitivity calculations. Output by SDSB.

DSPT1

Design sensitivity processing table. Output by DSAN and DSTA.

DSPT2

Old Design sensitivity processor table two. Output by DSTA.

DSROWL

Table of design sensitivity row labels for design sensitivity matrix, DSCMR. Output by DSTA.

DSTABR

Matrix of restrained perturbed dimensional stability derivatives.

DSTABU

Matrix of unrestrained perturbed dimensional stability derivatives.

DTB

Table of constants from the DTABLE Bulk Data entry. Output by DOPR1.

DTI

Table of all matrices specified on DTI Bulk Data entries. Output by IFP.

DTIi

Table data blocks created from DTI. Output by DTIIN.

DTINDX

Index into DTI. Output by IFP.

DTOS2

Design variable/property cross reference table. Same as DTOS2K except that the PREF in each entry is the product of a DPLDXI element and the corresponding design variable value. Output by DOPR5.

DTOS2*

Family of tables which are the same as DTOS2K* except that the PREF in each entry is the product of a DPLDXI element and the corresponding design variable value. Output by DOPR5.

DTOS2J

Table identifying independent design variables and property values. Output by DOPR1.

DTOS2J*

Family of tables identifying independent design variables and property. Output by DOPR1.

DTOS2K

Same as DTOS2J except that the dvid in each entry refers to the position of an internal design variable ID in the first TABDEQ record. Output by DOPR4.

DTOS2K*

Family of tables which are the same as DTOS2J* except that the dvid in each entry refers to the position of an internal design variable ID in the first TABDEQ record. Output by DOPR4.

DTOS4

Table relating design variable to grid perturbation. Same as DTOS4K except that the last three words in each entry contains the product of those in DTOS4K and the shape step size. Output by DOPR5.

DTOS4J

Designed grid perturbation vector in basic coordinate system. Output by DOPR2.

DTOS4K

Same as DTOS4J except that the ID in each five-word entry is the position of an internal design variable ID in the first TABDEQ record. Output by DOPR4.

DUGNI

Incremental displacement matrix between the last two converged steps. Output by NLITER.

6-12

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

DUX

Matrix of aerodynamic extra point displacements for the perturbed configuration. Output by ASG.

DVIDS

List of shape variable identification numbers to be used for the boundary DVGRID option. Output by DSAJ.

DVPTAB

DVPTAB

Table of attributes of the designed properties by internal property identification number order. Output by DOPR1.

DVPTAB*

DVPTAB

Family of tables of attributes of the designed properties by internal property identification number order. Output by DOPR1.

DVSLIS

List of design variables affected by shape variations. Output by DSVGP4.

DXDXI

Matrix relating linked and independent design variables. Output by DOPR1.

DXDXIT

Matrix transpose of DXDXI.

DYNAMIC

DYNAMIC

Table of Bulk Data entry images related to dynamics. Output by IFP. Table of Bulk Data entry images related to dynamics without DAREA entry images. Output by GP1.

DYNAMICB

DYNAMICS

DYNAMIC

Table of Bulk Data entry images related to dynamics for the current superelement. Output by SEP2 and SEP2X.

Data Block Name

Parent Data Block Format

Description

E

Rectangular matrix to be used in SMPYAD module product.

ECT

GEOM2

Element connectivity table. Output by GP2.

ECT*

GEOM2

Family of element connectivity tables for all superelements.

ECTA

GEOM2

Secondary element connectivity table. Output by GP2.

EDITVEC

Vector with zeros in rows to be removed under usetop=’filter’.

EDOM

Table of Bulk Data entries related to design sensitivity and optimization. Output by IFP.

EDOM*

Family of EDOM tables for all superelements.

EDOMM

Table of Bulk Data entries related to design sensitivity and optimization updated for p-element analysis. Output by OPTGP0.

EDOMS

Table of Bulk Data entries related to design sensitivity and optimization for a superelement. Output by SDSA.

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 and SET3 entries. Output by IFP.

EED

DYNAMIC

Table of eigenvalue extraction parameters. Output by DPD.

EFILL

Element fill ratio.

EGK

Pseudo-load (equilibrium variation) matrix in the g-set due to stiffness. Output by DSVG1P.

EGM

Pseudo-load (equilibrium variation) matrix in the g-set due to mass. Output by DSVG1P.

DMAP Programmer’s Guide

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Chapter 6

Glossaries

Data Block Name

Parent Data Block Format

Description

EGPSF

EGPSF

Table of element to grid point interpolation factors. Output by GPSTR1.

EGPSTR

EGPSTR

Table of grid point stresses or strains for post-processing in the DBC module. Output by GPSTR2.

EGTX

Pseudo-load matrix (variation in equilibrium) due to changes in the thermal load/design variables for the central, forward, or backward perturbed configuration. Output by DSVG2.

EGX

Pseudo-load (equilibrium variation) matrix in the g-set due to stiffness, mass, viscous damping or structural damping. Output by DSVG1P.

EHT

Element hierarchical table for p-element analysis. Output by GP0.

EHTA

Secondary element hierarchical table. Output by GP0.

ELDATA

Table of combined nonlinear information data. Output by NLCOMB.

ELDCT

ELDCT

Table of element stress discontinuities for post-processing in the DBC module. Output by STDCON.

ELEMVOL

Element volume table, contains p-element volumes and the p-value dependencies of each P-element grid, edge, face and body. Output by VIEWP.

ELGNST

Table of glue element stiffness.

ELSET

Table of element sets defined in OUTPUT(POST) or SETS DEFINITION section of Case Control. Output by PLTSET and SEPLOT.

EMAT

State-space [E] matrix for superelement.

EMM

Effective mass matrix. Output by EFFMAS.

EMVD

Equivalent modal viscous damping matrix for superelement.

EPSSE

Table of epsilon and external work. Output by SSG3, SOLVIT, and DISUTIL.

EPT

EPT

Table of Bulk Data entry images related to element properties. Output by IFP and IFP6.

EPTA

EPT

Secondary table of Bulk Data entry images related to element properties.

EPTC

EPT

Copy of EPT except PCOMP records are replaced by equivalent PSHELL records. Output by IFP6, CMPZPR, and DSTA.

EPTN

EPT

Updated (optimized) EPT. Output by DOM11.

EPTS

EPT

Table of Bulk Data entry images related to element properties for a superelement. Output by SEP2 and SEP2X.

EPTTAB

EPT

Table of designed property attributes. Output by DOPR1.

EPTTAB*

EPT

Family of tables of designed property attributes. Output by DOPR1.

EPT

EPT with design variable perturbations. Output by DSABO. Copy of EPT except PBCOMP records are replaced by equivalent PBEAM records. Output by IFP7. Copy of EPT except PBARL and PBEAML records are replaced by equivalent PBAR and PBEAM records. Output by IFP9. Copy of EPT except PACABS and PACABR entries are updated with TABLEij references.

EPTX

Equivalence table between internal fluid grid points and internal structural grid points which lie on the fluid/structure boundary. Output by GP5.

EQACST

EQDYN

6-14

EQEXIN

DMAP Programmer’s Guide

Equivalence table between external and internal grid/scalar/extra point identification numbers. (EQEXIN appended with extra point data). Output by DPD.

Glossaries

Data Block Name

Parent Data Block Format

Description

EQEXIN

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers. OUTPUT by GP1.

EQEXINS

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers for a superelement. Output by SEP2 and SEP2X.

EQMAP

Table of degree-of-freedom global-to-local maps for domain decomposition. Output by PRESOL.

ERHM

Matrix of dimensional unsplined restrained elastic hinge moment data

ERROR0

ERROR

Error estimate table generated by ADAPT module in previous superelement or adaptivity loop.

ERROR1

ERROR

Error-estimate table updated for current superelement or adaptivity loop. Output by ADAPT.

EST

Element summary table. Output by TA1.

ESTDATA

Table of superelement estimation data overrides. Output by DTIIN.

ESTL

Linear element summary table. Output by TA1.

ESTDCN

Element summary table which incorporates combined constraints and design variables. Output by DSAF and DSTA.

ESTDV2

Merged EST with grid and element property design variable perturbations. If CDIF=’YES’ then this is the forward perturbation. Output by DSAE.

ESTDVB

Element summary table for the backward perturbed configuration. Required only if CDIF=’YES’.

ESTDVM

EST

EST with updated material property identification numbers. Output by DSABO.

ESTDVP

EST with element property design variable perturbations. Output by DSABO and DSTA.

ESTDVS

EST with grid design variable perturbations. Output by DOPR6.

ESTF

Element summary table for follower force stiffness. Output by TAFF.

ESTNL

Nonlinear element summary table. Output by TA1.

ESTNL1

Nonlinear element summary table updated for heat transfer analysis. Output by TAHT.

ESTNLH

Nonlinear element summary table at converged step. Output by NLITER, NLTRD, and NLTRD2.

ESTR

EST table with reduced records. Output by MATMOD option 38.

ETT

Element temperature table. Output by GP3.

ETTDCN

Table of design variable and constraint internal identification numbers for the effects of temperature. Output by DSAF and DSTA.

ETTDV

Element temperature table where the original element identification numbers have been converted to new design variable identification numbers. Output by DSAN and DSTA.

EUHM

Matrix of dimensional unsplined unrestrained elastic hinge moment data.

DMAP Programmer’s Guide

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

F

Rectangular matrix to be used in SMPYAD module addition.

FENL

Strain energy and grid point force at every element from the previous load step in nonlinear matrix format.

FENL1

Strain energy and grid point force at every element at the current load step in nonlinear matrix format. Output by NLITER.

FFAJ

Matrix of pressures at aerodynamic boxes.

FFGH

Follower force for OLOAD output. Output by NLITER.

FG

Element forces due to large displacements. Output by GNFM.

FGNL

Nonlinear element force matrix from the last iteration. Output by NLITER.

FLUTAB

Flutter summary table for all subcases.

FMPF

Matrix of fluid mode participation factors. Output by MODEPF.

FN

Matrix of natural frequencies (mass normalized stiffness).

FOL

FOL

Frequency response frequency output list. Output by FRLG.

FOL1

FOL

Frequency response frequency output list truncated by the OFREQ Case Control command. Output by MODACC. Matrix of frequencies in radian units. Output by MATMOD Option 33.

FOLMAT FOLT

FOL

Frequency response frequency output list with first frequency truncated if first frequency is zero. UXF is also similarly truncated. Output by FRRD1 or FRRD2.

FORCE

Table of MSGSTRESS plotting commands defined under the OUTPUT(CARDS) section in CASE CONTROL and MSGMESH field information. Output by IFP1.

FORE

Transformation matrix from physical to cyclic components. Output by CYCLIC1.

FREQMASS

Matrix of frequencies and generalized masses.

FRL

Frequency response list. Output by FRLGEN.

FRLF

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list. Output by FRLG, TRLG, CEAD, and READ. However, with Version 6.0, for frequency response, this is no longer the same as the previous OL data block, but is now the full data block for the frequency sets data for the current cycle, together with a header record listing the frequency sets.

FRLTMP

A composite FRL data block containing only the relevant records from each FRL data block in multiple subcase, multiple frequency set, frequency response analysis, relevant when the PRESENS3 parameter is TRUE.

FRL1

Frequency response list for the current processor if distributed processing is requested. Output by FRLGEN.

FRLI

Frequency response list for a single frequency. Output by FRQDRV.

FRQDPV

Table of frequencies matching the perturbed elements summary table (ESTDV) when frequency dependent properties are designed.

FRQRMF

FRQRPR table for frequency response.

FRQRSP

Table of the count of type 1 frequency/time responses per response type per frequency or time step. Output by DOPR3.

FRQRPR

Table containing the number of first level (direct) retained responses per response type and per frequency or time step. Output by DSAD.

6-16

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

FRQRPRG

Table containing the number of first level (direct) retained responses per response type and per frequency or time step.

FSAVE

Flutter storage save or answer table. Output by FA1.

Data Block Name

Parent Data Block Format

Description

GAMMAD

Complex double precision. This is the scalar multiplier for [C].

GAOSM

Constraint matrix relating the a-set to the (o+s+m)-set for superelement.

GAPAR

Partitioning vector which is used to partition the local a-set displacements from the global a-set displacements. It contains a 1 at each row that does not have a contribution from the current processor and zero if it does. Required only for geometric domain decomp.

GC

Transformations matrix between symmetric (cosine) components and solution set components. Output by CYCLIC3.

GDGK

Aerodynamic transformation matrix for displacements from the k-set to g-set. Output by GI.

GDKI

Aerodynamic transformation matrix for displacements from the k-set to h-set.

GDNTAB

Table of grid points generated for p-element analysis. Output by GP0.

GEG

Element displacement interpolation matrix. Output by MGEN.

GEI

Table of general element data. Output by TA1.

GEOM1

GEOM1

Table of Bulk Data entry images related to geometry. Output by IFP.

GEOM1*

GEOM1

Family of GEOM1 tables for all partitioned superelements defined in separate Bulk Data sections.

GEOM1A

GEOM1

Table of Bulk Data entry images related to geometry and assigned to an auxiliary model. Output by IFP.

GEOM1C

GEOM1

Table of Bulk Data entry images related to geometry and merged from GEOM1 and GEOM1A. Output by AXMPR2.

GEOM1EX

GEOM1

GEOM1 table containing records which define an external superelement. Specifically, it contains CORD1j, CORD2j, EXTRN, and GRID Bulk Data records. Output by BDRYINFO.

GEOM1EXA

GEOM1

GEOM1 table containing all geometry definitions of an external superelement.

GEOM1M

GEOM1

Table of Bulk Data entry images related to geometry and updated for the current p-level. Output by GP0.

GEOM1N

GEOM1

Updated (optimized) GEOM1. Output by DOM11. Modified GEOM1 with CORD1j records converted to CORD2j records. Output by SECONVRT.

GEOM1P

GEOM1

Table of Bulk Data entry images related to geometry updated for p-elements and superelements. Output by MODGDN.

GEOM1Q

GEOM1

Same as GEOM1 except SEQGP Bulk Data entry records have been added and any pre-existing SEQGP records are removed. Output by SEQP. GEOM1 table with reduced GRID record. Output by MATMOD option 36.

GEOM1R GEOM1S

GEOM1

Table of Bulk Data entry images related to geometry for the current superelement. Output by SEP2 and SEP2X.

DMAP Programmer’s Guide

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Chapter 6

Glossaries

Data Block Name

Parent Data Block Format

Description

GEOM1VU

GEOM1

Table of Bulk Data entry images related to geometry with view-grids added. Output by VIEWP.

GEOM1X

GEOM1

GEOM1 table related to axisymmetric conical shell, hydroelastic, and acoustic cavity analysis. Output by IFP3, IFP4, and IFP5. GEOM1 table related to axisymmetric conical shell, hydroelastic, acoustic cavity, and spot weld element analysis. Output by MODGM2.

GEOM2

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points. Output by IFP.

GEOM2*

GEOM2

Family of GEOM2 tables for all partitioned superelements defined in separate Bulk Data sections.

GEOM2A

GEOM2

Table of secondary Bulk Data entry images related to element connectivity and updated for the current p-level. Output by GP0.

GEOM2EX

GEOM2

GEOM2 table containing records which define an external superelement. Specifically, it PLOTEL and SPOINT Bulk Data records. Output by BDRYINFO.

GEOM2EXA

GEOM2

GEOM2 table containing all element connectivity of an external superelement.

GEOM2M

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points and updated for the current p-level. Output by GP0.

GEOM2N

GEOM2

Updated (optimized) GEOM2. Output by DOM11. Modified GEOM2 with GO replaced by X1, X2, and X3 on CBAR, CBEAM, CBEND, CBUSH and CGAP records. Output by SECONVRT. GEOM2 table with reduced element record. Output by MATMOD option 37.

GEOM2R GEOM2S

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points for the current superelement. Output by SEP2 and SEP2X.

GEOM2VU

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points p-elements removed and view-elements added. Output by VIEWP.

GEOM2X

GEOM2

GEOM2 table related to axisymmetric conical shell, hydroelastic, and acoustic cavity analysis. Output by IFP3, IFP4, and IFP5. GEOM2 table augmented with fluid data and SPOINTS if ACMS=’YES’. Output by SEQP.

GEOM3

GEOM3

Table of Bulk Data entry images related to static and thermal loads. Output by IFP. Table of Bulk Data entry images related to static and thermal loads with DAREA entry images converted to equivalent FORCE and MOMENT entry images. Output by GP1.

GEOM3B

GEOM3M

GEOM3

Table of Bulk Data entry images related to static and thermal loads and updated for the current p-level. Output by GP0.

GEOM3N

GEOM3

Updated GEOM3 for cyclic symmetry analysis. Output by CYCLIC1. Modified GEOM3 with FORCEi and MOMENTi records converted to FORCE and MOMENT records. Output by SECONVRT.

GEOM3S

GEOM3

Table of Bulk Data entry images related to static and thermal loads for the current superelement. Output by SEP2 and SEP2X.

GEOM3T

GEOM3

GEOM3 table with new or modified temperatures. Output by MATMOD option 18.

GEOM3X

GEOM3

GEOM3 table related to axisymmetric conical shell, hydroelastic, and acoustic cavity analysis. Output by IFP3.

GEOM3XSE

GEOM3

Table of bulk data entry images related to static and thermal loads for the entire model that now contains FORCE and MOMENT bulk images to represent the external superelement applied loads.

6-18

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

GEOM4

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity. Output by IFP.

GEOM4*

GEOM4

Family of GEOM4 tables for all partitioned superelements defined in separate Bulk Data sections.

GEOM4EX

GEOM4

GEOM4 table containing records which define an external superelement. Specifically, ASETi and QSETi Bulk Data records. Output by BDRYINFO.

GEOM4EXA

GEOM4

GEOM4 table containing all constraints and sets of an external superelement.

GEOM4M

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity and updated for the current p-level. Output by GP0.

GEOM4N

GEOM4

Updated GEOM4 data block with the a-set data.

GEOM4P

GEOM4

Table of Bulk Data entry images related to constraints and updated for the constraints applied by GMBC, GMSPC, SPC, SPC1, or SPCD Bulk Data entries. Output by MODGM4.

GEOM4S

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity for the current superelement. Output by SEP2 and SEP2X.

GEOM4

GEOM4 table related to axisymmetric conical shell and hydroelastic Output by IFP3 and IFP4. GEOM4 table augmented with new RBE1 and RBE2 records (because all RBE1 and RBE2 elements are split so that each one contains only one m-set grid) for ACMS=’YES’. Also augmented with SEQSET1 records for ACMS=’YES’. Output by SEQP.

GEOM4X

GETNUMPN

Logical. Panel static load computation flag. If TRUE then get number of panels flag only and do not compute panel static loads.

GEQMAP

Table of grid based local equation map indicating which grid resides on which processors/partitions for domain decomposition. Output by SEQP.

GLBRSP

Matrix of global responses when system cell 297=-1. Output by SDRP.

GLBRSPDS

Global results matrix

GLBTAB

Table of global responses when system cell 297=-1. Output by SDRP.

GLBTABDS

Global results correlation table

GLERR

Table of global error estimates from previous iteration. Output by ADAPT.

GLERR1

Table of global error estimates for current iteration. Output by ADAPT.

GM

Multipoint constraint transformation matrix, m-set by n-set. Output by MCE1.

GMD

Multipoint constraint transformation matrix with extra points, m-set by ne-set. Output by UMERGE1.

GNELM

Glue element definition table.

GOA

Omitted degree-of-freedom transformation matrix, o-set by a-set. Output by FBS.

GOD

Omitted degree-of-freedom transformation matrix with extra points, o-set by d-set. Output by UMERGE1.

GPDCT

Table of grid point stress discontinuities for post-processing in the DBC module. Output by STDCON.

GPDT

GPDT

Grid point definition table. Output by GP1.

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

GPECT

Grid point element connection table. Output by TA1.

GPECT1

Grid point element connection table for heat transfer analysis. Output by TAHT.

GPECTF

Grid point element connection table for follower force stiffness. Output by TAFF.

GPFORCE

Integer. The number of columns in FENL. If GPFORCE less than or equal to zero then no GPFORCE or ESE command is present.

GPGK

Aerodynamic transformation matrix for loads from the k-set to g-set. Output by GI.

GPKH

Aerodynamic transformation matrix for loads from the k-set to h-set.

GPIK

Aerodynamic transformation matrix for loads from the h-set to k-set.

GPKE

Matrix of grid point kinetic energies.

GPL

GPL

External grid/scalar point identification number list. Output by GP1.

GPLD

External grid/scalar/extra point identification number list. (GPL appended with extra point data). Output by DPD.

GPMPF

Matrix of grid panel mode participation factors. Output by MODEPF.

GPSETS

Table of grid point sets related to the element plot sets. Output by PLTSET and SEPLOT.

GPSNT

Grid point shell normal table. Output by TASNP2.

GPSNTC

Table of grid point shell normals.

GPSNTS

Grid point shell normal table for the current superelement. Output by SEP2 and TASNP2.

GRIDFMP

Integer. Case Control set identification number of fluid grids that will be output.

GRIDMP

Integer. Case Control set identification number for a set of fluid grids.

GRIDSET

Integer. SET Case Control command identification number which contains a list grid point identification numbers.

GS

Transformation matrix between symmetric (sine) components and solution set components. Output by CYCLIC3.

Data Block Name

Parent Data Block Format

Description

HARM

Table of harmonic indices. Output by CYCLIC1.

HDRLBLi

Character. Header with up to 64 characters to be printed and centered at the top of of each page.

HEADCNTL

List of integer codes for header print control in the DISUTIL module under VECPLOT options IOPT=1 or 5. Output by VECPLOT.

HIS

HIS

Table of design iteration history.

HISADD

HIS

Table of design iteration history for current design cycle. Output by DOM12.

HMKT HOEF1

6-20

Matrix used to compute hinge moments for each AESURF entry. Output by ADG. OEF

DMAP Programmer’s Guide

Table of element fluxes in SORT1 format updated for CHBDYi elements. Output by SDRHT.

Glossaries

Data Block Name

Parent Data Block Format

Ii

Description Inputs to MATMOD and MATPCH module.

IEF

OEF

Table of element forces due to unit modal displacement in SORT1 or SORT2 format. Output by SDR2 or SDR3.

IES

OES

Table of element stresses or strains due to unit modal displacement in SORT1 or SORT2 format. Output by SDR2 or SDR3.

IFD

Matrix of nonlinear element forces at constrained points at the output time steps. Output by NLTRD and NLTRD2.

IFG

Matrix of nonlinear element forces for the g-set at the output time steps. Output by NLTRD.

IFPDB

Table data block with IFP module table attributes.

IFS

Matrix of total element forces and their rate of change. Output by NLTRD2.

IMi

Matrix of independent points.

IMAT

Matrix containing imaginary part of CMAT. Output by MATMOD option 34.

INDTA

Table of element stress/strain or force item code overrides.

INVEC

Starting vector(s).

IQG

OQG

Table of single point forces of constraint due to unit modal displacement in SORT1 or SORT2 format. Output by SDR2 or SDR3.

IUG

OUG

Table of displacements due to unit modal displacement in SORT1 or SORT2 format. Output by SDR2 or SDR3. Integer. If IUNITSOL=0, then trim solution is being supplied. If IUNITSOL>0, then IUNITSOL’th unit solution is being supplied.

IUNITSOL

Data Block Name

Parent Data Block Format

Description

K2DD

Stiffness matrix contribution from the K2PP Case Control command and reduced to the d-set. In frequency response analysis, K2DD may also include structural damping effects.

K2GG

Matrix defined on DMIG Bulk Data entries and referenced by the K2GG Case Control command. Output by MTRXIN.

K2PP

Matrix defined on DMIG Bulk Data entries and referenced by the K2PP Case Control command. Output by MTRXIN.

K4AA

Structural damping matrix in a-set or d-set.

K4KK

Structural damping matrix in cyclic components. Output by CYCLIC3.

K4XX

Structural damping matrix in any set. Usually h-set or d-set in FRRD1.

K42GG

Matrix defined on DMIG Bulk Data entries and referenced by the K42GG Case Control command. Output by MTRXIN.

KAA

Stiffness matrix in a-set or d-set.

KAAL

Element stiffness matrix for linear elements only reduced to a-set.

KBDD

Tangential stiffness in d-set.

KDD

Stiffness matrix for the d-set, linear elements only.

DMAP Programmer’s Guide

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Chapter 6

Glossaries

Data Block Name

Parent Data Block Format

Description

KDDICT

KDICT

KDELM dictionary table. Output by EMG.

KDELM

KELM

Table of element matrices for differential stiffness. Output by EMG.

KDICT

KDICT

KELM dictionary table. Output by EMG.

KDICT1

KDICT

KELM1 dictionary table. Output by GNFM.

KDICTDCN

KELM dictionary table. which incorporates combined constraints and design variables. Output by DSAF.

KDICTDS

Perturbed element stiffness matrix dictionary table. If CDIF=’YES’ then this is the forward perturbed element matrix dictionary. Output by EMG.

KDICTNL

KDICT

KELMNL dictionary table. Output by EMG.

KDICTX

KDICT

Baseline element stiffness matrix dictionary table for h-elements or p-elements. Output by EMG.

KELM

KELM

Table of element matrices for stiffness, heat conduction, differential stiffness, or follower stiffness. Output by EMG.

KELM1

KELM

Table of element matrices for incremental stiffness. Output by GNFM.

KELMDCN

KELM

Table of element matrices for stiffness, heat conduction, differential stiffness, or follower stiffness which incorporates combined constraints and design variables. Output by DSAF.

KELMDS

KELM

Table of perturbed element stiffness matrices. If CDIF=’YES’ then this is the forward perturbed element matrix dictionary. Output by EMG.

KELMNL

KELM

Table of element matrices for stiffness for nonlinear elements.

KFHH

Fluid partition of modal stiffness matrix KHH.

KFS

Stiffness matrix partition (f-set by s-set) from KNN.

KGG

Stiffness matrix in g-set.

KGG1

Stiffness matrix in g-set with general elements. Output by SMA3.

KGGNL

Stiffness (or heat conduction) matrix in g-set for material nonlinear elements only.

KGGNL1

Conduction matrix in g-set for material nonlinear elements only and updated for radiation. Output by RMG2.

KGGT

Total structural stiffness matrix in g-size (sum of linear, nonlinear and differential matrices).

KHH

Generalized (modal) stiffness matrix.

KHH1

Modified generalized (modal) stiffness matrix. Output by FA1.

KKK

Stiffness matrix in cyclic components. Output by CYCLIC3.

KLL

Stiffness matrix reduced to the l-set.

KLR

Stiffness matrix partition (l-set by r-set) from KTT.

KMM

Stiffness matrix in m-set (partition of KGG).

KNN

Stiffness matrix in n-set; after multipoint constraint reduction.

KOA

o-set and a-set matrix partition of stiffness matrix.

KOO

Stiffness matrix partitioned to the o-set from KFF.

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

KRDD

Combined linear and material nonlinear stiffness matrix in the d-set.

KRFGG

Stiffness matrix due to follower rotational forces in g-set. Output by EMAKFR.

KRR

Stiffness matrix partition (r-set by r-set) from KTT.

KRZX

Matrix of restrained dimensional elastic derivatives.

KSAZX

Matrix of dimensional rigid stability derivatives that includes the effect of splines.

KSGG

S-set by f-set matrix and s-set by s-set partitions of the material nonlinear stiffness matrix and expanded to g-set size.

KSS

Stiffness matrix partition (s-set by s-set) from KNN.

KUX

Matrix of stiffness multiplied by displacement or eigenvectors.

KVAL

Table of harmonic indices for analysis. Output by CYCLIC1.

KXX

Stiffness matrix in any set. Usually v-set in READ. Usually h-set or d-set in CEAD, FRRD1, FRRD2, TRD1, and TRD2.

Data Block Name

Parent Data Block Format

Description

L

Lower triangular decomposition factor. Output by MATMOD option 21.

LAJJT

Lower triangular decomposition factor matrix of AJJT.

LAM1DD

Lower triangular factor of the dynamic tangential matrix in the d-set.

LAMA

LAMA

Normal modes eigenvalue summary table. Output by READ, LANCZOS, MODACC, and UEIGL.

LAMA*

LAMA

Family of normal modes eigenvalue summary tables.

LAMA1

LAMA

Normal modes eigenvalue summary table updated for mode tracking. Output by MODTRK.

LAMAF

LAMA

Normal modes eigenvalue summary table for the fluid portion of the model.

LAMAS

LAMA

Normal modes eigenvalue summary table for the structural portion of the model.

LAMAX

LAMA

Modified LAMA table. Output by LAMX.

LAMMAT

Diagonal matrix containing eigenvalues on the diagonal. Output by READ, LANCZOS, and UEIGL.

LBTAB

Table of eigenvalues and generalized masses for retained buckling eigenvalue responses. Output by DSAH.

LCDVEC

Partitioning vector for load case deletion. The row size is the same number of columns in UGX and ones for columns which are retained in UGX1. LCDVEC is intended for partitioning of analysis results related to inertia relief and SPCforces. Output by DSAD.

LCOLLBLi

Character. Label with up to 32 characters to be printed left-justified in upper left corner of each page.

LCPHL

Left-handed complex eigenvector matrix in the l-set. Output by CEAD.

LCPHP

Left-handed complex eigenvector matrix in the p-set.

LCPHX

Left-handed complex eigenvector matrix in the d-set or h-set. Output by CEAD.

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

LD

Lower triangular factor/diagonal. Output by DECOMP and DCMP.

LFTAB

Table of eigenvalues and generalized masses for retained normal mode eigenvalue responses. Output by DSAH.

LGPART

Same as SPCPART except LGPART includes grid points not connected to any element. Output by SEQP.

LISET

Integer. Size of interference js-set extracted from the AEBGPTI table. Output by MTRXIN.

LJSET

Integer. Size of js-set extracted from the AEBGPTJ table. Output by MTRXIN.

LKSET

Integer. Size of ks-set extracted from the AEBGPTK table. Output by MTRXIN.

LLL

Lower triangular factor/diagonal for the l-set from KLL.

LLLT

Lower triangular factor for nonlinear elements including material, slideline, and differential stiffness effects.

LMAT

Normal modes eigenvalue summary table converted to a matrix. Output by LAMX.

LMTROWS

Integer. Number of Lagrange Multipliers appended to the A matrix. These rows are excluded from the internal reordering in the DCMP module.

LMPF

Matrix of fluid force to fluid mode participation factors. Output by MODEPF.

LOCVEC

Vector containing grid locations in the basic coordinate system.

LOO

Lower triangular factor/diagonal for the o-set from KOO. Output by DCMP.

LSEQ

Resequencing matrix based on internal resequencing of KLL. Output by DCMP and DECOMP.

LXX

Lower triangular factor/diagonal of shifted stiffness matrix.

Data Block Name

Parent Data Block Format

Description

M2DD

Mass matrix contribution from the M2PP Case Control command and reduced to the d-set.

M2GG

Matrix defined on DMIG Bulk Data entries and referenced by the M2GG Case Control command. Output by MTRXIN.

M2PP

Matrix defined on DMIG Bulk Data entries and referenced by the M2PP Case Control command. Output by MTRXIN.

MA

Rigid body mass matrix for the a-set. Output by EFFMAS.

MAA

Mass matrix in a-set or d-set.

MAG

Magnitudes of modal contributions matrix.

MAPS

Superelement upstream to downstream boundary coordinate system transformation matrix output by GENTRAN. Superelement boundary transformation matrix for secondary superelements (mirror, identical, and repeated), boundary resequencing and releases output by SEP2 and SEP2X.

MAPS*

Family of MAPS (superelement upstream to downstream boundary coordinate system, secondary (mirror, identical, and repeated), and release transformation matrix).

MAR

Table of virtual mass element areas. Output by MGEN.

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

MAT

Matrix. Output by MATGEN.

MATIi

Matrices defined on DMIJI Bulk Data entries. Output by MTRXIN.

MATGi

Matrices defined on DMIG Bulk Data entries and intended for the g-set. Output by MTRXIN.

MATJi

Matrices defined on DMIJ Bulk Data entries. Output by MTRXIN.

MATKi

Matrices defined on DMIK Bulk Data entries. Output by MTRXIN.

MATNAMi

Character. Matrix name found on DMIG, DMIJ, DMIK, and DMIJI Bulk Data entries.

MATPi

Matrices defined on DMIG Bulk Data entries and intended for the p-set. Output by MTRXIN.

MATPOOL

Table of Bulk Data entry images related to hydroelastic boundary, heat transfer radiation, virtual mass, DMIG, and DMIAX entries. Output by IFP and IFP4.

MATPOOLS

MATPOOL table for the current superelement. Output by SEP2X.

MATPOOLX

MATPOOL table related to hydroelastic analysis. Output by IFP4.

MATS

Any matrix on slave processors.

MATM

Any matrix on master processor. Output by DISUTIL.

MBODY

Body table for p-element analysis. Output by GP0.

MCEIGCC

Logical. Modal complex eigenvalue analysis subcase flag. Set to TRUE if at least one ANALYSIS=MCEIG command was found in CASECC and CASECEIG is specified in the output list. Output by MDCASE.

MCHI

Matrix relating displacements to source strengths. Output by MGEN.

MCHI2

Secondary matrix relating displacements to source strengths. Output by MGEN.

MDD

Mass (or radiation) matrix for the d-set

MDICT

MELM dictionary table. Output by EMG.

MDLIST

Selected mode list from EFFMAS.

MEA

Matrix of element forces per unit motion of the a-set.

MEDGE

Edge table for p-element analysis. Output by GP0.

MEF

Matrix form of element force output table. Output by DRMH1 and DRMS1.

MEM

Modal effective mass matrix. Output by EFFMAS.

MEMF

Modal effective mass fraction table. Output by EFFMAS.

MES

Matrix form of element stress or strain output table. Output by DRMH1 and DRMS1.

MELM

KELM

Table of element mass matrices. Output by EMG.

MESH

Mesh type for aerodynamic or structural components: ’AERO’ or ’STRU’.

MESTNL

Nonlinear element summary table at current step. Output by NLITER and NLTRD2.

MEW

Modal effective weight matrix. Output by EFFMAS.

MFACE

Face table for p-element analysis. Output by GP0.

MFHH

Fluid partition of modal mass matrix MHH.

DMAP Programmer’s Guide

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

MFORC

Modal force vector for superelement.

MFRDEP

Table for frequency dependent properties that can be designed.

MGG

Mass or radiation matrix in g-size.

MGGDIAG

Column vector of diagonal values from superelement mass matrix (g-set size).

MHH

Generalized (modal) mass matrix

MHH1

Modified generalized (modal) mass matrix. Output by FA1.

MI

Modal mass matrix. Output by READ and LANCZOS.

Mi

Matrix data block. Output by INPUTT4 and input to MATPRN and OUTPUT4.

MIDLIS

Table of pairs of user-supplied material property identification numbers (MIDs) and internal baseline MIDs. Output by DSABO.

MKK

Mass matrix in cyclic components. Output by CYCLIC3.

MKLIST

Table of Mach number and reduced frequency pairs. Output by GETMKL.

MLAM

Matrix relating element forces to source strengths. Output by MGEN.

MLAM2

Secondary matrix relating element forces to source strengths. Output by MGEN.

MLL

Mass matrix reduced to the l-set.

MLR

Mass matrix partition (l-set by r-set) from MTT.

MOA

Mass matrix partition (o-set by a-set) from MFF.

MOFPi

Matrix form of the i-th output table. Output by DRMH1 and DRMS1.

MON

Merged monitor table. Output by MRGMON.

MONi

Monitor tables

MONITOR

Structural monitor point table. Output by MAKAEMON and MAKMON.

MOO

Mass matrix partitioned to the o-set from KFF.

MPAER

Elastic restrained loads on aerodynamic monitor points at trim.

MPAERV

Elastic restrained monitor point loads on aerodynamic model

MPAEUV

Elastic unrestrained monitor point loads on aerodynamic model

MPAR

Rigid aerodynamic loads on aerodynamic monitor points at trim.

MPARV

Rigid monitor point loads on aerodynamic model

MPFEM

Modal participation factors for effective mass. Output by EFFMAS.

MPFMAP

Table describing content of mode participation factor matrices. Output by MODEPF.

MPJN2O

Mapping matrix to map j-set data from new order to old order. Output by APD.

MPOOL

Table of RADSET, RADLST, and RADMTX Bulk Data entry images. Output by VDR.

MPSER

Elastic restrained loads on structural monitor points at trim(excluding inertial loads and static applied loads).

MPSERP

Elastic restrained loads on structural monitor points due to static applied loads.

MPSERV

Elastic restrained monitor point loads on structural model

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

MPSEUV

Elastic unrestrained monitor point loads on structural model

MPSIR

Inertial loads on structural monitor points at trim.

MPSIRV

Inertial restrained monitor point loads on structural model

MPSIUV

Inertial unrestrained monitor point loads on structural model

MPSR

Rigid aerodynamic loads on structural monitor points at trim (excluding inertial loads and static applied loads).

MPSRP

Rigid loads on structural monitor points due to static applied loads.

MPSRV

Rigid splined monitor point loads on structural model

MPT

MPT

Table of Bulk Data entry images related to material properties. Output by IFP and IFP6.

MPTC

MPT

Copy of MPT except MAT8 records are replaced by equivalent MAT2 records. Output by IFP6, CMPZPR, and DSTA.

MPTN

MPT

Updated (optimized) MPT. Output by DOM11.

MPTS

MPT

Table of Bulk Data entry images related to material properties for the current superelement. Output by SEP2 and SEP2X.

MPTX

MPT

MPT with design variable perturbations. Output by DSABO. Copy of MPT except MATHP records are updated to include referenced TABLES1 Bulk Data entry information. Output by IFP8.

MQG

Matrix form of single or multipoint forces-of-constraint output table. Output by DRMH1 and DRMS1.

MR

Rigid body mass matrix (r-set by r-set). Output by RBMG4.

MRR

Stiffness matrix partition (r-set by r-set) from MTT.

MTRAK

Table of updated DRESP1 Bulk Data entry images corresponding to the new mode numbering. Output by MODTRK.

MUG

Matrix form of displacement output table. Output by DRMH1 and DRMS1.

MUGNI

Displacement (or temperature) matrix for stiffness (or heat conduction) update. Output by NLITER.

MULNT

Solution matrix from nonlinear transient response analysis in the d-set from the previous subcase. Output by NLTRD2.

MUX

Matrix of mass multiplied by displacements or eigenvectors.

MXX

Mass matrix in any set. Usually v-set in READ. Usually h-set or d-set in CEAD, FRRD1, FRRD2, TRD1, and TRD2.

MZZ

Generalized mass matrix based on PHZ.

Data Block Name

Parent Data Block Format

Description

NAMEi

Matrices defined on DMIG Bulk Data entries. Output by MTRXIN.

NEWDBi

Input table in Version 69 (or greater) format. Output by MAKENEW.

NFDICT

Nonlinear element energy/force index table. Output by TA1.

NLFT

Nonlinear Forcing function table. Output by DPD.

DMAP Programmer’s Guide

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

NPC

Normalized panel contributions results matrix.

NORTAB

Table containing fluid face and the maximum of eight structural grids which lie within the acoustic face. Output by GP5.

NSMEST

Non-structural mass element summary table.

Data Block Name

Parent Data Block Format

Description

Oi

Outputs of MATMOD module.

OBG1

Glue normal and tangential tractions at grid point in basic coordinate system.

OBJTAB

OBJTAB

Design objective table for a given analysis type and superelement. Objective attributes with retained response identification number. Output by DOPR3.

OBJTBG

OBJTAB

Design objective table. Objective attributes with retained response identification number.

OBJTBR

OBJTAB

Table of design objective attributes with retained response identification number. Output by DSAD.

OCCORF

Output table of cross-correlation functions. Output by RANDOM.

OCEIG

Complex eigenvalue extraction report. Output by CEAD.

OCPSDF

Output table of cross-power-spectral-density functions. Output by RANDOM.

OEDE1

Elemental energy loss. Output by GPFDR.

OEDS1

OES

Table of element stress discontinuities. Output by STDCON.

OEEATO2

OEE

Table of element strains in SORT2 format for the autocorrelation function. Output by RANDOM. Table of element strains in SORT2 format for the cross correlation function. Output by RANDOM.

OEECRM2 OEENO2

OEE

Table of element strains in SORT2 format for the NO function. Output by RANDOM.

OEEPSD2

OEE

Table of element strains in SORT2 format for the PSD function. Output by RANDOM.

OEERMS2

OEE

Table of element strains in SORT2 format for the RMS function. Output by RANDOM.

OEF

OEF

Table of element forces in SORT1 or SORT2 format. Output by DDRMM.

OEF1

OEF

Table of element forces (or fluxes) in SORT1 format. Output by SDR2 or DRMH3.

OEF1A

OEF

Table of element forces in SORT1 format for the composite elements only. Output by SDR2.

OEF1AA

OEF

Table of element forces in SORT1 format for the non-composite elements only. Output by SDRCOMP.

OEF1DS

OEF

Table of element forces, excluding non-composite elements, in SORT1 format for design responses.

OEF1VU

OEF

Table of element forces in SORT1 format for view elements. Output by SDRP.

OEF1X

OEF

Table of element forces in SORT1 format updated for PLOAD1 loads and intermediate station output. Output by SDRX and SDRXD.

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

OEF2

OEF

Table of element forces in SORT2 format.

OEFATO1

OEF

Table of element forces in SORT1 format for the autocorrelation function.

OEFATO1M

OEF

Table of element forces in SORT1 format in the material coordinate system for the autocorrelation

OEFATO2

OEF

Table of element forces in SORT2 format for the autocorrelation function. Output by RANDOM.

OEFATO2M

OEF

Table of element forces in SORT2 format in the material coordinate system for the autocorrelation. Output by RANDOM.

OEFCRM1

OEF

Table of element forces in SORT1 format for the CRMS function.

OEFCRM1M

OEF

Table of element forces in SORT1format in the material coordinate system for the CRMS function.

OEFCRM2

OEF

Table of element forces in SORT2 format for the cross correlation function. Output by RANDOM.

OEFCRM2M

OEF

Table of element forces in SORT2 format in the material coordinate system for the CRMS function. Output by RANDOM.

OEFDSN

OEF

Table of element forces, excluding non-composite elements, in SORT1 format for the perturbed configuration.

OEFIIP

OEF

Data block for in-plane ply failure indices.

OEFIIS

OEF

Data block for inter-laminar shear failure indices.

OEFIT

OEF

Table of composite element failure indices. Output by SDRCOMP.

OEFITDS

OEF

Table of composite element failure indices for design responses.

OEFITDSN

OEF

Table of composite element failure indices for the perturbed configuration.

OEFNL1

OEF

Table of nonlinear element fluxes in SORT1 format. Output by SDR2.

OEFNO1

OEF

Table of element forces in SORT1 format for the NO function.

OEFNO1M

OEF

Table of element forces in SORT1 format in the material coordinate system for the NO function.

OEFNO2

OEF

Table of element forces in SORT2 format for the NO function. Output by RANDOM.

OEFNO2M

OEF

Table of element forces in SORT2 format in the material coordinate system for the NO function. Output by RANDOM.

OEFPSD1

OEF

Table of element forces in SORT1 format for the PSD function.

OEFPSD1M

OEF

Table of element forces in SORT1 format in the material coordinate system for the PSD function.

OEFPSD2

OEF

Table of element forces in SORT2 format for the PSD function. Output by RANDOM.

OEFPSD2M

OEF

Table of element forces in SORT2 format in the material coordinate system for the PSD function. Output by RANDOM.

OEFRMS1

OEF

Table of element forces in SORT1 format for the RMS function.

OEFRMS1M

OEF

Table of element forces in SORT1 format in the material coordinate system for the RMS function.

OEFRMS2

OEF

Table of element forces in SORT2 format for the RMS function. Output by RANDOM.

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Chapter 6

Glossaries

Data Block Name

Parent Data Block Format

Description

OEFRMS2M

OEF

Table of element forces in SORT2 format in the material coordinate system for the RMS function. Output by RANDOM.

OEIG

Real eigenvalue extraction report. Output by READ.

OEKE1

Elemental kinetic energy. Output by GPFDR.

OEP

Table of element pressures due to virtual mass in SORT1 or SORT2 format. Output by MDATA.

OES

OES

Table of element stresses or strains in SORT1 or SORT2 format. Output by DDRMM.

OES1

OES

Table of element stresses or strains in SORT1 format. Output by SDR2 or DRMH3. OES1A Table of element strain/curvatures in SORT1 format for the composite elements only. Output by SDR2.

OES1C

OES

Table of composite element stresses or strains in SORT1 format. Output by SDRCOMP.

OES1CDS

OES

Table of composite element stresses in SORT1 format for design responses.

OES1DS

OES

Table of element stresses in SORT1 format for design responses.

OES1M

OES

Element stress or strain table in SORT1 format in the material coordinate system defined on the MAT1 entry. Output by CURV.

OES1G

OES

Grid point stress or strain table in SORT1 format and interpolated from the centroidal stress table, OES1M. Output by CURV.

OES1VU

OES

Table of element stresses in SORT1 format for view elements. Output by SDRP.

OES1X

OES

Table of element stresses in SORT1 format updated for PLOAD1 loads and intermediate station output. Output by SDRX and SDRXD. Table of linear and nonlinear element stresses in SORT1 and linear element format. Output by MERGEOFP.

OES2

OES

Table of element stresses or strains in SORT2 format.

OES2GX

OES

Table of grid point stresses in SORT2 format. Output by CURVPLOT.

OESATO1

OES

Table of element stresses in SORT1 format for the autocorrelation function.

OESATO1M

OES

Table of element stresses in SORT1 format in the material coordinate system for the autocorrelation function.

OESATO2

OES

Table of element stresses in SORT2 format for the autocorrelation function. Output by RANDOM.

OESATO2M

OES

Table of element stresses in SORT2 format in the material coordinate system for the autocorrelation function. Output by RANDOM.

OESCDSN

OES

Table of composite element stresses in SORT1 format for the perturbed configuration.

OESCRM1

OES

Table of element stresses in SORT1 format for the CRMS function.

OESCRM1M

OES

Table of element stresses in SORT1 format in the material coordinate system for the CRMS function.

OESCRM2

OES

Table of element stresses in SORT2 format for the CRMS function. Output by RANDOM

OESCRM2M

OES

Table of element stresses in SORT2 format in the material coordinate system for the CRMS function. Output by RANDOM

OESDSN

OES

Table of element stresses in SORT1 format for the perturbed configuration

OESNL1

OES

Table of nonlinear element stresses in SORT1 format. Output by NLTRD, NLTRD2, and SDRNL.

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DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

OESNLB1

OES

Table of slideline contact element stresses in SORT1 format. Output by NLTRD2 and SDRNL.

OESNLXR

OES

Table of nonlinear element stresses in SORT1 format and appended for all subcases (OESNLX from SDRNL).

OESNO1

OES

Table of element stresses in SORT1 format for the NO function.

OESNO1M

OES

Table of element stresses in SORT1 format in the material coordinate system for the NO function.

OESNO2

OES

Table of element stresses in SORT2 format for the NO function. Output by RANDOM.

OESNO2M

OES

Table of element stresses in SORT2 format in the material coordinate system for the NO function. Output by RANDOM.

OESPSD1

OES

Table of element stresses in SORT1 format for the PSD function.

OESPSD1M

OES

Table of element stresses in SORT1 format in the material coordinate system for the PSD function.

OESPSD2

OES

Table of element stresses in SORT2 format for the PSD function. Output by RANDOM.

OESPSD2M

OES

Table of element stresses in SORT2 format in the material coordinate system for the PSD function. Output by RANDOM.

OESRIP

OES

Data block for in-plane ply strength ratios.

OESRIS

OES

Data block for inter-laminar shear strength ratios.

OESRMS1

OES

Table of element stresses in SORT1 format for the RMS function.

OESRMS1M

OES

Table of element stresses in SORT1 format in the material coordinate system for the RMS function.

OESRMS2

OES

Table of element stresses in SORT2 format for the RMS function. Output by RANDOM.

OESRMS2M

OES

Table of element stresses in SORT2 format in the material coordinate system for the RMS function. Output by RANDOM.

OESRT

OEF

Table of composite element ply strength ratio. Output by SDRCOMP

OFMPF2M

Table of fluid modal participation factors by natural modes in SORT2 format. Output by RANDOM.

OFPE

Element data recovery table in SORT1 or SORT2 format.

OFPES

Filtered and sorted element data recovery table. Output by STRSORT.

OFPi

Output table suitable for processing by the OFP module.

OFPi1

Output table in SORT1 format usually created by, but not limited to, the SDR2 module.

OFPi2

Output table in SORT2 format.

OFPiX

Output table in SORT2 or SORT1 format. Output by SDR3.

OGDS1

Table of grid point stress discontinuities. Output by STDCON.

OGPFB1

OGF

Table of grid point forces. Output by GPFDR.

OGPFIN

Grid point force balance data block (SORT1 format) for which grid point force balance totals are to be recalculated.

OGPFOU

Resulting grid point force balance data block (SORT1 format).

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Chapter 6

Data Block Name

Glossaries

Parent Data Block Format

Description

OGPFTMP

Grid point force balance data block to be used as a template (SORT1 format).

OGPKE1

Table of grid point kinetic energies in SORT1 format. Output by SDR2.

OGPMPF2M

Table of panel grid modal participation factors by natural modes in SORT2 format. Output by RANDOM.

OGPWG

Grid point weight generator table in weight units. Output by GPWG or VECPLOT (option 7).

OGS1

OGS

Table of grid point stresses or strains in SORT1 format. Output by GPSTR2.

OINT

P-element output control table. Contains OUTPUT Bulk Data entries. Output by IFP.

OINTDS

P-element output control table for constrained elements. Output by DOPR3.

OINTDSF

P-element output control table for the perturbed configuration. Output by DSAH.

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list. Output by CEAD, READ, TRLG, and FRLG.

OL1

OL truncated by the OFREQ or OTIME or OMODES command.

OLDDBi

Output table in pre-Version 69 format. Output by MAKEOLD.

OLF

Nonlinear static load factor list.

OLMPF2M

Table of load modal participation factors by natural modes in SORT2 format. Output by RANDOM.

OM1

Transformation matrix describing the surface spline connection. NI rows by ND columns. NI = number of independent points. ND = number of dependent points.

ONRGY1

Table of element strain energies and energy densities. Output by GPFDR.

ONRGYDS

OEE

Table of element strain energies in SORT1 format for design responses. Output by GPFDR.

ONRGYDSN

OEE

Table of element strain energies and energy densities in SORT1 format for design responses for the perturbed configuration.

OPG1

OPG

Table of applied loads in SORT1 format. Output by SDR2.

OPG2

OPG

Table of applied loads in SORT2 format.

OPG2X

OPG

Table of applied loads in SORT2 format. Output by CURVPLOT.

OPGATO1

OPG

Table of applied loads in SORT1 format for the autocorrelation function.

OPGATO2

OPG

Table of applied loads in SORT2 format for the autocorrelation function. Output by RANDOM.

OPGCRM1

OPG

Table of applied loads in SORT1 format for the cross correlation function.

OPGCRM2

OPG

Table of applied loads in SORT2 format for the cross correlation function. Output by RANDOM.

OPGNO1

OPG

Table of applied loads in SORT1 format for the NO function.

OPGNO2

OPG

Table of applied loads in SORT2 format for the NO function. Output by RANDOM.

OPGPSD1

OPG

Table of applied loads in SORT1 format for the PSD function.

OPGPSD2

OPG

Table of applied loads in SORT2 format for the PSD function. Output by RANDOM.

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Glossaries

Data Block Name

Parent Data Block Format

Description

OPGRMS1

OPG

Table of applied loads in SORT1 format for the RMS function.

OPGRMS2

OPG

Table of applied loads in SORT2 format for the RMS function. Output by RANDOM.

OPMPF2M

Table of panel modal participation factors by natural modes in SORT2 format. Output by RANDOM.

OPNL1

Table of nonlinear loads in SORT1 format for the h-set or d-set. Output by VDR.

OPTPRM

OPTPRM

Table of optimization parameters.

OPTPRMG

OPTPRM

Table of optimization parameters. Updated table of optimization parameters. Output by DOM12.

OPTNEW OQG

OQG

Table of single or multipoint forces-of-constraint in SORT1 or SORT2 format. Output by DDRMM.

OQG1

OQG

Table of single or multipoint forces-of-constraint in SORT1 format. Output by SDR2 or DRMH3.

OQG1DS

OQG

Table of single point forces-of-constraint in SORT1 format for design responses.

OQG2

OQG

Table of single point forces of constraint in SORT2 format.

OQG2X

OQG

Table of single point forces of constraint in SORT2 format. Output by CURVPLOT.

OQGATO1

OQG

Table of single point forces of constraints in SORT1 format for the autocorrelation function.

OQGATO2

OQG

Table of single point forces of constraints in SORT2 format for the autocorrelation function. Output by RANDOM.

OQGCRM1

Table of single point forces of constraint in SORT1 format for the cross correlation.

OQGCRM2

Table of single point forces of constraint in SORT2 format for the cross correlation. Output by RANDOM.

OQGDSN

OQG

Table of single forces-of-constraint in SORT1 format for design responses for the perturbed configuration.

OQGGF1

OQG

Glue forces at grid point in basic coordinate system.

OQGNO1

OQG

Table of single point forces of constraint in SORT1 format for the NO function.

OQGNO2

OQG

Table of single point forces of constraint in SORT2 format for the NO function. Output by RANDOM.

OQGPSD1

OQG

Table of single point forces of constraint in SORT1 format for the PSD function.

OQGPSD2

OQG

Table of single point forces of constraint in SORT2 format for the PSD function. Output by RANDOM.

OQGRMS1

OQG

Table of single point forces of constraints in SORT1 format for the RMS function.

OQGRMS2

OQG

Table of single point forces of constraints in SORT2 format for the RMS function. Output by RANDOM.

OQMATO1

OQG

Table of multipoint forces of constraint in SORT1 format for the autocorrelation function.

OQMATO2

OQG

Table of multipoint forces of constraint in SORT2 format for the autocorrelation function. Output by RANDOM.

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Data Block Name

Glossaries

Parent Data Block Format

Description

OQMCRM1

Table of multipoint forces of constraints in SORT1 format for the CRMS function.

OQMCRM2

Table of multipoint forces of constraints in SORT2 format for the CRMS function. Output by RANDOM

OQMG2

OQG

Table of multipoint forces of constraint in SORT2 format.

OQMNO1

OQG

Table of multipoint forces of constraint in SORT1 format for the NO function.

OQMNO2

OQG

Table of multipoint forces of constraint in SORT2 format for the NO function. Output by RANDOM.

OQMPSD1

OQG

Table of multipoint forces of constraint in SORT1 format for the PSD function.

OQMPSD2

OQG

Table of multipoint forces of constraint in SORT2 format for the PSD function. Output by RANDOM.

OQMRMS1

OQG

Table of multipoint forces of constraint in SORT1 format for the RMS function.

OQMRMS2

OQG

Table of multipoint forces of constraints in SORT2 format for the RMS function. Output by RANDOM. Table of structural modal participation factors by natural modes in SORT2 format. Output by RANDOM.

OSMPF2M

OSTATO1M

OES

Table of element strains in SORT1 format in the material coordinate system for the autocorrelation function.

OSTATO2M

OES

Table of element strains in SORT2 format in the material coordinate system for the autocorrelation function. Output by RANDOM.

OSTCRM1M

OES

Table of element strains in SORT1 format in the material coordinate system for the CRMS function.

OSTCRM2M

OES

Table of element strains in SORT2 format in the material coordinate system for the CRMS function. Output by RANDOM

OSTNO1M

OES

Table of element strains in SORT1 format in the material coordinate system for the NO function.

OSTNO2M

OES

Table of element strains in SORT2 format in the material coordinate system for the NO function. Output by RANDOM.

OSTPSD1M

OES

Table of element strains in SORT1 format in the material coordinate system for the PSD function.

OSTPSD2M

OES

Table of element strains in SORT2 format in the material coordinate system for the PSD function. Output by RANDOM.

OSTR1CDS

OEE

Table of composite element strains in SORT1 format for design responses.

OSTR1DS

OEE

Table of element strains in SORT1 format for design responses.

OSTR1G

OEE

Table of grid point strains in SORT1 format. Output by CURV.

OSTR1VU

OEE

Table of element strains in SORT1 format for view elements. Output by SDRP. Table of element strains in SORT1 format augmented with strains for 1-D elements. Output by SDRX and SDRXD.

OSTR1X OSTR2

OEE

Table of element strains in SORT2 format.

OSTRATO1

OES

Table of element strains in SORT1 format for the autocorrelation function.

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Data Block Name

Parent Data Block Format

Description

OSTRATO2

OES

Table of element strains in SORT2 format for the autocorrelation function. Output by RANDOM.

OSTR2GX

OEE

Table of grid point strains in SORT2 format. Output by CURVPLOT.

OSTRCDSN

OEE

Table of composite element strains in SORT1 format for the perturbed configuration.

OSTRCRM1

OES

Table of element strains in SORT1 format for the CRMS function.

OSTRCRM2

OES

Table of element strains in SORT2 format for the CRMS function. Output by RANDOM

OSTRDSN

OEE

Table of element strains in SORT1 format for the perturbed configuration

OSTRMS1M

OES

Table of element strains in SORT1 format in the material coordinate system for the RMS function.

OSTRMS2M

OES

Table of element strains in SORT2 format in the material coordinate system for the RMS function. Output by RANDOM.

OSTRNO1

OES

Table of element strains in SORT1 format for the NO function.

OSTRNO2

OES

Table of element strains in SORT2 format for the NO function. Output by RANDOM.

OSTRPSD1

OES

Table of element strains in SORT1 format for the PSD function.

OSTRPSD2

OES

Table of element strains in SORT2 format for the PSD function. Output by RANDOM.

OSTRRMS1

OES

Table of element strains in SORT1 format for the RMS function.

OSTRRMS2

OES

Table of element strains in SORT2 format for the RMS function. Output by RANDOM.

OUG

OUG

Table of displacements in SORT1 or SORT2 format. Output by DDRMM.

OUG1

OUG

Table of displacements in SORT1 format. Output by SDR2 or DRMH3.

OUG1DS

OUG

Table of displacements in SORT1 format for design responses.

OUG1VU

OUG

Table of displacements in SORT1 format for view grids. Output by SDRP.

OUG2

OUG

Table of displacements in SORT2 format.

OUG2X

OUG

Table of displacements in SORT2 format. Output by CURVPLOT.

OUGATO1

OUG

Table of displacements in SORT1 format for the autocorrelation function.

OUGATO2

OUG

Table of displacements in SORT2 format for the autocorrelation function. Output by RANDOM.

OUGCRM1

OUG

Table of displacements in SORT1 format for the cross correlation function.

OUGCRM2

OUG

Table of displacements in SORT2 format for the cross correlation function. Output by RANDOM.

OUGDSN

OUG

Table of displacements in SORT1 format for design responses for the perturbed configuration.

OUGNO1

OUG

Table of displacements in SORT1 format for the NO function.

OUGNO2

OUG

Table of displacements in SORT2 format for the NO function. Output by RANDOM.

OUGPSD1

OUG

Table of displacements in SORT1 format for the PSD function.

OUGPSD2

OUG

Table of displacements in SORT2 format for the PSD function. Output by RANDOM.

OUGRMS1

OUG

Table of displacements in SORT1 format for the RMS function.

OUGRMS2

OUG

Table of displacements in SORT2 format for the RMS function. Output by RANDOM.

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Glossaries

Data Block Name

Parent Data Block Format

Description

OUGV1

OUG

Table of absolute displacement, velocity and acceleration in SORT1 format.

OUGV2

OUG

Table of absolute displacement, velocity and acceleration in SORT2 format.

OUTFLE

Table of panel or grid contributions in SORT1 format.

OUTVEC

Last vector block (Lanczos only). Output by READ.

OUXY1

OUG

Table of displacements in SORT1 format for h-set or d-set. Output by VDR.

OVG

Table of aeroelastic x-y plot data for V-g or V-f curves. Output by FA2.

OXRESP

Table of response spectra in SORT2 format. Output by RSPEC.

Data Block Name

Parent Data Block Format

Description

Pi1

Pi truncated by the OFREQ or OTIME or OMODES command.

P2G

Matrix defined on DMIG Bulk Data entries and referenced by the P2G Case Control command. Output by MTRXIN.

PA

Static load matrix reduced to the a-set. Output by SSG2.

PA*

Family of static load matrices (PA) applied on the boundary (a-set) of all upstream superelements.

PAK

Aerodynamic forces at aerodynamic boxes.

PANSLT

Panel static load table. Output by GP5.

PARTV

Partitioning vector.

PARTVEC

Partitioning vector with values of 1.0 at the rows corresponding to degrees-of-freedom which were eliminated in the partition to obtain KXX, etc. Required for maximum efficiency during symmetric decomposition and if KXX represents a subset of the d-set (SETNAME=’D’). PARTVEC is not required if KXX represents the h-set. See SETNAME parameter description below.

PBGPDT

BGPDT

Basic grid point definition table updated to support plotting CHBDYi elements. Output by PLTHBDY.

PBYG

Matrix of equivalent static loads due to enforced velocity for the g-set.

PC

Optional stepwise preconditioner in SOLVIT and STATICS, same as A and KGG respectively.

PC1

Updated stepwise preconditioner matrix. Output by SOLVIT and STATICS.

PCDB

Table of model (undeformed and deformed) plotting commands. Output by IFP1.

PCDBS

Table of model (undeformed and deformed) plotting commands for the current superelement (identification number equal to output value of SEID). Output by SEP2CT.

PCDBDR

Table of model (undeformed and deformed) plotting commands for the superelement (identification number equal to output value of SEID). Output by SEDR.

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry.

PCOMPTC

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry. Output by IFP6.

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Glossaries

Data Block Name

Parent Data Block Format

Description

PCOMPTX

PCOMPT with design variable perturbations. Output by DSABO.

PD

Dynamic load matrix for the d-set.

PD1

Equivalent load vector for mode acceleration computations for the a-set. Output by DDR2.

PDF

Frequency response load matrix in the d-set. Output by FRLG.

PDT

Transient response load matrix in the d-set for output time steps. Output by TRLG.

PDT1

Transient response load matrix in the d-set for all time steps. Output by TRLG.

PECT

Element connectivity table updated to support plotting CHBDYi elements. Output by PLTHBDY.

PELSDSF

P-element set table for the perturbed configuration. Output by DSAH.

PELSET

P-element set table, contains SETS DEFINITIONS. Output by PLTSET.

PELSETDS

P-element set table for constrained elements. Output by DOPR3.

PFHF

Fluid partition of frequency response modally reduced load matrix.

PFP

Frequency response load matrix in the p-set combined with gust loads. Output by GUST.

PG

Static load matrix applied to the g-set. In superelement analysis and output by SELA, PG includes the loads from upstream superelements. Output by SSG1 and SELA.

PG1

Combined static load matrix for the g-set and in the residual structure. Output by PCOMB.

PGG

Force matrix in g-set for all processors (global). Output by DISUTIL.

PGT

Static load matrix applied to the g-set appended for all boundary conditions. Output by SDR1.

PGUP

Static load matrix for the g-set and in the residual structure due to static loads in upstream superelements only.

PGVST

Static load vector matrix (g-set). Output by MAKAEFS.

PHA

Normal modes eigenvector matrix in the a-set. Output by READ.

PHA1

Normal modes eigenvector matrix in the a-set updated for mode tracking. Output by MODTRK.

PHAREF1

Designed normal modes eigenvector matrix in the a-set updated for mode tracking. Output by MODTRK.

PHASH2

Structural partition (row-wise) of eigenvector matrix PHDH. Also partitioned column-wise according to parameter STRUCTMP.

PHDFH

Fluid partition (row-wise) of eigenvector matrix PHDH.

PHDH

Transformation matrix from d-set to h-set (modal). Output by GKAM.

PHF

Frequency response load matrix in the h-set (modal). Output by FRLG.

PHF1

Frequency response load matrix in the h-set (modal) combined with gust loads. Output by GUST.

PHG

Normal modes eigenvector matrix in the g-set. Output by READ and LANCZOS.

PHG*

Family of normal modes eigenvector matrices in the g-set.

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Data Block Name

Glossaries

Parent Data Block Format

Description

PHG1

Normal modes eigenvector matrix in the g-set updated for mode tracking. Output by MODTRK.

PHGREF

Designed normal modes eigenvector matrix in the g-set from the prior design cycle output of MODTRK. Output by MODTRK.

PHGREF1

Designed normal modes eigenvector matrix in the g-set updated for mode tracking. Output by MODTRK.

PHIDLL

Retained left divergence eigenvector responses.

PHIDRL

Retained right divergence eigenvector responses.

PHIG

Mode shape matrix (U8-set) for superelement.

PHT

Transient response load matrix in the h-set (modal) for all time steps. Output by TRLG.

PHX

Right eigenvector matrix for real eigenvalues only. Output by UEIGL.

PHXL

Left eigenvector matrix for real eigenvalues only. Output by UEIGL.

PHZ

Generalized degree-of-freedom transformation matrix. Output by DYNREDU.

PJ

Static load matrix for the g-set of the current superelement and applied to its interior points only.

PKF

Matrix of k-set forces per frequency.

PKYG

Matrix of equivalent static loads due to enforced displacement for the g-set.

PL

Static load matrix reduced to the l-set. Output by SSG2.

PLI

Static load matrix with inertial loads and reduced to the l-set. Output by SSG4.

PLIST2

Table of type two properties on DVPREL2 Bulk Data entries. Output by DOPR1.

PLIST2*

Family of tables of type two properties on DVPREL2 Bulk Data entries. Output by DOPR1.

PLMAT

Initial and final load matrices for subcase.

PLOTMSG

Table of user informational messages generated during the plot process. Output by PLOT.

PLSETMSG

Table of user informational messages generated during the definition of element plot sets. Output by PLTSET and SEPLOT.

PLTPAR

Table of plot parameters and plot control. Output by PLTSET and SEPLOT.

PMPF

Matrix of contribution of structural panels to fluid mode participation factors. Output by MODEPF.

PMYG

Matrix of equivalent static loads due to enforced acceleration for the g-set.

PNL

Nonlinear load matrix appended from each output time step. Output by NLTRD, NLTRD2, TRD1, and TRD2.

PNLLST

Table of triplets defining panel names and their associated IPANEL qualifier values.

PO

Static load matrix partitioned to the o-set. Output by SSG2.

POI

Static load matrix with inertial loads and reduced to the o-set. Output by SSG4.

POSTCDB

Table of commands from the OUTPUT(POST) section of Case Control. Output by IFP1.

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Glossaries

Data Block Name

Parent Data Block Format

Description

PPF

Frequency response load matrix in the p-set. Output by FRLG.

PPT

Transient response load matrix in the p-set for output time steps. Output by TRLG.

PPVR

Partitioning vector for random responses. Output by DOPRAN.

PRBDOFS

Partitioning matrix to partition the "active" URDDI from the "inactive". Active URRDI are assigned a 1.0 value and are connected to the SUPORT degrees-of-freedom. Output by MAKETR.

PROPI

Matrix of initial property values. Output by DOPR1.

PROPI*

Family of matrices of initial property values. Output by DOPR1.

PROPO

Matrix of final (optimized) property values. Output by DOM9.

PS

Static load matrix partitioned to the s-set. Output by SSG2.

PSDF

Power spectral density table. Output by RANDOM.

PSDL

Power spectral density list. Output by DPD.

PSF

Frequency response load matrix in the s-set. Output by FRLG.

PSI

Modal partitioning factor matrix.

PST

Transient response load matrix in the s-set for output time steps. Output by TRLG.

PTELEM

Table of thermal loads in the elemental coordinate system. Output by SSG1.

PTELEM0

Table of thermal loads in the elemental coordinate system from prior subcase. Output by SSG1.

PTELMDCN

Table of thermal loads in the elemental coordinate system which incorporates combined constraints and design variables. Output by DSAF.

PTELMDSX

Table of thermal loads in the elemental coordinate system for the central, forward, or backward perturbed configuration. Output by SSG1.

PUG

Matrix of translational displacements. Output by SDR2.

PUG*

Family of matrices of translational displacements for all superelements.

PUGD

Matrix of translational displacements in dynamic analysis. Output by SDR2.

PUGS

Matrix of translational displacements in static analysis. Output by SDR2.

PUGX

PUG assembled for superelements defined on the SEPLOT or SEUPPLOT command. Output by SEPLOT.

PVAL0

P-value table generated by the ADAPT module in previous superelement, adaptivity cycle, or run.

PVAL1

P-value table updated for current superelement or adaptivity loop. Output by ADAPT.

PVEC

Partitioning vector for supported degrees-of-freedom specified on CYSUP Bulk Data entry. Output by CYCLIC3.

PVGRID

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to elements or grids specified on the following Case Control commands: DISPLACEMENT, VELOCITY, ACCELERATION, FORCE, STRESS, STRAIN, SPCFORCE, MPCFORCE, MPRES, GPFORCE, ESE, EKE, EDE, GPKE, MODCON, PANCON. Output by OUTPRT.

PVLOAD

Partitioning vector with ones at rows corresponding to degrees-of-freedom at which static and dynamic loads are applied. Output by OUTPRT.

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Data Block Name

Glossaries

Parent Data Block Format

Description

PVMPC

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to elements or grids specified on the MPCFORCE Case Control command. Output by OUTPRT.

PVSPC

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to elements or grids specified on the SPCFORCE Case Control command. Output by OUTPRT.

PVT

Table containing parameter values from PARAM Bulk Data entry images. Output by IFP.

PVTS

Table containing parameter values which are resolved from values in PVT, CASECC, and, optionally, the NDDL. Output by PVT.

PX

Inertial or pseudo-load matrix. Output by DSAP.

PXF

Frequency response load matrix in h-set (modal) or d-set.

PXT

Transient response load matrix in the h-set (modal) or d-set. Output by TRLG.

PXT1

Reduced transient response load matrix analysis. Output by DSAR.

PZ

Reduced aerostatic loads matrix.

Data Block Name

Parent Data Block Format

Description

QG

Single-point constraint forces of constraint matrix in the g-set. Output by LANCZOS, STATICS, and SDR1.

QHH

Aerodynamic matrix of size h- by h-set. Output by AMP.

QHHL

Aerodynamic matrix list

QHJ

Aerodynamic matrix of size h- by j-set. Output by AMP.

QHJK

Aero transformation matrix between h and j sets. Output by GUST.

QHJL

Aero transformation matrix between h and j sets.

QKH

Aerodynamic matrix of size k- by h-set. Output by AMP.

QKHL

Aero transformation matrix between h and k sets.

QLL

Aerodynamic matrix for divergence analysis.

QMG

Multipoint constraint forces of constraint matrix in the g-set. Output by LANCZOS and STATICS.

QNV

Quasi-Newton sweeping vectors. Output by NLITER.

QR

Matrix of determinate support forces. Output by SSG2.

QXX

Aerodynamic matrix in any set.

Data Block Name

Parent Data Block Format

R

Residual matrix. Output by SOLVIT.

R1MAPR

R1MAP

R1TAB

6-40

Description

Table of mapping from original first level (direct) retained responses. Output by DSAD. Table of first level (direct) (DRESP1 Bulk Data entry) attributes. Output by DOPR3.

DMAP Programmer’s Guide

Glossaries

Data Block Name

Parent Data Block Format

Description

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attributes. Output by DSAD.

R1TABRG

Table of attributes of the retained first level (direct) responses.

R1VAL

Matrix of initial values of the retained first level (direct) responses. Output by DSAD.

R1VALO

Matrix of final (optimized) values of the retained first level (direct) responses. Output by DOM9.

R1VALR

Matrix of retained type one responses. Output by DSAD.

R1VALRG

Matrix of initial values of the retained first level (direct) responses.

R2MAPR

Table of mapping from original second level (synthetic) retained responses. Output by DSAD.

R2VAL

Matrix of initial values of the retained second level (synthetic) responses. Output by DSAD.

R2VALO

Matrix of final (optimized) values of the second level (synthetic) responses. Output by DOM9.

R2VALR

Matrix of retained second level (synthetic) responses.

R2VALRG

Matrix of initial values of the retained second level (synthetic) responses.

R3VAL

Matrix of initial values of the retained third level responses. Output by DSAD.

R3VALO

Matrix of final values of the third level responses. Output by DOM9.

R3VALR

Matrix of initial values of the retained third level responses. Output by DSAD.

R3VALRG

Matrix of initial values of the retained third level responses.

RADAMPG

Structural damping ratio matrix

RADAMPZ

Viscous damping ratio matrix

RADCONS

OUG

Displacement Constraint Mode

RADDATC

OUG

Displacement Distributed Attachment Mode

RADEATC

OUG

Displacement Equivalent Inertia Attachment mode

RADEFFM

OUG

Displacement Effective Inertia Mode

RADEFMP

OUG

Displacement PHA^T

RADNATC

OUG

Displacement Nodal Attachment Mode

RAECONS

OES

Strain Constraint Mode

RAEDATC

OES

Strain Distributed Attachment Mode

RAEEATC

OES

Strain Equivalent Inertia Attachment mode

RAENATC

OES

Strain Nodal Attachment Mode

RAFCONS

OEF

Element Force Constraint Mode

RAFDATC

OEF

Element Force Distributed Attachment Mode

RAFEATC

OEF

Element Force Equivalent Inertia Attachment mode

RAFNATC

OEF

Element Force Nodal Attachment Mode

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Glossaries

Data Block Name

Parent Data Block Format

Description

RAGCONS

OEF

Grid Point Forces Constraint Mode

RAGDATC

OEF

Grid Point Forces Distributed Attachment Mode

RAGEATC

OEF

Grid Point Forces Equivalent Inertia Attachment mode

RAGNATC

OEF

Grid Point Forces Nodal Attachment Mode

RALDATC

OUG

Load vector used to compute the Distributed Attachment modes

RANCONS

OEE

Strain Energy Constraint Mode

RANDATC

OEE

Strain Energy Distributed Attachment Mode

RANEATC

OEE

Strain Energy Equivalent Inertia Attachment mode

RANNATC

OEE

Strain Energy Nodal Attachment Mode

RARCONS

OQG

Reaction Force Constraint Mode

RARDATC

OQG

Reaction Force Distributed Attachment Mode

RAREATC

OQG

Reaction Force Equivalent Inertia Attachment mode

RARNATC

OQG

Reaction Force Nodal Attachment Mode

RASCONS

OES

Stress Constraint Mode

RASDATC

OES

Stress Distributed Attachment Mode

RASEATC

OES

Stress Equivalent Inertia Attachment mode

RASNATC

OES

Stress Nodal Attachment Mode

RBF

Rigid body force matrix.

RCROSSL

Table of RCROSS Bulk Data entry images. Output by DPD.

RDEST

Radiation element summary table. Output by RMG2.

RECM

Radiation exchange coefficient matrix. Output by RMG2.

RESMAX

Resultant or maxima matrix. Output by VECPLOT.

RESMAX0

Resultant or maxima matrix for residual structure. Output by VECPLOT.

RESP3

Table of third level responses. Output by DOPR3.

RESP3R

Table of retained third level responses in RESP3. Output by DSAD.

RESP12

RESP12

Table of second level (synthetic) responses. Output by DOPR3.

RGG

Radiation transfer matrix in the g-set. Output by RMG2.

RHMCF

Matrix of dimensional rigid unsplined hinge moment data

RMAT

Matrix containing real part of CMAT. Output by MATMOD option 34.

RMATG

Rectangular matrix defined on DMIG Bulk Data entries and may have an arbitrary number of columns but g-set rows, similar to P2G. Output by MTRXIN.

RMG

Multipoint constraint equation matrix. Output by GP4.

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Glossaries

Data Block Name

Parent Data Block Format

Description

RMSTAB

Table of RMS responses. Output by DOPRAN.

RMSTABR

Table of retained RMS responses in RMSTAB. Output by DSAD.

RMSTBR

Table of retained RMS responses.

RMSVAL

Matrix of initial RMS values. Output by DSARME.

RMSVALR

Matrix of initial values of the retained RMS responses in RMSVAL. Output by DSAD.

RMSVLR

Matrix of retained RMS values.

ROUGV1

OUG

Table of relative displacement, velocity and acceleration in SORT1 format.

ROUGV2

OUG

Table of relative displacement, velocity and acceleration in SORT2 format.

RP

Row partitioning vector.

RPX

Reduction matrix from p-set to h-set (modal) or d-set.

RR2IDR

Table of retained referenced type two response identification list. Output by DSAD.

RSLTDATA

Table of actual results data when system cell 297=3. Output by SDRP.

RSLTSTAT

Table of result-state information when system cell 297=2. Output by SDRP.

RSP12R

RESP12

Table of the count of type 1 responses per response type per subcase in R1TAB. Output by DOPR3.

RSP1CT RSP2RG

Table of retained second level (synthetic) responses in RESP12. Output by DSAD.

RESP12

Table of attributes of the retained second level (synthetic) responses.

RSP3RG

Table of attributes of the retained third level responses.

RSQUERY

Table of results state query.

RSTAB

Matrix of dimensional rigid stability derivatives generated directly from the aerodynamic model.

RUG

Residual matrix for the g-set. Output by STATICS.

RUL

Residual matrix for the l-set. Output by SSG3.

RUO

Residual matrix for the o-set. Output by SSG3.

Data Block Name

Parent Data Block Format

Description

SABFIL

Table of SOL 200 related information regarding the RANDPS data, frequency responses, and load PSD values associated with constrained PSD responses.

SCSTM

Table of global transformation matrices for partitioned superelements. Output by SEP1X.

SELIST

Table containing the list of partitioned superelements defined in separate Bulk Data sections. Output by SEPR1.

SELOAD

DTI table for SELOAD bulk entry images.

SEMAP

SEMAP

Mapping matrix for resequencing. Output by SEQP.

SEQMAP SET

Superelement map table. Output by SEP1 or SEP1X.

SET

Table of combined sets. Output by NASSETS.

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Data Block Name

Glossaries

Parent Data Block Format

Description

SETMC

Table of SETMC Case Control definitions.

SETREE

Superelement tree table usually input via the DTI,SETREE Bulk Data entry.

SGPDT

Superelement basic grid point definition table. Output by SEP1X.

SGPDTS

Superelement basic grid point definition table for the current superelement. Output by SEP2X.

SGPDTS*

Family of SGPDTS tables created in previous runs.

SHPVEC

Matrix of basis vectors - coefficients relating designed grid coordinates and design variables. Output by DOPR2.

SIL

Scalar index list. Output by GP1.

SIL0

SIL table from a previous adaptivity index in p-version analysis.

SILD

Scalar index list for the p-set. Output by DPD.

SKJ

Integration matrix. Output by AMG.

SLGRIDS

List of selected grids (for DATTYP=2).

SLIST

Superelement processing list to matrix generation, assembly, and reduction. Output by SEP3.

SLT

Table of static loads. Output by GP3.

SLT1

Table of static loads updated for nonlinear analysis. Output by NLCOMB.

SLTH

Table of static loads updated for heat transfer analysis. Output by SSG1.

SMPF

Matrix of contribution of structure to fluid mode participation factors. Output by MODEPF.

SNORM*

Family of shell normal vectors at superelement boundaries.

SNORMS

Table of shell normal vectors on a superelement’s boundary. Output by TASNP1.

SORTBOOL

Square matrix containing unity at a row position in the column associated with the sorted row terms. Output by MATMOD option 35.

SORTLIST

Vector consisting of the row numbers of the original positions of the sorted terms. Output by MATMOD option 35.

SPAN1RG

Global table of DRSPAN related DRESP1 information.

SPAN23

Table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

SPANSV

Relevant DRSPAN related internal DRESP1 IDs and their values for the current DSAD call.

SPANSVG

Global form of SPANSV, containing information from all DSAD calls in the analysis types loop.

SPCCOL

Local f-size partitioning vector with 1.0 for the local boundary’s s-set degrees-of-freedom. Required only for geometric domain decomp.

SPCPART

Partitioning vector for domain decomposition. Output by SEQP.

SPECSEL

Response spectra input correlation table.

SPLINE

Table of SETi, AELIST, and SPLINEi Bulk Data entry images with external grid identification numbers. Output by MKSPLINE.

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Data Block Name

Parent Data Block Format

Description

SPSEL

Table of response spectra generation correlation selections.

SRKS

Matrix of monitor point rigid body vectors. Output by MONVEC.

SRKT

Matrix used to sum the forces and moments acting on the k-set degrees-of-freedom to the reference point. Output by ADG.

STATDATA

Table of state information when system cell 297=1. Output by SDRP.

STBDER

Table of aerostatic stability derivatives for a single subcase. Output by SDP.

STBTAB

Table of aerostatic stability derivatives for all subcases.

STRUCOMP

Table of structural components when MESH=’STRU’. Output by MAKCOMP.

SVEC

Starting "random" eigenvector matrix.

SZR

Merged monitor matrices. Output by MRGMON.

SZRi

Associated monitor matrices

Data Block Name

Parent Data Block Format

Description

T

Table information to support MATGEN module options. Diagonal from symmetric decomposition. Output by MATMOD option 21.

TA

Secondary table to be merged into TOLD to form TNEW.

TAB

Table.

TABi

Tables.

TABDEQ

Table of unique design variable identification numbers. Output by DOPR4.

TABECN

Table of relationship between internal identification numbers of constraints in ESTDCN and elements and responses in R1TABR. Output by DSAF.

TABEVP

Cross-reference table between ESTDVP records and element and design variable identification numbers. Output by DSABO.

TABEVS

Cross reference table between ESTDVS records and element and design variable identification numbers. Output by DOPR6.

TABEV2

Merged cross reference table of TABEVP and TABEVS. Output by DSAE.

TB

Secondary table to be merged into TOLD to form TNEW.

TC

Secondary table to be merged into TOLD to form TNEW.

TEF

Directory table for MEF. Output by DRMH1 and DRMS1.

TEL

Transient response time output list appended from each subcase. Output by NLTRD and NLTRD2.

TEMF

Total effective mass fraction table. Output by EFFMAS.

TES

Directory table for MES. Output by DRMH1 and DRMS1.

TFPOOL

Table of TF Bulk Data entry images. Output by DPD.

TIMSIZ

Table of CPU and disk space estimation parameters. Output by SEQP.

TNEW

Table data block to be edited by TABEDIT.

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Data Block Name

Glossaries

Parent Data Block Format

Description

TNSPAN23

DOPR3 module updated temporary copy of SPAN23, the table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

TOFPi

Directory table for MOFPi. Output by DRMH1 and DRMS1.

TOL

TOL

Transient response time output list. Output by IFT, TOLAPP, TRD2 and TRLG.

TOL1

TOL

Transient response time output list reduced by the OTIME Case Control command or for the current nonlinear transient subcase. Output by MODACC and TOLAPP.

TOLD

Table data block to be edited by TABEDIT.

TOUT

DRMH1 directory table in table data block or DTI format.

TQG

Directory table for MQG. Output by DRMH1 and DRMS1.

TR

Matrix to transform forces from the support point to the aerodynamic reference point. Output by MAKETR.

TRANTR

Transpose of TR where the number of columns of TR matches the URDDUXV states of TRX. Both are reduced to just the active origin rigid body degrees-of-freedom. Output by MAKETR.

TRL

Transient response list. Output by DPD.

TRX

Boolean matrix to select accelerations from the list of aerodynamic extra points. Output by ADG.

TSPAN23

Temporary copy of SPAN23, the table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

TUG

Directory table for MUG. Output by DRMH1 and DRMS1.

TXY

DRMH1 directory table in DTI or table data block format. Output by DRMH1.

Data Block Name

Parent Data Block Format

Description

U

Upper triangular factor. Output by DECOMP and DCMP.

U1

U truncated by the OFREQ or OTIME or OMODES command.

U7DOF

U7-set DOF vector (input DOF) for superelement.

U8DOF

U8-set DOF vector (output DOF) for superelement.

UA

Displacement or eigenvector matrix in the a-set or solution matrix on the boundary (a-set) of the superelement (identification number equal to output value of SEID).

UACCE

Reduced acceleration solution matrix from transient response analysis. Output by DSAR.

UAJJT

Upper triangular decomposition factor matrix of AJJT.

UAM1DD

Upper triangular factor of the dynamic tangential matrix in the d-set.

UD

Solution matrix for the d-set. Displacements only in frequency response. Displacements, velocities, and accelerations in transient response.

UD1

Improved solution matrix for the d-set. Output by DDR2.

UDISP

Reduced displacement solution matrix from transient response analysis. Output by DSAR.

UE

Improved solution matrix for the e-set (extra points). Output by DDR2.

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Data Block Name

Parent Data Block Format

Description

UG

Displacement matrix in g-set. For the DSVG1 module and transient analysis, UG can also represent velocity or acceleration. Output by SDR1 and STATICS.

UGD

Displacement matrix in g-set for the downstream superelement.

UGDS

Displacement matrix in g-set due to pseudo-loads.

UGDS1

Displacement matrix in g-set for the total variation. Output by DSVG3.

UGG

Displacement matrix in g-set for all processors (global). Output by DISUTIL.

UGLCURB

Global displacements in basic coordinate system.

UGNI

Displacement matrix at converged step in the g-set. Output by NLITER.

UGNT

Total displacement matrix in the g-set. Output by UGVADD.

UGT

Updated temperature matrix in g-set. Output by MATMOD option 19.

UGX

Matrix of analysis model displacements in g-set or p-set.

UGX1

Copy of UGX matrix with null columns in place of the deleted responses. Output by DSAD.

UH

Solution matrix for the h-set (modal degrees-of-freedom). Modal displacements only in frequency response. Modal displacements, velocities, and accelerations in transient response.

UHD

Modal velocities solution matrix for the h-set (modal degrees-of-freedom). Required only for frequency response.

UHFF

Fluid partition (row-wise) of solution matrix UHF. Also partitioned column-wise according to parameter FLUIDMP.

UHFS

Structural partition (row-wise) of solution matrix UHF. Also partitioned column-wise according to parameter STRUCTMP.

UHR

Modal displacement vector for spectral analysis. Output by INTERR.

UL

Displacement matrix in l-set. Output by SSG3.

ULAMA

Unsymmetric eigenvalue summary table. Output by UEIGL.

ULL

Upper triangular factor for the l-set from KLL.

ULLT

Upper triangular factor for nonlinear elements including material, slideline, and differential stiffness effects.

ULNT

Solution matrix from nonlinear transient response analysis in the d-set. Output by NLTRD and NLTRD2.

UNITS

UNITS data block from the DTI,UNITS bulk data entry.

UO

Displacement matrix in o-set. Output by SSG3.

UOO

Displacement matrix in o-set due to applied loads on the o-set with the a-set fixed (set to zero).

UPSDT

Table of transfer function data needed for RMS calculations.

URDDIDX

An instance of an ADBINDX that describes the acceleration entries. Output by MAKETR.

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Data Block Name

Glossaries

Parent Data Block Format

Description UX vector states for the active URDDi. These are rows of TRX that are non-null. Null rows occur either because the USER didn’t define AESTAT, URDDi, OR because the associated URDDi is invalid for this symmetry condition (e.g., URDD1,3,5 are invalid for antisymmetric analysis). Output by MAKETR.

URDDUXV

USET

USET

Degree-of-freedom set membership table for g-set. Output by GPSP.

USET0

USET

Degree-of-freedom set membership table for g-set usually prior to Auto-SPC update in GPSP. Output by GP4. USET table from a previous adaptivity index in p-version analysis.

USET1

USET

USET updated with constraints from upstream superelements. Output by BNDSPC.

USETD

USET

Degree-of-freedom set membership table for p-set. Output by DPD.

USETM

USET

Modified degree-of-freedom set membership table for g-set. Output by MODUSET.

UVELO

Reduced velocity solution matrix from transient response analysis. Output by DSAR.

UX

Matrix of aerodynamic extra point displacements. Output by ASG.

UXDAT

Table of aerodynamic extra point identification numbers, displacements, labels, type, status, position and hinge moments. Output by ASG.

UXDIFV

Derivative interpolation factors matrix at UX = UXREF. Output by ASG and SDP.

UXF

Solution matrix from frequency response analysis in d- or h-set. Output by FRRD1 or FRRD2.

UXR

Matrix of aerodynamic extra point vectors for use in calculating the sensitivity of restrained stability derivatives. Output by DSARLP.

UXT

Solution matrix from transient response analysis in d- or h-set. Output by TRD1, TRD2, and IFT.

UXT1

Reduced solution matrix from transient response analysis. Output by DSAR.

UXTRIM

UX vector at trim.

UXU

Matrix of aerodynamic extra point vectors for use in calculating the sensitivity of unrestrained stability derivatives. Output by DSARLP.

UXV

Control state matrix for ADB or AEDB

UXVBRL

Controller state matrix for WJVBRL downwash vectors. UXVBRL has NX rows and NV columns. Output by ADG.

UXVF

Matrix of UXVEC vectors defined by the AEFORCE Bulk Data entries. Ouptut by MAKAEFA.

UXVP

Matrix of UXVEC vectors defined by the AEPRESS Bulk Data entries. Ouptut by MAKAEFA.

UXVST

Aerodynamic extra point displacement matrix. Output by MAKAEFS.

UXVW

Matrix of UXVEC vectors defined by the AEDW Bulk Data entries. Ouptut by MAKAEFA.

Data Block Name

Parent Data Block Format

Description

V01P

Partitioning vector for sparse load reduction.

VAXWN

Modified VAXW corresponding to USETN.

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Data Block Name

Parent Data Block Format

Description

VDXC

Partitioning vector with 1.0 at rows corresponding to null columns in KDD, BDD, and MDD.

VDXR

Partitioning vector with 1.0 at rows corresponding to null rows in KDD, BDD, and MDD.

VELEM

Table of element lengths, areas, and volumes. Output by ELTPRT.

VELEMDCN

Table of element lengths, areas, and volumes which incorporates combined constraints and design variables. Output by DSAF.

VELEMN

Table of element lengths, areas, and volumes for the perturbed configuration. Output by ELTPRT.

VFO1

VFO zero-partition by SPCCOL. VFO is the local f-size partitioning vector with 6 values of 1.0 for every grid in the local residual. Required only for geometric domain decomp.

VG

Left-handed displacement matrix in g-set. Divergence and flutter analysis only.

VGA

G-set size partitioning vector with values of 1.0 at the rows corresponding to the a-set.

VGF

Fluid/structure partitioning vector with ones at the rows corresponding to fluid degrees-of-freedom. Output by GP1.

VGFD

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to frequency-dependent elements. Output by TA1.

VGA

G-set size partitioning vector with values of 1.0 at the rows corresponding to the a-set.

VGQ

Partitioning vector with values of 1.0 at rows corresponding to degrees-of-freedom in the q-set.

VIEWTB

VIEWTB

View information table, contains the relationship between each p-element and its view-elements and view-grids. Output by VIEWP.

VIEWTBDS

VIEWTB

View information table, contains the relationship between each p-element and its view-elements and view-grids for the perturbed model. Output by DVIEWP. Table of flutter sensitivity data. Output by DSFLTE.

VTQU

Data Block Name

Parent Data Block Format

Description

WGTM

Table of 6x6 rigid body mass matrix. Output by WEIGHT.

WJ

Gust matrix. Output by GUST.

WMID

Table of weight as a function of material identification number. Output by WEIGHT.

WRJVBRL

Downwash matrix (NJ rows by NV columns). Downwash at the j-points due to the linear, angle/rate rigid body aerodynamic extra-points and linear control surfaces. Output by ADG.

WSKJF

Weighted integration matrix.

WTCRID

Table of retained weight responses with column and row numbers in rigid mass matrix. Output by DSAW.

WTDSCP

Partitioning vector for weight. Output by DSAW.

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Data Block Name

Glossaries

Parent Data Block Format

Description

X

Solution of the equation [A][X]=[B]. Output by FBS, SOLVE, and SOLVIT. Matrix product. Output by MPYAD and SMPYAD. Matrix transpose. Output by TRNSP.

X66

Triple-product of XG with rigid body modes for IOPT=9 or 10. Output by VECPLOT.

X66P

Previous output of X66, usually at g-set. Used by IOPT=9, when setnam’g’, as a baseline to compare against the non-g-set results in X66.

XAA

Reduced square matrix in a-set. Output by MATREDU.

XAA*

Family of reduced square matrices in a-set pertaining to the upstream superelements.

XD

Rectangular matrix of displacements or loads in the p-set. Output by UREDUC.

XDD

Reduced square matrix in d-set. Output by MATREDU.

XDICT

KDICT

Baseline element matrix dictionary table.

XDICTDS

KDICT

Perturbed element matrix dictionary table. If CDIF=’YES’ then this is the forward or backward perturbed element matrix dictionary.

XDICTX

KDICT

Baseline element matrix dictionary table or backward perturbed element matrix dictionary if CDIF=’YES’.

XELM

KELM

Baseline element matrices. Output by EMG.

XELMDS

KELM

Table of perturbed element matrices. If CDIF=’YES’ then this is the forward or backward perturbed element matrix dictionary.

XELMX

KELM

Baseline element matrices or backward perturbed element matrices if CDIF=’YES’.

XG

Rectangular matrix of displacements or loads in the g-set.

XGG

Square matrix in g-set. In superelement analysis, XGG includes contributions from upstream superelements. Output by EMA and SEMA.

XGGi

Square matrices in g-set. Output by EMA and SEMA.

XH

Rectangular matrix of displacements or loads in the h-set (modal). Output by UREDUC.

XINIT

Matrix of initial values of the design variables. Output by DOPR1.

XJJ

Square matrix for the g-set of the current superelement and applied to its interior points only.

XNNi

Square matrices in n-set. Output by MCE2.

XO

Matrix of final (optimized) values of the design variables.

XORTH

Cross-orthogonality matrix. Output by CEAD and UEIGL.

XOUT

Resultant to table output. Output by VECPLOT.

XP

Rectangular matrix of displacements or loads in the p-set

XPP

Square matrix in p-set.

XS

Optional starting vector, same type as B and PG in SOLVIT and STATICS, respectively. Rectangular matrix of displacements or loads in the s-set. Output by UREDUC.

XSELOAD

Table of DTI,SELOAD definitions of the external superelement consistent with the applied loads.

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Data Block Name

Parent Data Block Format

Description

XSF

S-set by f-set matrix partition of XGG or XPP after multipoint constraint elimination and reduction. Output by MATREDU.

XSS

S-set by s-set matrix partition of XGG or XPP after multipoint constraint elimination and reduction. Output by MATREDU.

XYCDB

Table of x-y plotting commands. Output by IFP1.

XYCDBDR

Table of x-y plotting commands for a superelement (identification number equal to output value of SEID). Output by SEDR.

XYCDBS

Table of x-y plotting commands for the current superelement (identification number equal to output value of SEID). Output by SEP2CT.

XYPLOT

Table of x-y plot control values. Output by XYTRAN.

XZ

Matrix containing the constant portion of the dependent to independent design variable linking relationship. Output y DOPR1.

Data Block Name

Parent Data Block Format

Description

YGBNDR

Boundary shape matrices appended for all auxiliary or geometric models.

YPF

Frequency response enforced motion matrix in the p-set. Output by FRLG.

YPO

Transient response enforced motion matrix in the p-set and for the output time steps. Output by TRLG.

YPT

Transient response enforced motion matrix in the p-set. Output by TRLG.

YS

Matrix of enforced displacements or temperatures. Output by GPSP.

YS0

Matrix of enforced displacements temperatures usually prior to Auto-SPC update in GPSP. Output by GP4.

YS1

YS updated with enforced displacements from upstream superelements. Output by BNDSPC.

YSD

Accumulated matrix of enforced displacements from upstream superelements.

YSD1

YSD updated with enforced displacements from upstream and current superelements to be passed to downstream superelements. Output by BNDSPC.

YSMAT

Initial and final enforced displacement matrices.

Data Block Name

Parent Data Block Format

Description

ZETA

Diagonal matrix of modal damping coefficients as produced by the GKAM module.

ZETAH

Mass-normalized damping.

Z1ZX

Matrix of unrestrained dimensional elastic derivatives

ZZX

Reduced aerostatic solution matrix.

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Data Block Naming Conventions Stiffness, Damping, and Mass: K_____

Stiffness

KD____

Differential stiffness

B_____

Viscous damping

K4____

Structural damping (See GE field on MATi entries)

__2DD

Stiffness in dynamic formulation

M____

Mass

___JJ

Stiffness, damping, and mass matrices without upstream superelement contributions. Exception: __AJJ_ is the aerodynamic influence matrix.

L__, U__

Lower and upper triangular decomposition factors

Note Some of the above names may be prefixed with a "C" to indicate a complex matrix. Superelements: CM____

Superelement (component) modes

_____S

Assigned only to SEP2 and GP1 module outputs

__LIST

Superelement processing list; for example, SLIST, DRLIST, and DSLIST

MAPS

Superelement boundary grid map

SEMAP

Superelement map

Loads and Solutions: A_____

Aeroelastic or aerostatic

B_____

Buckling

C_____

Complex modes

CY____

Cyclic symmetry

F_____

Flutter

_____F

Frequency response

_____T

Transient response

___NL_

Nonlinear static or transient response; for example, USETNL, ESTNL and OESNLX

_____NI

Nonlinear static or transient response generated in a nonlinear loop.

___PH__

Eigensolution

PH____

Normal modes eigenvector matrix; for example, PHG (g-set) and PHA(a-set)

CPH___

Complex modes eigenvector matrix; for example, CPHD (d-set) and CPHL (l-set).

BPH___

Buckling eigenvector matrix; for example, BPHA (a-set)

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Solutions: ___U___

Static and dynamics (except eigen-) solution; for example, CYUG is the cyclic static solution g-set

___Q___

Single point forces of constraint in statics and dynamics solution; for example, QG, QPT, and CYQG. Also aerodynamic matrices; for example, QHH, QKHL, and QLL

___QM__

Multipoint forces of constraint in statics and dynamics solution; for example, QMG, QMPT, and CYQMG

CMPH___

Component modes eigenvector matrices.

__LAMA

Eigenvalue summary table; for example, LAMA, BLAMA (buckling), CLAMA (complex), and CMLAMA (component modes)

__UH__

Dynamic solution at modal degrees-of-freedom; for example, AUHF is the Aeroelastic solution h-set

__OL__

Dynamic output list; for example, FOL (frequency) and TOL (transient).

___NT__

Nonlinear transient response; for example, UPNT and ULNTH

_____N

Nonlinear static solution appended for all loops; for example, UGN and QGN

Loads: P_____

Dynamic and static loads

Y___

Enforced displacement

PA

Static loads a-set

PJ

Static loads g-set (no upstream loads)

PG

Static loads g-set

PP____

Dynamic loads p-set

PH____

Dynamic loads h-set

__PPF_

Dynamic loads p-set, frequency response

__PPT_

Dynamic loads p-set, transient response

__UH__

Dynamic solution at modal degrees-of-freedom

__UG__

Static solution g-set; for example, UGN is the nonlinear solution at the g-set.

__UL__

Static or dynamic solution l-set; for example, ULN is the nonlinear solution at the g-set.

__UP__

Dynamic solution p-set; for example, UPN is the nonlinear transient solution at the p-set.

Solution Output Tables: O__ES__

Element stresses (STRESS=n)

O__GPS__

Grid point stresses (GPSTRESS=n)

O__GPF__

Grid point forces (GPFORCE=n)

O__NRG__

Element strain energy (ESE=n)

O__EF__

Element forces (FORCE=n)

O__EE__

Element strains (STRAIN=n)

O__STR__

Element strains (STRAIN=n)

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O__UG__

Static solution (DISP=n)

O__UP__

Dynamic solution (DISP=n)

O__QG__

Static spcforces (SPCF=n)

O__QMG_

Static mpcforces (MPCF=n)

O__QP__

Dynamic spcforces (SPCF=n)

O_____1

SORT1 format

O_____2

SORT2 format

Miscellaneous: __CASE__

Case Control section tables; for example, Outputs from IFP1, SEP2 and SEDRDR are CASECC, CASES, and CASEDR.

___CDB_

Control data blocks from the OUTPUT(XY_____), OUTPUT(PLOT), and OUTPUT(POST) sections; for example, Outputs from IFP1, SEP2, and SEDRDR are POSTCDB, PCDBS, and PCDBDR.

GEOM__

Table of Bulk Data entry images related to geometry, connectivity, static loads, and degree-of-freedom set membership.

USET__

Degree-of-freedom set; for example, USET0 (from GP4), USET (from GPSP), and USETD (from DPD).

_GPDT_

Grid point definition tables; for example, BGPDT and GPDT.

CSTM_

Coordinate Systems Transformation matrix tables; for example, CSTM, CSTMS, CSTMA

O_____

Solution output tables; for example, OCYES1 is cyclic statics, element stresses, and SORT1. OCPHQP1 is complex modes, SPCForces, and SORT1. OUG2 is statics, displacements, and SORT2.

_EST__

Element summary table; for example, Outputs from TA1 are named EST and ESTL. Output from NLITER and NLTRD is named ESTNL.

_DICT_

Dictionary table for element stiffness, mass, etc.; for example, KDICT (linear), KDDICT (differential), KDICTNL (material nonlinear), MDICT (mass)

_ELM_

Element stiffness, mass, etc.; for example, KELM (linear), KDELM (differential), MELM (mass)

_____1

MODACC module outputs. (OTIME and OFREQ); for example, ULF1, FOL1

_____1X

SDRX and SDRXD module outputs; for example, OES1X, OEF1X

Inconsistent Names: BUG

Buckling eigenvector matrix; should be renamed to BPHG.

GM

Transformation between m-set and n-set; should be renamed to GMN.

POS

Static loads on the o-set; should be renamed to PO.

PSS

Static loads on the s-set; should be renamed to PS.

DM

Transformation between l-set and r-set; should be renamed to DLR.

MR

Rigid body mass matrix (r-set by r-set); should be renamed to MRR.

MRR

Stiffness matrix partition (r-set by r-set) from MTT; should be renamed to MRR1.

__V__

Obsolete designation indicating "vector"; for example, OUGV1, UGVS, UHVF.

__PHI__

Obsolete designation indicating eigensolution; for example, PHIDH (should be PHDH)

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PHDH

Transformation from d-set to h-set; should be renamed to PHD.

6.2 Parameter Glossary The parameter Glossary lists the names and a brief description of all parameters shown in the module descriptions in “Descriptions of DMAP Modules and Statements” . Naming conventions appear at the end of the glossary. Name

Type and Description

ACMS

Character. Automatic Component Mode Synthesis flag. If ACMS=’YES’, then the model will be automatically partitioned into superelements according to NTIPS, TIPSCOL, AND ZCOLLCT.

ACON

Integer. B-set constraint flag. If ACON65535 rows) format flag.

BITID

Integer. Bit position of a degree-of-freedom set.

BOV

Real. Conversion from frequency to reduced frequency. Value calculated by REFC/(2.*VELOCITY). Output by APD.

BOXIDF

Integer. Box corner point identification flag. Output by APD. 0

Points have unique identification numbers starting with the aerodynamic component identification number.

-1

Points identification numbers are incremented by 1, to avoid an overlap if they were started with the aerodynamic component identification numbers. No display of the corner points is possible.

BSKIP

Logical. Pre-buckling subcase skip flag. If TRUE, the skip first subcase in CASECC.

BTBRS

Real. Parameter for electromagnetic analysis.

BUCKCC

Logical. Buckling analysis subcase flag. Set to TRUE if at least one ANALYSIS=BUCK command was found in CASECC and CASEBUCK is specified in the output list. Output by MDCASE.

BULKFGi

Integer. Bulk Data entry record existence flag. Set to -1 if Bulk Data entry record exists. Output by PARAML.

BULKNMi

Integer. Bulk Data entry name.

CARDNO

Integer. Punch file line counter. CARDNO is incremented by one for each line written to the punch file and is also written into columns 73-80 of each line. Output by XYTRAN.

CASCOMi

Character. Case Control command names.

CFDFLG

Integer. Central finite difference flag.

CDIF

1

Forward

-1

Backward

Character. Finite difference scheme. ’YES’

Central

’NO’

Forward

CDITER

Integer. Maximum number of iterations in a constrained displacement analysis.

CHAR

Character. Character value of table element. Output by PARAML.

CHAR2

Character. Character value of table element concatenated from the values in the WRDNUM and WRDNUM-th position. Output by PARAML.

CHARi

Character. Character value for PRGNAME.

CHOLSKY

Integer. Cholesky decomposition flag. Real. Close natural frequency scale factor. Under the OPTION=’ABS’ method, close natural frequencies will be summed if the natural frequencies satisfy:

CLOSE

CLOSEOPT

Integer. FORTIO close options.

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Name

Glossaries

Type and Description 1

Rewind (leaves file open, if open)

2

Close/keep (default)

3

Close/delete

CMPDIF

Integer. If CMPDIF=1, the comparison between DB1 and DB2 found differences. Only valid for DB1 and DB2 existing with DLSTIN purged.

CMPLX

Complex single-precision value.

CMPLXD

Complex double-precision value.

CMPX

Complex. Complex value in the next record.

CMPXD

Complex double precision. Complex double precision value in the next record.

CMPXi

Complex. Complex value for PRGNAME.

CNCNT

Integer. Counter for constraints in CONTAB. Output by DOPR3.

CNVFLG

Integer. Design optimization convergence flag. Output by DOM12. 0

No convergence is achieved

1

Soft convergence is achieved

2

Hard convergence is achieved

COLINC

Integer. Column increment. Extract every COLINC’th column between STARTCOL and ENDCOL.

COLNAM

Character. Degree-of-freedom set name for labeling matrix rows MATGPR output.

COLNUM

Integer. Selects the column number of the input matrix that will be sorted to produce SORTLIST and SORTBOOL. Default selects the first column.

COMPRPLC

Logical. If TRUE then components with duplicate names will be copied from COMP1 into COMP.

CONFAC

Integer. Image superelement congruence tolerance for the location of boundary grid points and displacement coordinate systems.

CONSEC

Integer. A composite number equal to 10*(value of NSTEP the last time MAXBIS was reached) + (the number of consecutive time steps which have reached MAXBIS). If CONSEC=5, then solution process is terminated. Output by NLTRD and NLTRD2.

CONV

Integer. Nonlinear analysis convergence flag. Output by NLITER, NLTRD, and NLTRD2. On input: 0

Initialization

On output: -1

Convergence has not been achieved

1

Convergence has been achieved.

COORID

Integer. Coordinate system identification number.

COUPMASS

Integer. Coupled mass generation flag. -1

Lumped

0

Coupled

CP

Integer. DBC module control parameter. Output by DBC.

CSTRN

Integer. Composite lamina strain constraint flag. Set to >0 if any constraint. Output by DSPRM.

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Name

Type and Description

CSTRES

Integer. Composite lamina stress constraint flag. Set to >0 if any constraint. Output by DSPRM.

CTYPE

Character. Cyclic symmetry type as specified on CYSYM Bulk Data entry. Output by CYCLIC1.

CVTYP

’ROT’

Rotational

’AXI’

Axisymmetric

’DIH’

Dihedral

Integer. Type of convergence test. 1

Soft convergence is to be checked

2

Hard convergence is to be checked

3

Final iteration histories are to be printed

CYCLIC

Logical or integer. Set to TRUE or -1 for cyclic symmetry models.

DATAREC

Integer. Data recovery flag. If DATAREC>0, then DPD will not perform UFM 2071 checks for DELAY and DPHASE which are not need in data recovery.

DATTYP

Integer. Data type. 1

Panel contributions

2

Grid contributions

3

Reciprocal panel contributions

DBCPATH

Integer. Dummy variable parameter to allow passing of qualifiers from the NASTRAN database to the DBC database.

DCEIGCC

Logical. Direct complex eigenvalue analysis subcase flag. Set to TRUE if at least one ANALYSIS=DCEIG command was found in CASECC and CASECEIG is specified in the output list. Output by MDCASE.

DEBUG

Integer. Passive column logic control flag in DCMP and DECOMP.

DECOMP

Integer. DCMP and DECOMP module error termination flag.

DEFORMED

Integer. Deformed plot request flag. 1

Plot undeformed shapes

-1

Plot deformed shapes

DEFRMID

Integer. Element deformation set identification number. Usually obtained from the DEFORM Case Control command. Required for use in stress recovery of differential stiffness.

DELG

Real. Scale factor on perturbed length.

DELTAB

Real. Relative finite difference move parameter as specified on the DOPTPRM Bulk Data entry and stored in the OPTPRM data block.

DELTAD

Complex double precision. This is the scalar multiplier for [D].

DESCYCLE

Integer. Design cycle analysis counter or flag.

DESGLB

Integer. DESGLB Case Control command set identification number. Output by DOPR3 and MDCASE.

DESITER

Integer. Design optimization iteration number.

DESMAX

Integer. Maximum allowed design optimization iteration number.

DESOBJ

Integer. DESOBJ Case Control command set identification number. Output by DOPR3 and MDCASE.

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Glossaries

Name

Type and Description

DESOPT

Integer. Non-composite element force flag. If set to 1, then the non-composite element forces are extracted form OEF1A and copied to OEF1AA.

DESPCH

Integer. Punch control for updated DESVAR, DREPS1 and GRID Bulk Data entries. See “DESPCH” in the NX Nastran Quick Reference Guide .

DESVAR

Integer. Retained DVPRELi or DVGRID entry flag for superelement SEID. Set to -1 if there are retained design variable perturbations. Output by SDSA.

DET

Complex. Scaled value of the determinant of a matrix. Output by DCMP and DECOMP.

DETER

Complex. Shift value. Output by DYCNTRL.

DFLAG

Integer. Displacement output flag. 0

Output displacement

1

Do not output displacement

Real. Duplicate frequency threshold. Two frequencies, f 1 and f 2 , are considered duplicates if DFREQ

where fmax and fmin are the maximum and minimum frequencies across all FREQi Bulk Data entries. DFRQCC

Logical. Direct frequency response analysis subcase flag. Set to TRUE if at least one ANALYSIS=DFREQ command was found in CASECC and CASEFREQ is specified in the output list. Output by MDCASE.

DIGITS

Integer. Number of digits for the fractional part of values written by the OUTPUT4 module.

DISMETH

Integer. Method of processing in DISUTIL module.

DISVAR

Logical. Discrete optimization variable flag. Set to TRUE if discrete optimization design variables are specified. Output by DOPR1.

DMRESD

Integer. Design model flag. If set to -1, then the design model is limited to the residual structure. Output by SDSB.

DOANALY

Integer. Any analysis retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOBUCK

Integer. Buckling constraint flag. Set to >0 if any constraint. Output by DSPRM.

DOCEIG

Integer. Complex eigenvalue response retained response flag. Set to >0 if any retained response.

DODIVG

Integer. Divergence analysis retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOESE

Integer. Static analysis retained element strain energy response flag. Set to >0 if any retained response. Output by DSPRM.

DOFLUT

Integer. Flutter analysis retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOFREQ

Integer. Frequency response retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOFSPC

Integer. Frequency response retained SPCforce response flag. Set to >0 if any retained response. Output by DSPRM.

DOMODES

Integer. Normal modes constraint flag. Set to >0 if any constraint. Output by DSPRM.

DOMTRAN

Integer. Transient response retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOPT

Integer. Scaling method between grid points on the abscissa for the CURVPLOT module.

DORMS

Integer. RMS response retained response flag. Set to >0 if any retained response.

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Name

Type and Description

DOSAERO

Integer. Aerostatic trim or stability derivative retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOSASTAT

Integer. Statics or aerostatic retained response flag. Set to >0 if any retained response. Output by DSPRM.

DOSSPCF

Integer. Static analysis retained SPCforce response flag. Set to >0 if any retained response. Output by DSPRM.

DOSTAT

Integer. Statics constraint flag. Set to >0 if any constraint. Output by DSPRM.

DOTSPC

Integer. Transient response retained SPCforce response flag. Set to >0 if any retained response. Output by DSPRM.

DOWGHT

Integer. Weight retained response flag. Set to >0 if any retained response. Output by DSPRM.

DPEPS

Real. Tolerance for design model override of analysis model properties. See further description in theNX Nastran Quick Reference Guide .

DRESP

Integer. Retained DRESP1 entry flag for superelement SEID. Set to -1 if there are retained design responses. Output by SDSA.

DSAPRT

Logical. DSAPRT Case Control command print flag.

DSENS

Integer. Acceleration matrix creation flag. Set to 1 to generate AG, accelerations due to inertial loads.

DSFLAG

Logical. Design sensitivity flag. Set to TRUE for design sensitivity job.

DSNOKD

Real. Scale factor on the differential stiffness matrix in buckling design sensitivity analysis. Usually specified as a user parameter.

DSVGF

Integer. Specifies scaling of solution vector by eigenvalue. 0

No scaling

1

Scale

DSZERO

Real. Design sensitivity coefficient print threshold. If the absolute value of the coefficient is greater than DSZERO then the coefficient will be printed.

DTMi

Integer. Mode acceleration based displacement matrix flag. If DTMi0, then MOPFi is a mode acceleration based displacement matrix and, therefore, velocities and accelerations will not be output to OFPi. For APP=’TRANRESP’, MOFPi must have only one column per time step instead of the usual three.

DUPWG

Integer. Duplicate word group option in the TABEDIT module.

DVGRDN

Character. Flag for skipping basis vector components associated with all GRIDNs in DESVCP. If DVGRDN=’YES’, then components will be skipped.

DVRGCC

Logical. Aerostatic divergence analysis subcase flag. Set to TRUE if at least one ANALYSIS=DIVERG command was found in CASECC and CASEDVRG is specified in the output list. Output by MDCASE.

EIGNFREQ

Integer. Eigenvalue/frequency response type flag. Output by DOPR3.

ECTYPE

EIGRFLD

1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

Integer. Type of element connectivity input and plot set output: 0

ECT and ELSET

1

GEOM2 and ELSET

2

ECT and PELSET

Character. Field name of EIGR or EIGRL entry. EIGRFLD is also an output if the field value is a character string. Output by MATMOD option 23.

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Glossaries

Name

Type and Description

EIGRVALI

Integer. Extracted integer value from the EIGR or EIGRL entry. Output by MATMOD option 23.

EIGRVALR

Real. Extracted real value from the EIGR or EIGRL entry. Output by MATMOD option 23.

ELEMSET

Integer. SET Case Control command identification number that contains a list element point identification numbers.

ENDCOL

Integer. Ending column number to extract from I1.

ENFM

Integer

EPPRT

Real. Singularity print parameter. Singularities greater than EPPRT will not be printed if PRGPST=’YES’.

EPS

Real. Convergence criterion. By default EPS will be set to N/10000 where N is the size of KXX, etc.

EPSBIG

Real. Large number for tuning.

EPSI

Integer. Static solution error ratio flag. Set to -1 if the error ratio is greater than 1.E-3. Output by SSG3 and DISUTIL.

EPSLND

Complex double precision. This is the scalar multiplier for [E].

EPSMALC

Real. Small number for tuning.

EPSNO

Integer. Number of eigensolutions to check and the quantity of error checking output. If left at its default value, only the highest epsilon for the first ten or NEIGV modes (whichever is less) are printed. If EPSNO is greater than zero, the epsilons for the first EPSNO are printed.

EPZERO

Real. Singularity test parameter. Singularities greater than EPZERO will not be constrained.

EQVBLK

Logical. Copy/equivalence flag of BULKOLD to BULK. If on input EQVBLK=FALSE, and no new Bulk Data then copy BULKOLD to BULK. If on input and output EQVBLK=TRUE and no new Bulk Data, then BULKOLD must be be equivalenced to BULK in a subsequent EQUIVX statement. If there are any new Bulk Data then EQVBLK will be set to FALSE on output. xsort.

ERR

Integer. Bad factor diagonal ratio flag. Output by DCMP and DECOMP.

ERROR

Integer. Duplicate element identification flag. Output by ELTPRT.

ETYPE

Character. Energy type. Inputs to VDRE.

EXISTS

EXTNAME

6-62

Enforced motion flag. Set to ‘0’ if no enforced motion. Set to ‘1’ if enforced motion exists. Output by LCGEN.

‘SEC’

Strain energy - constant.

‘SED’

Strain energy - oscillating.

‘KEC’

Kinetic energy - constant.

‘KED’

Kinetic energy - oscillating.

‘TOTC’

Total energy - constant.

‘TOTD’

Total energy - oscillating.

Character. Project and version status. Output by PROJVER. ’EXISTS’

If project and version exists

’DELETED’

If project and version is deleted

’NONE’

If project and version never existed

Character. Name of the qualifier used to identify External Superelements. Note linkage to the SEBULK data entry.

DMAP Programmer’s Guide

Glossaries

Name

Type and Description

EXTRN

Integer. External superelement flag. Set to -1 if superelement is defined by the CSUPER Bulk Data entry with PEID=0. Output by SEP2DR and SEDRDR.

EXTWORK

Real. External work. Output by SSG3.

F1

Real. The lower frequency bound in cycles per unit time in READ and UEIGL. Tolerance for treating small values as zero during decomposition in DCMP and DECOMP. Maximum value to print in MATGPR output.

F2

Real. The upper frequency bound in cycles per unit time in READ and UEIGL. The default value of 0.0 indicates machine infinity.

FAC1

Complex. Square of the reciprocal of the time step increment. Imaginary part is always zero. Output by TRLG.

FAC2

Complex. Reciprocal of twice the time step increment. Imaginary part is always zero. Output by TRLG.

FAC3

Complex. Negative of the reciprocal of the time step increment. Imaginary part is always zero. Output by TRLG.

FACTOR

Integer. Factor in the computation of the sequenced identification number (SEQID) in the SEQP module.

FAILI

Integer. Composite failure index constraint flag. Set to >0 if any constraint. Output by DSPRM.

FBTYP

Integer. Forward or backward pass selection.

FCSENS

Integer. Flutter/complex eigenvalue sensitivity flag.

Fij

Integer. Form of output matrix partitions.

FILTERF

Real. Filter for fluid factor matrices.

FILTERS

Real. Filter for structure factor matrices.

FIRSTBA

Logical. Zero frequency truncation flag. Set to TRUE if first frequency is truncated. Output by FRRD1 or FRRD2.

FLOOP

Integer. Flutter eigenvalue analysis loop counter. Set to zero for initial entry and incremented by one for each loop until the last loop then set to -1. Output by FA1.

FLUID

Logical. Fluid processing flag. GKAM

If TRUE, then modal damping set identification number is obtained from the SDAMPING(FLUID) Case Control command.

READ and LANCZOS

METHOD command option (FLUID or STRUCTURE). If FLUID=TRUE, the EIGRL entry is selected from METHOD(FLUID) Case Control command.

FLUIDMP

Integer. Number of fluid modes to use in computing factors. If FLUIDMP>0 then compute factors for the first FLUIDMP modes.

FLUIDSE

Integer. Fluid superelement identification number. Set to a value greater than zero if ACMS=’YES’ and fluid elements are present. Output by SEQP.

FLUTCC

Logical. Flutter analysis subcase flag. Set to TRUE if at least one ANALYSIS=FLUTTER command was found in CASECC and CASEFLUT is specified in the output list.

FLXONL

Integer

FLEXONLY keyword from ADAMSMNF case control entry. Set to ‘0’ to solve residual structure. Set to ‘1’ to not solve residual structure. Output by NXNADAMS.

FLXERR

Integer

Error flag. Set to ‘0’ for no error. Set to ‘1’ if error occured during MNF creation (process should be terminated). Output by NXNADAMS.

FMODE

Integer. The lowest mode number resulting from LMODES or LFREQ and HFREQ.

FMPFEPS

Real. Threshold for filtering out small fluid factor magnitudes.

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Name

Type and Description

FORM

Integer. Form of output matrix.

FORMAT

Character. Eigenvalue problem type. Must specify ’MODES’. Buckling problems are not supported.

FOUND

Integer. Integer value search flag. Set to -1 if integer value is found by PARAML. Output by PARAML.

FOURIER

Integer. Fourier transform. Set to 1 if TLOADi Bulk Data entries are referenced by the DLOAD set identification number in CASECC. Output by FRLG.

FREQDEP

Logical. Frequency-dependent element flag. Set to TRUE if frequency-dependent elements are present or to be processed. Output by TA1.

FREQINDX

Integer. Frequency or time step index. Selects frequency associated with UA.

FREQTYP

Character. Frequency dependent element processing mode: ’ESTF’

Compute frequency dependent stiffness

’ESTNF’

Compute nominal frequency dependent stiffness

FREQVAL

Real. Frequency value for frequency dependent element generation. Output by FRQDRV.

FREQWA

Real. Parameter for electromagnetic analysis.

FRQLOOP

Integer. Frequency loop counter. On input, FRQLOOP should be initialized to 0 before the loop. On output, FRQLOOP is incremented by one and at the last frequency, FRQLOOP is negated. For example, if the fifth frequency is the last then FRQLOOP is output as -5. Output by FRQDRV.

FSDCYC

Logical. Fully stressed design cycle flag. Set to TRUE if this is a fully stressed design cycle.

FSFLAG

Integer. Fluid/structure flag. Only applies to IRTYPEs 1 thru 7. 0

Structural modal contribution results from structural modes.

1

Fluid modal contribution results from structural modes.

11

Fluid modal contribution results from fluid modes.

GAMMA

Complex double precision. This is l, the scalar multiplier for [C].

GAMMAD

Complex double precision. This is the scalar multiplier for [C].

GEOMU

Integer. Fortran unit number to which the DBC module writes geometric information.

GETNUMPN

Logical. Panel static load computation flag. If TRUE then get number of panels flag only and do not compute panel static loads.

GMAFLG

Integer. Test control flag for changes in the set identification numbers specified for the SDAMPING, K2PP, M2PP, B2PP, and TFL commands.

GPF

Integer. Parameter for electromagnetic analysis.

GPFORCE

Integer. The number of columns in FENL. If GPFORCE less than or equal to zero then no GPFORCE or ESE command is present.

GRDPNT

Integer. Reference grid point identification number. Inertias are computed GRDPNT. If GRDPNT=-1 then the origin of the basic coordinate system is used. Output by VECPLOT.

GRIDFMP

Integer. Case Control set identification number of fluid grids that will be output.

GRIDMP

Integer. Case Control set identification number for a set of fluid grids.

GRIDSET

Integer. SET Case Control command identification number which contains a list grid point identification numbers.

GUSTAERO

Integer. QHJ computed only if GUSTAERO0, then IUNITSOL’th unit solution is being supplied.

IVALUE

Integer. Integer value to search for in a table.

JPLOT

Integer. Number of element plot sets. Set to -1 if there are none. Output by PLTSET and SEPLOT.

K6ROT

Real. Normal rotational stiffness factor for CQUAD4 and CTRIA3 elements.

KBAR

Real. Reduced frequency.

KDAMP

Integer. Viscous modal to structural damping flag. If set to -1, then viscous modal damping (SDAMPING Case Control command) will be included in the stiffness matrix as structural damping.

KDGEN

Integer. Differential stiffness matrix generation flag. Usually the column number in UG to use in differential stiffness matrix generation.

KEY

Character. Generic or NDDL name of a data block.

KFLAG

Integer. Stiffness update flag. Set to -1 to update stiffness before starting bisection. It reflects the NEWK and CONV status at the last converged solution or stiffness update. Output by NLITER.

KGTH

Integer. Set to -1 if all harmonic IDs (in analysis set) have been processed. Output by CYCLIC3.

KMATUP

Integer. Stiffness matrix update count within the increment. Output by NLITER.

KRATIO

Complex. Stiffness ratio to be used for time step adjustment. Output by NLTRD2.

KSTEP

Integer. Frequency of solve in complex eigenvalue analysis.

KSYM

Integer. Symmetric decomposition flag. Output by DCMP and DECOMP.

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Name

Type and Description

KTIME

Real. CPU time remaining. If KTIME is positive then KTIME is the time remaining at the start of the stiffness update. If negative, no stiffness update was done since the last exit from NLITER. KTIME still holds the negative of the stiffness update time from the last stiffness update. Output by NLITER, NLTRD, and NLTRD2.

LABL

Character. Label on the Fortran unit identified by IUNIT.

LANGLE

Integer. Large rotation calculation method: 1

Gimbal angle

2

Rotation vector

LASTBULK

Logical. Flag to indicate the current Bulk Data section is the last section in the input file. Output by XSORT.

LASTCC

Integer. Last auxiliary model Case Control section flag. Output by IFP1.

LASTCNMU

Real. Last converged value of the arc-length load factor. Output by NLITER.

LASTSE

Integer. Last superelement flag. Set to -1 if the current superelement is the last to process. Output by SEP2DR and SEDRDR.

LASTUPD

Integer. The time step number of the last stiffness update. Set to 0 if the stiffness update is performed due to the CGAP element during the iteration. Output by NLTRD and NLTRD2.

LCOLLBLi

Character. Label with up to 32 characters to be printed left-justified in upper left corner of each page.

LDSEQ

Integer. PG column number. On input, last column number of PG on previous SELA execution. On output, last column number of PG on current execution. Output by SELA.

LFREQ

Real. Lower frequency limit of modes to use in modal transformation.

LGDISP

Integer. Large displacement and follower force flag. -1

No large displacement and follower force effects will be considered.

1

Large displacement and follower force effects will be considered.

2

Only large displacement effects will be considered.

LINC

Integer. Number of load increments for this subcase.

LISET

Integer. Size of interference js-set extracted from the AEBGPTI table. Output by MTRXIN.

LJSET

Integer. Size of js-set extracted from the AEBGPTJ table. Output by MTRXIN.

LKSET

Integer. Size of ks-set extracted from the AEBGPTK table. Output by MTRXIN.

LMDYM

Integer. Power of 10 used to reduce the stiffness in a dynamic analysis.

LMFACT

Scale factor for the stiffness matrix of Lagrange rigid elements.

LMODES

Integer. The number of lowest modes to use in modal transformation. All outputs will have LMODES number of columns.

LMSTAT

Integer. Power of 10 used to reduce the stiffness in a static analysis.

LMTROWS

Integer. Number of Lagrange Multipliers appended to the A matrix. These rows are excluded from the internal reordering in the DCMP module.

LOAD

Integer. LOAD Case Control command set identification number specified in the fourth word of the NSKIP-th record of CASECC.

LOADFAC

Complex. Load factor. The real part is the load factor for the current iteration, having a fractional value between 0 and 1. Output by NLITER.

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Name

Type and Description

LOADFACR

Real. Load factor in nonlinear static analysis. (Same as LOADFAC except real).

LOADID

Integer. Load set identification number for the current subcase.

LOADIDP

Integer. Load set identification number for the previous subcase.

LOADU

Integer. Fortran unit number to which the DBC module writes static load information.

LPFLG

Integer. Flag to indicate whether there is another CASEA record to process. Set to -1 for the last subcase and Mach number. Output by AELOOP and DSARLP.

LPRINT

Logical. Print flag for divergence analysis (DIVERG), flutter analysis (FA1), and stability derivatives (SDP).

LSEQ

Integer. LOADSET Case Control command set identification number specified in the 205-th word of the NSKIP-th record of CASECC.

LST2REC

Integer. Last two records write flag. Set to TRUE to write last two records.

LSTEP

Integer. Load step. The current iteration step at the subcase level for static solutions.

LSTRN

Integer. Laminar strain flag. 0

Compute laminar stresses

1

Compute laminar strains

LUMPB

Real. Lumping factor for electromagnetic damping.

LUMPM

Real. Lumping factor for electromagnetic mass.

LUSET

Integer. The number of degrees-of-freedom in the g-set. Output by GP1 or PARAML.

LUSETD

Integer. The number of degrees-of-freedom in the p-set. Output by DPD.

LUSETS

Integer. The number of degrees-of-freedom in the g-set of the current superelement. Output by GP1.

MACH

Real. Mach number. Output by AELOOP and DSARLP.

MACH0

Real. Previously processed Mach number. Output by AMG.

MAJOR

Character. Name of the major degree-of-freedom set.

MATCH

Integer. Type of fluid/structural mesh matching. Output by GP5. 0

Matching mesh

1

Non-matching mesh

MATCPX

Integer. Complex material properties flag for electromagnetic elements.

MATNAMi

Character. Matrix name found on DMIG, DMIJ, DMIK, and DMIJI Bulk Data entries.

MAXBLK

Integer. Maximum block size.

MAXLP

Integer. Maximum limit allowed for element relaxation iteration and the material subincrement processes.

MAXR

Integer. Maximum physical record size.

MAXRAT

Real. Maximum value of factor diagonal ratio. Output by DECOMP.

MAXRATIO

Real. Minimum value of factor diagonal ratio which causes termination of decomposition.

MAXSET

Integer. Vector block size for Lanczos method only. The actual value of block size may be reduced depending on available memory and problem size.

MBCFLG

Logical. Multiple boundary condition in static analysis flag. Set to TRUE if multiple boundary conditions are specified in static analysis.

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Name

Type and Description

MCEIGCC

Logical. Modal complex eigenvalue analysis subcase flag. Set to TRUE if at least one ANALYSIS=MCEIG command was found in CASECC and CASECEIG is specified in the output list. Output by MDCASE.

MCFLAG

Integer. Modal contribution set usage flag.

MDTRKFLG

0

Grids and elements.

1

Grids only.

2

Elements only.

3

Acoustic/fluid points only.

Integer. Mode tracking status flag. 0

Mode tracking was successful

1

Mode tracking was unsuccessful

MEL

Integer. Maximum number of elements connected to a grid.

MESH

Character. Shading summary print flag. Set to ’YES’ to print summary; ’NO’ otherwise. Mesh type for aerodynamic or structural components: ’AERO’ or ’STRU’.

MESHSET

Integer. MSGMESH set processing flag. If nonzero, then combine mesh sets defined in the MSGMESH punch file.

METH

Character. Method of real eigenvalue extraction.

METHCMRS

Integer. Residual structure METHOD set identification (SID) override. METHCMRS>0 overrides SID value specified in CASES.

METRIK

Integer. Parameter for electromagnetic analysis.

MINDIAG

Real. Norm of the minimum diagonal term in U. Output by DCMP and DECOMP.

MFACT

Complex. Scale factor for hydroelastic boundary mass matrix. Output by BMG.

MFLG

Integer. Flag to indicate whether there is another Mach number to process in the current subcase. Set to 0 for the last Mach number in the subcase. Output by AELOOP.

MFRQCC

Logical. Modal frequency response analysis subcase flag. Set to TRUE if at least one ANALYSIS=MFREQ command was found in CASECC and CASEFREQ is specified in the output list. Output by MDCASE.

MODE

Character. Boundary condition change ignore flag. ’NONLINEAR’ Ignore boundary condition changes ’STATICS’ Do not ignore boundary condition changes

MODECC

Logical. Normal modes analysis subcase flag. Set to TRUE if at least one ANALYSIS=MODES command was found in CASECC and CASEMODE is specified in the output list. Output by MDCASE.

MODEPT

Logical. Analysis model element property modification flag. Set to TRUE indicates that the design model is overriding element properties in the analysis model. Output by DOPR1.

MODETRAK

Integer. Mode tracking request flag. 0

Mode tracking was not requested

>0

Mode tracking is requested

MODGEOM2

Logical. Analysis model connectivity modification flag. Set to TRUE indicates that the design model is overriding connectivity in the analysis model. Output by DOPR1.

MODGM4

Logical. GEOM4P update flag. Set to TRUE if GEOM4M is updated. Output by MODGM4.

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Name

Type and Description

MODMPT

Logical. Analysis model material property modification flag. Set to TRUE indicates that the design model is overriding material properties in the analysis model. Output by DOPR1.

MONRPLC

Logical. If TRUE then components with duplicate names will be copied from MON1 into MON.

MPC

Integer. MPC Case Control command set identification number specified in the second word of the NSKIP-th record of CASECC.

MPCF2

Integer. Multipoint constraint set identification number change flag. Set to 1 if the current subcase contains a different multipoint constraint set from the previous subcase. Set to -1 otherwise or if there are no multipoint constraints in the current subcase. Output by GP4.

MPCFLG

Integer. Controls whether the grid point connectivity created by multipoint constraint Bulk Data entries (MPC, MPCADD, and MPCAX and the rigid element entries; e.g., RBAR) is considered during resequencing.

MPCMETH

Character. Multipoint constraint processing method. Also indicates the type of matrix in the second input position: ’RG’ for RMG and ’KMM’ for KMM.

MPFSORT

Integer. Sort flag. A value in the first table is added to a value in the second table.

MPNFLG

Integer. Set to 1 if multiple panels exist. Output by GP5.

MSCHG

Integer. Boundary condition change flag in. In nonlinear static analysis only. Output by CASE.

MSGINP1

Integer. Optional integer input.

MSGINP2

Integer. Optional integer input.

MSGLVL

Integer. The level of diagnostic output for the Lanczos method only. 0

No output

1

Warning and fatal messages

2

Summary output

3

Detailed output on cost and convergence

4

More detailed output on orthogonalizations and some extra arithmetic to check on orthogonality

Integer. Diagnostic output flag in the SEQP module. 0

No

1

Yes

Integer. Diagnostic output flag in the SOLVIT module. 0

Minimal; i.e, UIM 6447

1

UIM 6447, convergence ratios, and residual norms

Integer. Diagnostic output flag in the TABEDIT module. MSGNUM

Integer. Message number.

MSGOUT

Integer. Optional integer output. Output by MSGHAN.

MTRNCC

Logical. Modal transient response analysis subcase flag. Set to TRUE if at least one ANALYSIS=MTRAN command was found in CASECC and CASEMTRN is specified in the output list. Output by MDCASE.

MU

Real. The magnitude of the last g-set displacement matrix. Output by NLTRD.

NAME

Character. Name of a data block. Output by PARAML.

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Name

Type and Description

NAME1

Character. If NAME1 is specified, read the DMI matrix associated with NAME1 instead of the output data block DMI1.

NAME2

Character. If NAME2 is specified, read the DMI matrix associated with NAME2 instead of the output data block DMI2.

NASOUT

Logical. Print flag for fluid/structural mesh matching summary.

NBCONT

Integer. Number of bisections due to slideline contact. Output by NLITER and NLTRD2.

NBIS

Integer. Current bisection counter. Output by NLITER and NLTRD2.

NBLOCK

Integer. Number of spill blocks to form if “out of memory” algorithm is used.

NBRCHG

Integer. Number of negative terms on the diagonal. Output by DCMP and DECOMP.

NBSORT2

Integer. Contact region output sort format flag. Output by BGCASO. 1

If SORT2 format is requested for printing

2

If x-y plotting is requested

NCNOFFST

Integer. Counter for retained constraints. The value is initialized to 1 in and is incremented by the number of records in CNTABR. Output by DSAD.

NCOL

Integer. Number of columns (i.e.; subcases, modes, time steps or frequencies) desired in the output matrices. By default, all data records will be converted into the output matrices. If NCOL is less than the number of data records in the input table, then the first NCOL records are converted and the remaining records are ignored. Output by TRD1 and TRD2. Integer. Number of columns. Output by NORM.

NCUL

Integer. Number of columns desired in the solution matrix for the residual structure. Usually determined by the PARAML module.

ND

Integer. The number of desired eigenvalues.

ND1

Integer. The number of desired eigenvalues in first complex region.

NDAMP

Real. Numerical damping.

NDDLNAMi

Character. NDDL name of the DBi-th data block.

NDES

Integer. The number of desired eigenvalues. If the last mode is repeated, then nDes + m (where m is the multiplicity of the last mode) solutions are found.

NDJ

Integer. The number of desired eigenvalues in j-th complex region. for pre-Version 70.5 Lanczos method.

NDVTOT

Integer. Number of unique referenced design variables.

NE

Integer. Number of estimated eigenvalues. Integer. The number of estimated eigenvalues for non-Lanczos methods only. For the Lanczos method, NE is the problem size which the QL Householder method is used.

NEIG

Integer. Number of eigenvalues to keep. 0

Keep all eigenvalues

>0

Keep first NEIG-th eigenvalues

NEIGV

Integer. The number of eigenvectors found. Set to -1 if none were found. Output by CEAD, READ, LANCZOS, and UEIGL.

NEWCASE

Integer. CASECCBO output flag. Set to 1 if CASSECBO is generated. Output by BGCASO.

NEWK

Integer. Stiffness update flag. Output by NLITER, NLTRD, and NLTRD2.

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Do not update stiffness.

1

Update stiffness.

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Name

Type and Description 2

Update stiffness, the solution is diverging and MAXBIS has been reached.

NEWNAMi

Character. The generic name of the corresponding input table; e.g., NEWNAM3 corresponds to NEWDB3, etc.

NEWP

Integer. New subcase flag. Output by NLITER, NLTRD, NLTRD2, and TOLAPP. -1

Current subcase has not been completed.

1

Current subcase has been completed.

NEXTID

Integer. Identification number which appears on the BEGIN BULK command of the next Bulk Data section; usually superelement or auxiliary model identification number. Output by XSORT.

NFEXIT

Logical. Termination flag. If FALSE do not issue User Fatal Message 2070 and do not terminate the module if the matrix is not found.

NFREQ

Integer. Number of frequencies for frequency response analysis. Output by CYCLIC1.

NGERR

Integer. Error flag. If errors are encountered, then NGERR is set to -1; otherwise +1. Output by GPSP.

NGP

Integer. Number of grid points and scalar points in the structure. Output by PLTSET and SEPLOT.

NHBDY

Integer. Number of CHBDYi elements. Set to -1 if none exist. Output by PLTHBDY.

Ni

Character. Continuation entry prefix.

NINPTPS

Integer. Approximate number of surrounding independent element interpolation points to be considered when interpolating at a grid point for a given material coordinate system.

NJ

Integer. Number of degrees-of-freedom in j-set degrees-of-freedom. Output by APD.

NK

Integer. Number of degrees-of-freedom in k-set degrees-of-freedom. Output by APD.

NKEYS

Integer. Duplicate value sort option specification.

NLAM

Integer. Number modes to create in LAMAX.

NLAYERS

Integer. Number of layers to integrate through the thickness of CQUAD4 and CTRIA3 elements in nonlinear analysis.

NLFLAG

Integer. Output by NLITER.

NLOADS

Integer. The number of subcase records contiguous with respect to the MPC and SPC command in the first subcase of the current boundary condition.

NLSTRAIN

Logical. Nonlinear strain data recovery, otherwise flag at word 11 of OES1 takes precedence. Set to TRUE if nonlinear strains are to be processed.

NLTYPE

Integer. Nonlinear analysis type. 0

Statics

1

Transient response

NMAT

Integer. Number of matrices.

NMK

Integer. Number of Mach number and reduced frequency pairs. Output by GETMKL.

NNDFRQ

Integer. Number of forcing frequencies which depend upon natural frequencies.

NOA

Integer. Constraint and omit set flag. Set to -1 if NOMSET=-1, NOSSET=-1, and NOOSET=-1; otherwise the number of degrees-of-freedom in the a-set. Output by GP4 and GPSP.

NOABFL

Integer. Matrix ABFL existence flag; 0 if ABFL exists and -1 otherwise. Output by BMG.

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Name

Type and Description

NOASM

Integer. Matrix assembly flag. Set to -1 if no matrix assembly and reduction is requested for the current superelement based on the SEKR or SEALL Case Control commands. Output by SEP2DR and SEP3.

NOB2

Integer. B2GG or B2PP generation flag. Set to +1 if B2GG or B2PP is generated; -1 otherwise. Output by MTRXIN.

NOBGG

Integer. Same as NOKGG except for BELM and BDICT. Output by EMG.

NOBKGG

Integer. Slideline contact stiffness generation flag. Set to 1 to generate slideline contact stiffness.

NOBSET0

Integer. Number of null columns in PHZ in front of non-null columns. Output by DYNREDU.

NOCEAD

Integer. Complex eigenvalue analysis flag. Set to 1 if complex eigenvalue analysis needs to be performed, otherwise, set to -1. Output by FA1.

NOCHAR

Integer. Number of character value inputs.

NOCMPX

Integer. Number of complex value inputs.

NOCOMP

Integer. Composite stress/strain flag. -5

Forces of composites in STRAIN=sid

-2

Forces of composites in STRESS=sid

-1

Stresses for all elements (same as 0 except in DMAP)

0

Stresses for all elements

1

Stresses for non-composites only

2

Strain/curvature and forces of composites in STRESS=sid

3

Strains for all elements and MPCForces

4

Strains for non-composites only

5

Strain/curvature of composites in STRAIN=sid

NODLT

Integer. Set to 1 if dynamics loads Bulk Data entries are processed, -1 otherwise. 1 also means DLT is created. Output by DPD.

NODR

Integer. Data recovery request flag. Set to -1 if there is no data recovery requested for any superelement. Output by SEDRDR and SEP4.

NOEDS1

Integer. OEDS1 generation flag. Set to 0 if OEDS1 is generated. Output by STDCON.

NOEED

Integer. Set to 1 if eigenvalue extraction Bulk Data entries are processed, -1 otherwise. 1 also means EED is created. Output by DPD.

NOEGPSF

Integer. EGPSF creation flag. Set to zero if EGPSF is created.

NOEGPSTR

Integer. EGPSTR creation flag. Set to 0 if EGPSTR is created. Output by GPSTR2.

NOELDCT

Integer. ELDCT generation flag. Set to 0 if ELDCT is generated. Output by STDCON.

NOEST

Integer. Processing status flag. Output by MATMOD option 38.

NOESTL

Integer. ESTL generation output flag. Set to 1 if ESTL is generated; -1 otherwise. Output by TA1.

NOFORT

Integer. OUTPUT4 flag. Set to 0 if FORT is requested on the legacy SENSITY Case Control command. Output by DSTA.

NOFREQ

Integer. Number of excitation frequencies.

NOFRL

Integer. FRL generation flag. Set to -1 if FRL is not generated. Output by FRLGEN.

NOGDS1

Integer. OGDS1 generation flag. Set to 0 if OGDS1 is generated. Output by STDCON.

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Name

Type and Description

NOGEOM1

Integer. Processing status flag. Output by MATMOD option 36.

NOGEOM2

Integer. Processing status flag. Output by MATMOD option 37.

NOGEOM3

Integer. GEOM3N creation flag. Set to 1 if GEOM3N is created, otherwise set to -1. Output by CYCLIC1.

NOGENL

Integer. The number of general elements. Set to -1 if there are no general elements.

NOGOIFP

Logical. IFP module error return flag. Set to TRUE if an error was detected. Output by IFP.

NOGOIFPi

Logical. IFPi module error return flag. Set to TRUE if an error was detected. Output by IFPi.

NOGOMEPT

Logical. MODEPT module error return flag. Set to TRUE if an error was detected. Output by MODEPT.

NOGOMGM2

Logical. MODGM2 module error return flag. Set to TRUE if an error is found. Output by MODGM2.

NOGONL

Integer. Nonlinear "no-go" flag. Set to +1 to continue or -1 to terminate. Output by NLTRD2.

NOGOXSRT

Logical. XSORT module error return flag. Set to TRUE if an error was detected. Output by XSORT.

NOGPDCT

Integer. GPDCT generation flag. Set to 0 if GPDCT is generated. Output by STDCON.

NOGRAV

Integer. Gravity load existence flag. Set to -1 if no GRAV Bulk Data entry images, +1 otherwise. Output by GP3.

NOGUST

Integer. Gust load flag. Set to -1 if no gust loads exist; otherwise set to 1. Output by GUST.

NOINT

Integer. Number of integer value inputs for PRGNAME.

NOK2

Integer. K2GG or K2PP generation flag. Set to +1 if K2GG or K2PP is generated; -1 otherwise. Output by MTRXIN.

NOK4GG

Integer. Differential stiffness or structural damping generation flag. Output by EMG. On input: ≥3

Compute geometric nonlinear effects

0, then matrix exists.

NOUNIT

Integer. Number of Fortran input units.

NOUP

Integer. Upstream superelement flag. Set to -1 if there are no superelements connected upstream from the current superelement. Output by SEP2DR and SEDR.

NOXGG

Integer. XGG existence flag. Set to -1 if XGG does not exist. Output by MATREDU.

NOXOUT

Integer. SDRX update flag. Output by SDRX and SDRXD. 0

OEF1X and OES1X are updated

-1

OEF1X and OES1X are not updated

NOXPLZER

Integer. Explicit zero existence flag. Set to -1 if no explicit zeros are found. Output by MATMOD option 39.

NOXPP

Integer. XPP existence flag. Set to -1 if XPP does not exist. Output by MATREDU.

NOXYPLOT

Integer. X-Y plot request flag. Set to -1 if no x-y plot requests are specified for the current superelement. Output by SEDR and XYTRAN.

NOYSET

Integer. Number of generalized degrees-of-freedom with non-null columns in PHZ.

NOZSET

Integer. Number of generalized degrees-of-freedom. Also number of columns in PHZ.

NQMAX

Integer. Maximum number of auto-q-set’s allowed per partitioned superelement. See NQSET.

NQSET

Integer. Number of automatic q-set degrees-of-freedom (auto-q-set). Each superelement will have NQSET number of q-set degrees-of-freedom.

NR1OFFST

Integer. Counter for retained type 1 responses. The value is initialized to 1 and is incremented by the number of records in R1TABR. Output by DSAD.

NR2OFFST

Integer. Counter for retained type 2 responses. The value is initialized to 1 and is incremented by the number of records in RSP12R. Output by DSAD.

NR3OFFST

Integer. Counter for retained type 3 responses. The value is initialized to 1 and is incremented by the number of records in RESP3R. Output by DSAD.

NROW

Integer. Number of rows. Output by NORM.

NSEG

Integer. Number of cyclic segments as specified on CYSYM Bulk Data entry. Output by CYCLIC1.

NSENQSET

Integer. Number of SENQSET degrees-of-freedom allocated to the current superelement.

NSKIP

Integer. Record number in CASECC with special meanings in the following applications. Output by GP4, CASE, and BCDR. GP4, BCDR, and SDR1: The first subcase of the current boundary condition.

CASE

The first subcase of the current boundary condition (nonlinear statics only) or current FREQ, K2PP, M2PP, B2PP, TFL, or SDAMP condition (frequency response or complex eigenvalue analysis).

AELOOP

Trim subcase counter.

DSARLP

Trim subcase counter.

FRRD1 and SOLVIT

Record number of current subcase in CASECC and used only if the SMETHOD command selects the ITER Bulk Data entry which specifies values for the desired iteration parameters. If NSKIP=-1 then CASECC is not required and the values are taken from the module specification of the values.

GETCOL

Subcase record number to read in CASEBUCK for the STATSUB subcase identification number.

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Name

Glossaries

Type and Description GNFM

Loop counter in old geometric nonlinear analysis.

READ and LANCZOS

Subcase record number to read in CASECC for the METHOD set identification number.

LCGEN

Subcase record number to read in CASECC for the LOADSET set identification number.

NLCOMB, PCOMB, and SDRNL

Subcase record number to read in CASECC.

NLITER and TOLAPP

On input: Subcase record number to read in CASECC. On output: Set to -2 if run is to be terminated.

NSOUT

Integer. Number of time steps to output. By default all time steps are output.

NSTEP

Integer. Current time step position for subcase, set to 0 at the beginning of the subcase. Output by NLTRD and NLTRD2.

NSWELM

Integer. Current spot weld element ID. Output by MODGM2 and MODGM4.

NSWPPT

Integer. Current spot weld projection point ID.

NTIPS

Integer. The number of domains (tip superelements to be created automatically when ACMS=’YES’. If NTIPS=0, then the number of domains will be set equal to the number of processors. Output by SEQP.

NULLMAT

Integer. Null matrix flag. Set to -1 if MAT is null.

NULLROW

Integer. Flag to insert null rows in the output matrices for nonlinear quantities. 0

Insert null rows, which is compatible with DRMS1 output format

1

Do not insert null rows, which is required for DRMH3 processing

NUMHDOF

Integer. The number of modes.

NUMOUT

Integer. Output element quantity flag. >0

Number of element quantities per element type to be output

0

Output all quantities for elements in a group if the absolute value of one or more elements is greater than BIGER.

-1

Output sorted quantities with absolute value greater than BIGER.

-2

Output filtered quantities with absolute value greater than BIGER.

NUMPAN

Integer. Number of panels. Output by GP5.

NVEC

Integer. Number of solution results to process.

NVECT

Integer. Number of columns in CVECT and PG1. Output by PCOMB.

NX

Integer. Number of extra aerodynamic degrees-of-freedom. Output by ADG.

OADPMAX

Integer. Total number of adaptivity cycles performed.

OBJIN

Real. Initial objective value.

OBJOUT

Real. Final objective value. Output by DOM9.

OBJSID

Integer. Superelement identification number associated with DESOBJ. Set to -1 for all cases unless the user specifies the DESOBJ command in a particular superelement subcase. Output by MDCASE.

OBJVAL

Real. Objective value. Output by DSAD.

ODESMAX

Integer. Total number of design cycles performed.

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Name

Type and Description

OG

Integer. CURV module’s grid point processing flag. If set to 0, then grid point stresses or strains are computed.

OLDDT

Real. Time step increment used in the previous iteration or time step to be used after the matrix update or subcase switch. Output by NLTRD and NLTRD2.

OLDNAMi

Character. The generic name of the corresponding output; e.g., OLDNAM3 corresponds to OLDDB3, etc.

OMEGAJ

Real. Imaginary part of shift point Aj for pre-Version 70.5 Lanczos method.

OMID

Character. Material output coordinate system flag. If OMID=’YES’ then stresses, strains, and forces are output in the material coordinate system of CQUAD4, CTRIA3, CQUAD8, and CTRIA6 elements.

OPERATN

Character. FORTIO operation.

OPT

’EXISTS’

Check for assigned physical file existence

’OPEN’

Open file

’CLOSE’

Close file

Character. DIAGONAL module processing option. ’COLUMN’

Extract diagonal to a column matrix and raise all elements to POWER

’SQUARE’

Extract diagonal to a square matrix and raise all elements to POWER

’WHOLE’

Raise all elements to POWER

OPTi

Integer. Print control parameters in the TABPRT module.

OPTEXIT

Integer. Design optimization termination option. See the “OPTEXIT” in the NX Nastran Quick Reference Guide .

OPTFLG

Integer. DSVG1P application method:

OPTION

1

Statics

2

Normal modes

3

Ncceleration load

Character. Response summation method for scaled response spectra analysis. Possible values are: ’ABS’

Absolute

SRSS’

Square root of the sum of the squares

’NRL’

Naval Research Laboratory (new)

’NRLO’

Naval Research Laboratory (old)

OSTEP

Integer. Restart step number.

OSWELM

Integer. Offset for spot weld element IDs.

OSWPPT

Integer. Offset for spot weld projection point IDs.

OUTFMP

Integer. Number of fluid modes to output.

OUTOPT

Integer. CURV module’s output option.

OUTSMP

Integer. Number of structure modes to output.

OVRWRT

Character. DBC database overwrite flag.

P2,P3

Integer. Used to define boundary condition of the surface spline.

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Name

Glossaries

Type and Description

P4

0,0

Surface spline is unconstrained at the edges.

-1,0

A zero moment X-directional end condition is imposed on the surface spline.

0,-1

A zero moment Y-directional end condition is imposed on the surface spline.

Integer. Coordinate pair selection. 1

XY point pairs are used for the surface spline fit.

2

XZ point pairs are used for the surface spline fit.

3

YZ point pairs are used for the surface spline fit.

P5

Real. Used to stiffen springs applied during the surface spline generation.

PANAME

Character. The name of the panel whose coupling matrix is created. Output by ACMG.

PANELMP

Integer. Flag to compute panel participation factors.

PARM

Integer. Equivalence flag on the EQUIVX module. Purge flag on the PURGEX module.

PARMi

Logical. Output data block presence flag. Output by DMIIN and DTIIN.

PARTSE

Logical. Partitioned superelement flag. Set to TRUE if the current superelement is a partitioned superelement. Output by SEP2DR.

PATH

Character. Direction of cyclic transformation: ’FORE’

Forward (analysis)

’BACK’

Backward (data recovery)

PBCONT

Integer. Slideline contact flag.

PDEPDO

Integer. Skip factor flag. See NOi on TSTEP Bulk Data entry. Output by TRLG. 0

Skip factor is >1.

-1

Skip factor is 1.

PEID

Integer. Primary superelement identification number. Output by SEP2DR and SEDRDR.

PENFAC

Real. Penalty factor for electromagnetic elements.

PEXIST

Logical. Set to TRUE if p-elements are present.

Pi

Character. Generic name of the data block DBi to be processed by the DBC module. Integer. Inputs to the MATGEN, MATMOD, and PARAML module. Any type. Inputs to MESSAGE module.

PLSIZE

Integer. Size of the load matrix. Compared to the size of load matrix in the previous subcase in order to detect boundary condition changes in the current subcase. Boundary condition changes are not allowed in the arc-length method. Output by NLITER.

PLTCNT

Integer. SEPLOT (or SEUPPLOT) command counter. Output by SEPLOT. On input: 0

Initialization

On output: >0

Current SEPLOT (or SEUPPLOT) command

PLTNUM

Output. Plot frame counter. Output by PLOT, MSGSTRES, and XYTRAN.

PNLPTV

Logical. Panel participation/partition vector flag. If TRUE, then generate a partitioning vector APART which may be used to partition the g-set size coupling matrix to obtain the panel’s coupling matrix.

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Name

Type and Description

PNQALNAM

Character. Name of qualifier for panels.

POSTU

Integer. Fortran unit number to which the DBC module writes data recovery information.

POUTF

Integer. Intermediate output flag. Set to -1 if intermediate output is not requested. Output by NLITER and TOLAPP.

POWER

Integer. Power of 10 to be multiplied by DET in DCMP and DECOMP. Exponent to which the real part of each element in A is raised in the DIAGONAL module.

PREC

Integer. Precision of output matrix. 0

Machine-precision

1

Single

2

Double

PRECOL

Integer. Subcase record number in CASESTAT referenced by the STATSUB(PRELOAD) subcase identification number. PRECOL also corresponds to the column number of static solution vector. Output by GETCOL.

PREFDB

Real. Peak pressure reference for pressure level in units of dB or dBA.

PREFONLY

Integer. Preface execution only flag in SOLVIT module.

PRESENS3

Logical parameter that is TRUE when one or more of FREQ3, FREQ4, or FREQ5 types of bulk data exist.

PRESORT

Integer. Pre-sort flag. Set to -1 if column is already sorted. Output by MATMOD option 35.

PRGNAME

Character. Name of external program called by ISHELL module.

PRGPST

Character. Singularity summary print flag. If set to ’YES’, then the summary is printed.

PRNTOPT

Character. MATGPR module print options.

PRJVEROP

Character. Operation name.

PROGRAM

’GET’

Get current project and version

’NEXT’

Get next non-deleted project and version

’SET’

Set current project and version

’LAST’

Get the last (bottom) project and version

’RESTART’

Get restart project and version

Character. DBC database format flag. ’XL’

MSC.Patran

’GRASP’

NX Nastran Access

PROJ

Integer. Project number. Output by PROJVER.

PROPOPT

Integer. Property optimization flag. Set to 1 if element properties are defined as design variables. Output by DSABO.

PROPTN

Integer. In order to support a pre-Version 68 capability, if PROPTN=-1 then an EPT data block which is based on the values and the property to design variable relations will be produced.

PROTYP

Integer. Designed property type code. Output by DOPR1. 1

DVPRELi entries exist

2

DVCRELi entries exist

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Name

Glossaries

Type and Description 4

DVMRELi entries exist

>0

For combinations add above values

PROUT

Integer. Print control for the ELTPRT module.

PRTSWM

Logical. UWM 6991 print control flag in NORM module.

PRTUIM

Logical. UIM 4570 print control flag in SELA module.

PSEQOPT

Character. P-element append flag. Specifies append (default) or insert option for p-elements in the SEQP module.

PVALNEW

Integer. New p-value set identification number. Output by ADAPT.

Q

Real. Dynamic pressure. Output by AELOOP and DSARLP.

QUALNAM

Character. Name of qualifier to be varied when selecting MAPS from MAPS* in SEMA, SELA, and SEDR modules. Character. Keyword which appears on the BEGIN BULK command of the next Bulk Data section; usually AUXMODEL or SEID. Output by XSORT.

QUALNAMP

Character. Name of qualifier to be used in selecting PUG.

QUALVAL

Integer. QUALNAM value assigned to the Main Bulk Data section.

R1CNT

Integer. Counter for type 1 responses in data block R1TAB. Output by DOPR3.

R2CNT

Integer. Counter for type 2 responses in data block RESP12. Output by DOPR3.

R3CNT

Integer. Counter for type 3 responses in the RESP3 table. Output by DOPR3.

RBFAIL

Logical. Set to TRUE if grounding check does not pass strain energy threshold used by IOPT=10. Output by VEPCLOT.

RCOLLBLi

Character. If RCOLLBLi is blank then ’COLUMN’ will be printed. Label with up to 32 characters to be printed right-justified in upper right corner of each page. RCOLLBLi is then followed by column number.

REACT

Integer. For zero-th and first harmonic, set to -1 if no support degrees-of-freedom; +1 if support degrees-of-freedom exist. For harmonics greater than 1 REACT is always -1. Output by CYCLIC3.

REAL

Real. Real part of matrix or table element. Output by PARAML.

REALD

Real double precision. Real value in the next record.

REALi

Real. Real value for PRGNAME.

RECNUM

Integer. Record number of table element. Output by PARAML.

REFC

Real. Output by PARAML of AERO data block.

REPEAT

Integer. Last boundary condition flag. Set to -1 at the last boundary condition; +1 otherwise. Output by GP4.

RESFLG

Integer. Residual vector eigenvalue subheading print flag to be used by the OFP module.

RESPi

Character. Response type.

RESTYP

Integer. Optimization results flag.

RGSENS

Logical. Rigid element sensitivity flag. Output by DOPR5 or DSVGP4.

ROWNAM

Character. Degree-of-freedom set name for labeling matrix rows in MATGPR output.

RSEID

Integer. Repeated superelement identification number as specified on the SEBULK Bulk Data entry. Output by SEP2DR and SEDRDR.

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Name

Type and Description

RSFLAG

Logical. Main Bulk Data superelement presence flag. Set to TRUE if superelements are defined in the main Bulk Data section. Output by SEP1X.

RSTEP

Integer. Controlled increments counter. Output by NLITER.

RUNIFPi

Logical. IFPi module execution flag. Set to TRUE if IFPi module execution is required. Output by IFP.

RUNMEPT

Logical. MODEPT module execution flag. Set to TRUE if MODEPT module execution is required. Output by IFP.

SAERCC

Logical. Aerostatic analysis subcase flag. Set to TRUE if at least one ANALYSIS=SAERO command was found in CASECC and CASESAER is specified in the output list. Output by MDCASE.

SCNDRY

Integer. Secondary (identical or mirror) superelement flag. Set to -1 if superelement is defined by the CSUPER Bulk Data entry with PEID>0. Output by SEP2DR and SEDRDR.

SDFLG

Integer. Flag to indicate whether the current subcase has active stability derivative response (STABDER on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response. Output by DSARLP.

SDRDENS

Integer. Sparse data recovery ceiling density. If the density of PVGRID is greater than SDRDENS divided by 100, then choose full data recovery.

SDRMETH

Integer. Data recovery method flag. Output by OUTPRT.

SDROVR

Character. Override for data recovery method flag.

SDRPOPT

Character. Principal stress/strain computation selection: ’SDRP’

Compute in SDRP

’OFP’

Compute in OFP

SEBULK

Logical. Partitioned superelement presence flag. Set to TRUE if partitioned superelements are present or BEGIN SUPER is specified for the first BEGIN BULK Case Control command.

SEDRCNTL

Character. Processing list selection. ’’

All superelements will be processed (default).

’CURR’

Only the superelement specified by SEID parameter will be processed.

SEDWN

Integer. Downstream superelement identification number. Output by SEP2DR and SEDRDR.

SEFLAG

Logical. Set to TRUE if partitioned superelements are present. Output by SEPR1.

SEID

Integer. Superelement identification number. On output from SEP3 and SEP4, SEID is an initialization flag; i.e., if there are superelements, then SEID is set to -1 to initialize SEP2DR and SEDRDR; otherwise 0. Output by SEP2DR, SEDRDR, SEP3, and SEP4.

SEP1XOVR

Integer. Over-ride bits for module processing. Bit(s)

Value(s)

Description

1-3

1-5

Override Search Algorithm Selection.

4

8

Disable Automatic Main Bulk Scalar

5

16

Print RSSCON old/new locations.

6

32

Print Boundary Search Sequence.

7

64

SEP1X "Diag 30" Debugging Output.

8

128

Auto-SET in Residual place in OSET when other sets present in the Residual.

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Name

Type and Description

SEP2CNTL

Character. Processing selection.

SEP4CNTL

’ALL’

All superelements will be processed

’PSLGDV’

Only superelements specified on the SEDV Case Control commands

’DSLIST’

Only superelements specified on the SERESP Case Control commands

’SLIST’

Only superelements specified on the SEALL, SEMG, SEKR, SELG, SELR, or SEMR Case Control commands.

’SEDWN’

All superelements that have SEDWN as their downstream superelement.

’CURR’

Only the superelement specified by SEID parameter will be processed.

Integer. Processing list selection. ’ALL’

All superelements will be processed

’ALL’

Only superelements specified on SEDR Case Control command

SEPRTN

Logical. SUPER command processing flag. Set to TRUE to ignore SUPER command.

SEQMETH

Integer. Resequencing method.

SEQOUT

Integer. SEQP module output options.

SETi

Character. Degree-of-freedom set name.

SETKNTR

Integer. Pointer to desired member in set; e.g., 1 means first member in set, 2 means second member, etc. If the set is exhausted then SETKNTR is reset to -1. Output by PARAML SET option.

SETNAM

Character. Degree-of-freedom set name used by IOPT=9 and 10.

SETNAME

Character. Degree-of-freedom set name. SOLVIT, DCMP, READ: For maximum efficiency, the rows and columns of the input matrices must correspond to or be a partition of the degree-of-freedom specified by SETNAME. SEQP

SETYPE

Specifies size of MAT in SEQP module.

Character. Superelement type as specified on the SEBULK Bulk Data entry. Output by SEP2DR and SEDRDR. ’REPEAT’

Repeated

’MIRROR’

Mirror

’COLLTR’

Collector

’EXTRNA’

External

’PRIMARY’

Primary

SHAPEOPT

Integer. Shape optimization flag. Set to 1 if shape optimization is activated. Output by DSAM.

SHAPES

Logical. Shape optimization Bulk Data entry presence flag. Must be TRUE if DVGRID, DVSHAP, or DVBSHAP Bulk Data entries are present.

SHFSCL

Real. Estimate of the first flexible natural frequency. SHFSCL must be greater than 0.0.

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Name

Type and Description

SID

Integer. Alternate set identification number. If SID=0, the set identification number is obtained from the METHOD command in CASECC and used to select the EIGR, EIGB, or EIGRL entries in DYNAMIC. Similarly for CMETHOD and EIGC. If SID>0, then METHOD command is ignored and the EIGR, EIGB, or EIGRL is selected by this parameter value. All subsequent parameter values (METH, F1, etc.) are ignored. Similarly for CMETHOD and EIGC for Lanczos method only. If SID0, then singularities identified by this module are written to the PUNCH file as SPC Bulk Data entries.

SPSELREC

Output. Last record number processed in SPSEL. Set to -1 when processing last record. Output by RSPEC.

SRCOMP

Character. Flag to request output table of ply strength ratios (OESRT).

SRCOMPS

Character. Requests output of failure indices for composite solid elements. If SRCOMPS=‘YES”, requests output of strength ratios for composite solid elements.

SRTELTYP

Integer. Element type to be filtered and sorted. By default, all element types will be filtered and sorted.

SRTOPT

Integer. Filter/sort option based on NUMOUT and BIGER. 0

Maximum magnitude

1

Pinimum magnitude

2

Maximum algebraic

3

Minimum algebraic

SRTTYP

Integer. Item code 1 sort flag. Set to 1 to perform an integer sort on item code 1 which is usually an integer quantity.

START

Integer. Number of the grid points at the beginning of the input sequence in the SEQP module.

STARTCOL

Integer. Starting column number to extract from I1.

STATCC

Logical. Static analysis subcase flag. Set to TRUE if at least one ANALYSIS=STATICS command was found in CASECC and CASESTAT is specified in the output list. Output by MDCASE.

STATIC

Integer. Static analysis flag. Set to zero for static analysis and one for dynamic analysis.

STATOPT

Character. Static solution method.

STATSUB

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’DRCT’

Direct

’ITER’

Iterative.

Integer. STATSUB Case Control command set identification number specified in the 256-th word of the NSKIP-th record of CASECC.

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Glossaries

Name

Type and Description

STFLG

Integer. Flag to indicate whether the current subcase has active static response (DISP, STRAIN,STRESS, FORCE, CSTRAIN, CSTRESS, or CFORCE on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response. Output by DSARLP.

STIME

Real. On initial input, starting time step and on output, accumulated time used for restarts. Output by NLTRD and NLTRD2.

STPSCL

Real. Shape step size scaling factor.

STRUCTMP

Integer. Number of structure modes to use computing factors.

SUPAERO

Character. Method for supersonic aero; ’ZONA’ or ’CPM’.

SUPER

Integer. Selects coupled or uncoupled sequencing or special handling of multipoint constraints in the SEQP module.

SUPORT

Integer. SUPORT Case Control command set identification number specified in the 255-th word of the NSKIP-th record of CASECC.

SWEXIST

Logical. Spot weld element existence flag. Set to TRUE if spot weld elements exist. Output by MODGM2.

SYM

Integer. Symmetric partition or merge flag. 0

Symmetric; i.e., CP is used for RP

0

Asymmetric; i.e., CP and RP are distinct

SYMFLG

Complex. Scale factor.

SYMXY

Integer. Aerodynamic x-y symmetry flag. Output by AEMODEL.

SYMXZ

Integer. Aerodynamic z-y symmetry flag. Output by AEMODEL.

SYS66

Integer. System cell 66 override for matrix multiply.

T

Integer. Transpose flag for first matrix input to MPYAD. 1

Transpose

0

Do not transpose

TABID

Integer. TABLED1 punch flag. If IDTAB is greater than zero, all requests for XYPUNCH will produce TABLED1 Bulk Data entries for the curve. The table identification number will start at TABID and increase by one for each table punched. Output by XYTRAN.

TABS

Real. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius or 459.69 in Fahrenheit.

TEMPSID

Integer. Temperature set identification number. Usually obtained from the TEMPERATURE Case Control command. Required for use in stress recovery of differential stiffness.

TESTNEG

Integer. Load increment method flag in nonlinear static analysis. Output by CASE.

TFLG

Integer. Flag to indicate whether the current subcase has active trim responses (TRIM on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response. Output by DSARLP.

TFLID

Integer. Transfer function set identification number. TFLID is ignored if IOPT=3, 4, 5, 13, 14, or 15.

THRESH

Integer. Exponent of 10 which defines the pivoting threshold for unsymmetric decomposition.

Ti

Integer. Transpose flag for first four matrices input to SMPYAD.

TINY

1

Transpose

0

Do not transpose

Real. Small element strain energy value. Element strain energies less than TINY will not be printed.

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Name

Type and Description

TIPSCOL

Integer. The number of tip superelements upstream of each downstream collector superelement. See ACMS=’YES’. Output by SEQP.

TITLEi

Character. Titles for VECPLOT module printed output.

TNSPAN23

DOPR3 updated temporary copy of TSPAN23, the table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

TOLAPPF

Integer. Nonlinear analysis type: 1

Nonlinear transient

0

Nonlinear statics

TOLRSC

Real. RSSCON element alignment tolerance factor.

TOTALK

Integer. Total number of harmonics. Output by CYCLIC1.

TOUT

Integer. TRLG processing flag.

TRD2OPT

0 if any retained response. Output by DSPRM.

WRDNUM

Integer. Word number of table element. Output by PARAML.

WTMASS

Real. Scale factor on structural mass matrix.

WVFLG

Integer. Weight/volume response flag. If CASECC does not contain any subcases for statics, normal modes, or buckling subcase then set to 1 if there is a weight or volume response specified on the DRESP1 Bulk Data entry image in EDOM. Output by MDCASE.

XFLAG

Integer. Strain energy method selection.

XNORM

0

Elemental force

1

Cross displacement

Real. Maximum absolute normalizing value over all columns. Output by NORM.

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Name

Type and Description

XNORMD

Real-double precision. Same as XNORM except in double precision.

XTYPE

Integer. Type of element matrix data: 0

Stiffness

1

Damping

2

Mass

Character. Degree-of-freedom set type.

XYSET

’SOL’

Solution set (d-set or h-set)

’DSET’

d-set

’HSET’

h-set

’PSET’

p-set

XYUNIT

Integer. FORTRAN unit number to which the DOM12 module writes design optimization x-y plot data.

ZCOLLCT

Integer. The absolute value is the number of collectors in the last level of a multilevel tree (see ACMS=’YES). If ZCOLLCT=0 ) $ AELOOP CASECC,EDT/ CASEA/ S,N,NSKIP/S,N,LPFLG/MFLG/S,N,MACH/S,N,Q $ NSKIP = NSKIP + 1 $ ENDDO $ LPFLG>=0

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2. Set up for divergence analysis. DO WHILE ( LPFLG>=0 ) $ Loop on number of subcases MFLG = 1 $ DO WHILE ( MFLG>0 ) $ Loop on Mach number AELOOP CASECC,EDT/ CASEA/ S,N,NSKIP/S,N,LPFLG/S,N,MFLG/S,N,MACH/S,N,Q $ ENDDO $ MFLG>0 ENDDO $ LPFLG>=0

9.9 AEMODEL Aerodynamic model loop driver Drives the aerodynamic model loop and sets parameter values for the generation of aerodynamic tables.

Format: AEMODEL

CASECC,EDT// S,N,NSKIP/S,N,LPFLG/S,N,AECONFIG/S,N,SYMXY/S,N,SY

Input Data Blocks: CASECC

Table of Case Control command images.

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

Output Data Blocks: None.

Parameters: NSKIP

Input/output-integer-default=0. Trim subcase counter.

LPFLG

Input/output-integer-default=0. Flag to indicate whether there is another case control record to process. Set to -1 for the last aerodynamic subcase.

AECONFIG

Output-character-no default. Aerodynamic configuration.

SYMXZ

Output-integer-no default. Aerodynamic z-y symmetry flag.

SYMXY

Output-integer-no default. Aerodynamic x-y symmetry flag.

9.10 AMG Builds aerodynamic influence matrix

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Generates a list of aerodynamic influence matrices (AJJT) and the transformation matrices needed to convert these to the aerodynamic grid points (SKJ, D1JK, D2JK).

Format: AMG

MKLIST,ACPT/ AJJT,SKJ,D1JK,D2JK/ NK/NJ/SYMXZ/SYMXY/REFC/S,N,MACH0/MACHNO/ KBAR/APP/SUPAERO $

Input Data Blocks: MKLIST

Aerodynamic matrix generation table

ACPT

Aerodynamic connection and property table

Output Data Blocks: AJJT

Aerodynamic influence matrix

SKJ

Integration matrix list

D1JK

Real part of downwash matrix

D2JK

Imaginary part of downwash matrix

Parameters: NK

Input-integer-no default. Number of degrees of freedom in k-set.

NJ

Input-integer-no default. Number of degrees of freedom in j-set.

SYMXZ

Input-integer-no default. Aerodynamic z-y symmetry flag.

SYMXY

Input-integer-no default. Aerodynamic x-y symmetry flag.

REFC

Input-real-no default.

MACH0

Input/output-real-default=-1.0. Previously processed Mach number.

MACHNO

Input-real-default=0.0. Mach number.

KBAR

Input-real-default = 0.0. Reduced frequency.

APP

Input-character-default=’ ’ Analysis type. ‘FREQRESP’- aeroelastic ‘FLUTTER’- flutter

SUPAERO

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Input-character-default=‘ZONA’ Method selection for supersonic aerodynamics. An alternate method is ‘CPM’

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Remarks: 1. Neither AERO nor ACPT can be purged. 2. D2JK is not used in aerostatic analysis.

Examples: 1. Set up AMG for aerostatic analysis. AMG

AERO,ACPT/ AJJT,SKJ,D1JK,D2JX/ NK/NJ/S,N,MACH0/MACH/0.0/‘STATICS’$

2. Set up AMG for aeroelastic or flutter analysis. AMG

AERO,ACPT/ AJJT,SKJ1,D1JK,D2JK/ NK/NJ/S,N,MACH0/MACH/KBAR $

9.11 AMP Generates modal aerodynamic matrices

Format: AMP

AJJT,WSKJF,D1JK,D2JK,GDKI,GPIK,GPKH,D1JE,D2JE, MKLIST,LAJJT,UAJJT/ QHH,QKH,QHJ/ NUMHDOF/NOUE/GUSTAERO/MACH/KBAR $

Input Data Blocks: AJJT

Aerodynamic influence matrix

WSKJF

Weighted integration matrix

D1JK

Real part of downwash matrix

D2JK

Imaginary part of downwash matrix

GDKI

Aerodynamic transformation matrix for displacements from the k-set to h-set

GPIK

Aerodynamic transformation matrix for loads from the h-set to k-set

GPKH

Aerodynamic transformation matrix for loads from the k-set to h-set

D1JE

Imaginary part of downwash matrix due to extra points

D2JE

Imaginary part of downwash matrix due to extra points

MKLIST

Table of Mach number and reduced frequency pairs

LAJJT

Lower triangular decomposition factor matrix of AJJT

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UAJJT

Upper triangular decomposition factor matrix of AJJT

Output Data Blocks: QHH

Aerodynamic matrix of size h- by h-set

QKH

Aerodynamic matrix of size k- by h-set

QHJ

Aerodynamic matrix of size h- by j-set

Parameters: NUMHDOF

Input-integer-no default. The number of modes.

NOUE

Input-integer-no default. The number of extra points.

GUSTAERO

Input-integer-default=0. QHJ computed only if GUSTAERO9, trailer word 1 contains a count of the number of data records on the file and word 2 contains the value of the NULL1 parameter.

Examples: 1. Generate a matrix [U] whose five columns are a vector {US} multiplied by the column number. DIAG

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SOL X COMPILE X SUBDMAP X TYPE PARM,,CS,N,CF $ TYPE PARM,,RS,N,FACTOR $ FILE U=APPEND $ MATGEN ,/US/5/1/7 $ DO WHILE ( FACTOR < 5. ) S FACTOR=FACTOR+1. CF=CMPLX(FACTOR,0.) $ ADD5 US,,,,/UI/CF $ APPEND UI,/U/2 $ ENDDO $ MATPRN U/ $ END $ CEND BEGIN BULK ENDDATA

2. Create a matrix B by appending five null columns to matrix A. APPEND

A,/B/1//5 $

3. Create a table with a one word record that contains the integer value 1001. APPEND

,,/OUT1/10//1001 $

9.14 ASDR Prints the aerodynamic extra point displacements and the aerodynamic pressures and forces as requested in Case Control.

Format: ASDR

CASEA,UXDAT,AECTRL,FFAJ,ACPT,PAK,AEUSET,AEBGPDT, AECOMP,MONITOR,MPSR,MPSER,MPSIR,MPSRPS,MPSERPS, AEMONPT,MPAR,MPAER,AERO,CSTMA// MACH/Q/AECONFIG/SYMXY/SYMXZ/IUNITSOL $

Input Data Blocks: CASEA

A single record (subcase) of CASECC for aerodynamic analysis

UXDAT

Table of aerodynamic extra point identification numbers, displacements, labels, type, status, position and hinge moments

AECTRL

Table of aeroelastic model controls

FFAJ

Matrix of pressures at aerodynamic boxes

ACPT

Aerodynamic connection and property table

PAK

Matrix of aerodynamic forces at aerodynamic boxes

AEUSET

Aerodynamic USET table

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AEBGPDT

Basic grid point definition table with the aerodynamic degrees of freedom added (ksa-set in AEUSET)

AECOMP

Aerodynamic component definition table

MONITOR

Structural monitor point table

MPSR

Rigid aerodynamic loads on structural monitor points at trim (excluding inertial loads and static applied loads)

MPSER

Elastic restrained loads on structural monitor points at trim (excluding inertial loads and static applied loads)

MPSIR

Inertial loads on structural monitor points at trim

MPSRP

Rigid loads on structural monitor points due to static applied loads

MPSERP

Elastic restrained loads on structural monitor points due to static applied loads

AEMONPT

Aerodynamic monitor point table

MPAR

Rigid aerodynamic loads on aerodynamic monitor points at trim

MPAER

Elastic restrained loads on aerodynamic monitor points at trim

AERO

Table of control information for aerodynamic analysis.

CSTMA

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points

Output Data Blocks: None.

Parameters: MACH

Input-real-no default. Mach number.

Q

Input-real-no default. Dynamic pressure.

AECONFIG

Input-character-no default. Aerodynamic configuration.

SYMXY

Input-integer-no default. Aerodynamic x-y symmetry flag.

SYMXZ

Input-integer-no default. Aerodynamic x-z symmetry flag.

IUNITSOL

Input-integer-default=0. If IUNITSOL=0, trim solution is being supplied. If IUNITSOL>0, IUNITSOL‘th unit solution is being supplied.

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9.15 ASG Computes the aerodynamic extra point displacements

Format: ASG

CASEA,AEMONPT,MONITOR,MPAERV,MPSERV,MPSIR,AEDBUXV, MPSERP,AECTRL,EDT,PRBDOFS,DIT,AEDBINDX/ UX,UXDAT,UXDIFV/SYMXZ/ISENS $

Input Data Blocks: CASEA

A single record (subcase) of CASECC for aerodynamic analysis

AEMONPT

Aerodynamic monitor point table

MONITOR

Structural monitor point table

MPAERV

Elastic restrained monitor point loads on aerodynamic model

MPSERV

Elastic restrained monitor point loads on structural model

MPSIR

Inertial loads on structural monitor points at trim

AEDBUXV

Matrix of vehicle states

MPSERP

Elastic restrained loads on structural monitor points due to static applied loads

AECTRL

Table of aerodynamic model‘s control definition

EDT

Table of Bulk Data entry images related to aerodynamics

PRBDOFS

Partitioning matrix to partition the "active" URDDI from the "inactive." Active URRDI are assigned a 1.0 value and are connected to the SUPORT degrees-of-freedom.

DIT

Table of TABLEij Bulk Data entry images

AEDBINDX

Aeroelastic database index for monitor point data

Output Data Blocks: UX

Matrix of aerodynamic extra point displacements

UXDAT

Table of aerodynamic extra point identification numbers, displacements, labels, type, status, position and hinge moments

UXDIFV

Derivative interpolation factors matrix at UX = UXREF

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Parameter: SYMXZ

Input-integer-no default. Aerodynamic x-z symmetry flag.

ISENS

Input-integer-default=0. Set to 1 if a sensitivity analysis is to be performed.

Remarks: 1. TR, KRZX, DIT, ERHM, and UXDAT can be purged if ISENS=1. 2. ASG solves the following equation for UX:

Equation 9-5. where the number of rows in the UX vector is equal to the number of aerodynamic extra points. The ZZX and PZ vectors have as many rows as there are r-set degrees of freedom. The IP matrix is a pseudo identity matrix with as many rows as there are constrained extra points specified on the TRIM Bulk Data entry. The IP matrix has ones in the row and columns corresponding to the constrained variable and zeros located elsewhere. The Y vector contains the magnitudes of the trim variable constraints. The AEL matrix contains the constraint relations (if any) specified by AELINK Bulk Data entries. It has as many rows as there are AELINK constraints. The sum of the number of supported degrees of freedom plus the number of TRIM constraints and number of AELINK constraints must equal the number of aerodynamic extra points.

9.16 AXMDRV Loop driver for auxiliary model processing

Format: AXMDRV

AMLIST//S,N,AUXMID/S,N,AUXMFL $

Input Data Blocks: AMLIST

List of auxiliary model identification numbers

Output Data Blocks: None.

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Parameters: AUXMID

Output-integer-default=0. Auxiliary model identification number.

AUXMFL

Output-logical-default=TRUE. Auxiliary model loop control flag. Set to FALSE when processing the last auxiliary model.

Remarks: AXMDRV is intended to be called in a DMAP loop. Each time through the loop AXMDRV outputs the current auxiliary model identification number defined in AMLIST. AUXMFL is TRUE except for the last call when AUXMFL is set to FALSE, that is, for the last auxiliary model.

Example: AUXMID=-1 $ INITIALIZE DO WHILE ( AUXMFL ) $ IF ( AUXMID=-1 ) THEN $ AUXMID=0 $ ELSE $ AXMDRV AMLIST//S,N,AUXMID/S,N,AUXMFL $ ENDIF $ . . . ENDDO $

9.17 AXMPR1 Builds a list of auxiliary model Bulk Data sections

Format: AXMPR1

CASECC*,BULK*/ AMLIST/ S,N,AMLFLG $

Input Data Blocks: CASECC*

Family of auxiliary model Case Control sections

BULK*

Family of auxiliary model Bulk Data sections

Output Data Blocks: AMLIST

List of auxiliary model identification numbers

Parameters: AMLFLG

Output-logical-default=FALSE. Set to TRUE if AMLIST if generated.

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Remarks: 1. All auxiliary model identification numbers that are specified on the AUXCASE command in the Case Control section (258th word in CASECC*) are written to the AMLIST table. 2. AXMPR1 checks for the following preliminary errors: Verify that the AUXCAS Case Control command specifies a unique and existing BULK file. Verify that each Bulk Data section is identified with a unique auxiliary model number.

Example: This is how AXMPR1 is used in subDMAP IFPL. CASEXX and IBULK are generated from IFP1 and XSORT. DBVIEW CASEXXAF = CASEXX (WHERE AUXMID>0) $ DBVIEW BULKAF = IBULK (WHERE AUXMID>0) $ AXMPR1 CASEXXAF,BULKAF/AMLIST $

9.18 AXMPR2 Merges the geometry of the primary model and an auxiliary model and create a Case Control table with PARTN command specifying auxiliary model grid points.

Format: AXMPR2

GEOM1,GEOM1A/ GEOM1C,CASEVEC/ AUXMID $

Input Data Blocks: GEOM1

Table of Bulk Data entry images related to geometry and assigned to the primary model

GEOM1A

Table of Bulk Data entry images related to geometry and assigned to the auxiliary model identified by AUXMID

Output Data Blocks: GEOM1C

Table of Bulk Data entry images related to geometry and merged from GEOM1 and GEOM1A

CASEVEC

Case Control table with the PARTN command referencing all of auxiliary model‘s grid identification numbers

Parameter: AUXMID

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Auxiliary Model Identification Number

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Remarks: AXMPR2 merges the primary model geometry (GRID and COORDi Bulk Data entry images) in GEOM1 with the auxiliary model in GEOM1A. AXMPR2 also writes the grid identification numbers from all of the auxiliary model grid points in GEOM1A to CASEVEC as a set referenced by the PARTN command.

9.19 BCDR Drives a DMAP loop based on the boundary condition Case Control commands SPC and MPC.

Format: BCDR

CASECC// SEID/SOLAPP/S,N,NSKIP/S,N,NLOADS/S,N,BCFLAG/S,N,SPC/ S,N,MPC/S,N,SUPORT/S,N,BCSET/S,N,BGSET/S,N,BOLTPRE/ S,N,RIGID/S,N,LOAD/S,N,LSEQ/S,N,STATSUB/ S,N,BC/ BCLABL $

Input Data Block: CASECC

Table of Case Control command images. Output by IFP1.

Output Data Block: None.

Parameters: SEID

Input-integer-no default. Superelement identification number.

SOLAPP

Input-character-no default. Design optimization analysis type. Currently not used.

NSKIP

Input/output-integer-no default. The record number in CASECC corresponding to the first subcase of the current boundary condition.

NLOADS

Output-integer-default=0. The number of subcase records contiguous with respect to the MPC and SPC command in the first subcase of the current boundary condition.

BCFLAG

Output-logical-no default. Set to FALSE at the last boundary condition.

SPC

Output-integer-default=0. SPC Case Control command set identification number specified in the third word of the SKIP-th record of CASECC

MPC

Output-integer-default=0. MPC Case Control command set identification number specified in the second word of the NSKIP-th record of CASECC.

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SUPORT

Output-integer-default=0. SUPORT Case Control command set identification number specified in the 255-th word of the NSKIP-th record of CASECC.

BCSET

Output-integer-default=0. Contact set identification number.

BGSET

Output-integer-default=0. Glue set identification number.

BOLTPRE

Output-integer-default=0. Bolt preload identification number.

RIGID

Output-character-default=linear. Selects the rigid element processing method for RBAR, RBE1, RBE2, RROD and RTRPLT elements.

LOAD

Output-integer-default=0. LOAD Case Control command set identification number specified in the fourth word of the NSKIP-th record of CASECC.

LSEQ

Output-integer-default=0. LOADSET Case Control command set identification number specified in the 205-th word of the NSKIP-th record of CASECC.

STATSUB

Output-integer-default=0. STATSUB Case Control command set identification number specified in the 256-th word of the NSKIP-th record of CASECC.

BC

Output-integer-default=0. BC Case Control command set identification number specified in the 257-th word of the NSKIP-th record of CASECC.

BCLBL

Input-integer-default=0. f06 file page header control. -1 Clear page header 0

Initialize page header without page eject

1

Initialize page header with page eject.

Example: Excerpt from subDMAP PHASE0: BCFLAG=TRUE $ NSKIP=0 $ DO WHILE ( BCFLAG ) $ BCDR CASES//SEID/’‘/ S,N,NSKIP/S,N,NLOADS/S,N,BCFLAG/S,N,SPC/S,N,MPC/ S,N,SUPORT/S,N,BCSET/S,N,BGSET/S,N,BOLTPRE/ S,N,RIGID/S,N,LOAD/S,N,LSEQ//S,N,BC $ . . . ENDDO $

9.20 BDRYINFO Generate the geometry and connectivity information for an external superelement definition based on the ASETi and QSETi Bulk Data entries and requested by the EXTSEOUT Case Control command.

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Format: BDRYINFO

CASECC,GEOM1,GEOM2,BGPDT,GPDT,USET/GEOM1EX,GEOM2EX,GEOM4EX,CASEX/ NOMATK/NOMATM/NOMATB/NOMATKY/NOMATP/DMIGSFIX $

Input Data Blocks: CASECC

Table of Case Control command images

GEOM1

Table of Bulk Data entry images related to geometry

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

BGPDT

Basic grid point definition table

GPDT

Grid point definition table

USET

Degree-of-freedom set membership table for g-set

Output Data Block: GEOM1EX

GEOM1 table containing records which define an external superelement. Specifically, it contains CORD1j, CORD2j, EXTRN, and GRID Bulk Data records.

GEOM2EX

GEOM2 table containing records which define an external superelement. Specifically, it contains PLOTEL and SPOINT Bulk Data records.

GEOM4EX

GEOM4 table containing records which define an external superelement. Specifically, it contains ASETi and QSETi Bulk Data records.

CASEX

Table of Case Control command images modified with additional output requests due to PLOTELs.

Parameters: NOMATK

NOMATM

Input-integer-default = -1. Stiffness matrix existence flag. -1

Does not exist

0

Empty

1

Exists

Input-integer-default = -1. Mass matrix existence flag. -1

Does not exist

0

Empty

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1 NOMATB

NOMATKY

NOMATP

DMIGSFIX

Exists

Input-integer-default = -1. Viscous damping matrix existence flag. -1

Does not exist

0

Empty

1

Exists

Input-integer-default = -1. Hysteretic damping matrix existence flag. -1

Does not exist

0

Empty

1

Exists

Input-integer-default = -1. Load matrix existence flag. -1

Does not exist

0

Empty

1

Exists

Input-character-default = “ DMIG matrices.

” (default = eight blank spaces). Suffix for

9.21 BGCASO Updates Case Control table for contact region data recovery operations.

Format BGCASO

CONTACT,BTOPO,CASECC,XYCDB/ CASECCBO/ S,N,NEWCASE/S,N,NBSORT2 $

Input Data Blocks: CONTACT

Table of Bulk Data entries related to contact regions

CASECC

Table of Case Control command images

BTOPO

Contact regions topological information table

XYCDB

Table of x-y plotting command

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Output Data Block: CASECCBO

Updated CASECC for contact region data recovery operations

Parameters: NEWCASE

Output-integer-no default. CASECCBO output flag. Set to 1 if CASSECBO is generated.

NBSORT2

Output-integer-default=0. Contact region output sort format flag. 1 if SORT2 format is requested for printing 2 if x-y plotting is requested

9.22 BGP Processes the geometry for the boundary contact regions. Updates the penalty values for slideline elements in the contact regions topological information table and creates a new boundary grid point element connection table.

Format: BGP

CSTM,SIL,KGGT/ BTOPO,BGPECT/ ADPCON/ISKIP $

Input Data Blocks: CSTM

Table of coordinate system transformation matrices

SIL

Scalar index list

KGGT

Total structural stiffness matrix in g-size (sum of linear, nonlinear and differential matrices)

Output Data Block: BTOPO

Contact regions topological information table

BGPECT

Boundary grid point element connection table

Parameters: ADPCON

Input-real-default=1.0. Scale factor for adjusting penalty values on restart. Update penalty values if positive.

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ISKIP

Input-integer-default=0. Counter to update penalty values; updates on first pass and no update later.

Remarks: 1. CSTM can be purged. 2. BTOPO is both input and output. See example.

Example: Excerpt of BGP for a nonlinear loop in SOL 106: FILE BGP COPY

BTOPSTF=APPEND/BTOPCNV=APPEND $ CSTMS,SILS,KGGT/BTOPSTF,BGPECT/ADPCONx/ISKIP $ BTOPSTF/BTOPCNV/-1/1 $

9.23 BMG Generates boundary matrices (in DMIG format) for hydroelastic analysis.

Format: BMG

MATPOOL,BGPDT,CSTM/ BDPOOL/ S,N,NOKBFL/S,N,NOABFL/S,N,MFACT $

Input Data Blocks: MATPOOL

Table of Bulk Data entry images related to hydroelastic boundary data

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

Output Data Block: BDPOOL

Hydroelastic boundary matrices in DMIG Bulk Data entry format

Parameters: NOKBFL

Output-integer-no default. Matrix KBFL existence flag; 0 if KBFL exists and -1 otherwise.

NOABFL

Output-integer-no default. Matrix ABFL existence flag; 0 if ABFL exists and -1 otherwise.

MFACT

Output-complex-no default. Scale factor for hydroelastic boundary mass matrix.

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Remarks: MTRXIN must always be used in conjunction with module BMG to produce the matrices. See example.

Example: Generate hydroelastic boundary matrices. BMG

MATPOOL,BGPDTS,CSTMS/ BDPOOL/ S,N,NOKBFL/S,N,NOABFL/S,N,MFACT $ ABFL = NOTL(NOABFL) $ IF ( ABFL OR NOTL(NOKBFL) ) MTRXIN ,,BDPOOL,EQDYN,,/ ABFL,KBFL,/ LUSETD/NOABFL/NOKBFL/0 $

9.24 BNDSPC Processes constraints and enforced displacements applied on superelement boundaries.

Format: BNDSPC

SEMAP,USET,BGPDT,YS,YSD/ USET1,YS1/ SEID/NLOADS $

Input Data Blocks: SEMAP

Superelement map table

USET

Degree-of-freedom set membership table

BGPDT

Basic grid point definition table for the current superelement

YS

Matrix of enforced displacements

YSD

Accumulated matrix of enforced displacements from upstream superelements

Output Data Blocks: USET1

USET updated with constraints from upstream superelements

YS1

YS updated with enforced displacements from upstream superelements

Parameters: SEID

Integer-input-default=0. Superelement identification number.

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Integer-input-default=0. The number of subcase records contiguous with respect to the MPC and SPC command in the first subcase of the current boundary condition.

Remarks: 1. BNDSPC performs one of three possible operations, depending on the coordinate system alignment at the boundary: a. Allow the SPC to be applied in the current superelement. b. Move the constraint to a downstream superelement. c. Issue a fatal error due to incompatible coordinate systems. 2. YS cannot be purged.

Example: Excerpt from subDMAP PHASE0 with BNDSPC in a superelement and boundary condition loop: DO WHILE (LPFLG >= 0) $ . . . BCFLAG=TRUE $ DO WHILE ( BCFLAG ) $ . . . BNDSPC EMAP,USET0,BGPDTS,YSB,YSD/ USET01,YSB1/ SEID/NLOADS $ EQUIVX USET01/USET0/-1 $ EQUIVX YSB1/YSB/-1 $ . . . ENDDO $ BCFLAG ENDDO $ LPFLG

9.25 BOLTFOR Calculates bolt forces from preload

Format: BOLTFOR

CASECC,BGPDT,CSTM,GEOM3,ECT,EDT,SIL/ BTFG,EBOLT,BNFDAT/NSKIP/S,N,LUSET/S,N,NBOLTS $

Input Data Blocks: CASECC

Table of case control command images.

BGPDT

Basic grid point definition table.

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CSTM

Table of coordinate system transformation matrices.

GEOM3

Table of Bulk Data entry images related to static and thermal loads.

ECT

Element connectivity table.

EDT

Element data table.

SIL

Scalar index list.

Output Data Blocks: BTFG

Bolt load vector applied to the g-set.

EBOLT

Table of element ids of bolt elements.

BNFDAT

Bolt element grid point force data.

Parameters: NSKIP

Input-integer-no default. Record number in CASECC corresponding to the first subcase of the current boundary condition.

LUSET

Integer-input-no default. Number of degrees of freedom in the g-set.

NBOLTS

Output-integer-no default. Number of bolts defined to be preloaded.

9.26 BOLTSF Calculates bolt strain force

Format: BOLTSF

CASECC,BGPDT,CSTM,GEOM3,KDICT,KELM,EDT,UG,BNFDAT/ BOLTFOR,BTSFG/NSKIP $

Input Data Blocks: CASECC

Table of Case Control command images.

BGPDT

Basic grid point definition table.

CSTM

Table of coordinate system transformation matrices.

GEOM3

Table of Bulk Data entry images related to static and thermal loads.

KDICT

Element stiffness dictionary.

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KELM

Element stiffness matrix.

EDT

Element data table.

UG

Displacements due to bolt preload forces in the g-set.

BNFDAT

Bolt element grid point force data.

Output Data Blocks: BOLTFOR

List of element numbers and bolt force for SDRX.

BTSFG

Bolt force vector due to initial strain applied to the g-set

Parameter: NSKIP

Input-integer-default=0. Number of cases to skip.

9.27 CASE Dynamic analysis case control loop driver Assembles the appropriate subcases (records) of Case Control for the current loop based on various Case Control commands.

Format 1: CASE

CASECC,PSDL/ CASEXX/ APP/S,N,NSKIP/S,N,NOLOOP/S,N,LINC/GMAFLG/ S,N,MSCHG/S,N,TESTNEG/S,N,IMETHOD/CASCOM1/CASCOM2/ CASCOM3/CASCOM4/CASCOM5/CASCOM6/CASCOM7/CASCOM8/ CASCOM9/CASCOM10/

Format 2: CASE

9-38

CASECC,MPT/ CASEXX/ APP/S,N,NSKIP/S,N,NOLOOP/S,N,LINC/LGDISP/ S,N,MSCHG/S,N,TESTNEG/S,N,IMETHOD/CASCOM1/CASCOM2/ CASCOM3/CASCOM4/CASCOM5/CASCOM6/CASCOM7/CASCOM8/ CASCOM9/CASCOM10/

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Input Data Blocks: CASECC

Table of Case Control command images.

PSDL

Power spectral density list. Applicable only when APP=‘FREQ’

MPT

Table of Bulk Data entry images for TSTEPNL, NLPARM, and NLPCI. Applicable only when APP=‘NONL’

Output Data Block: CASEXX

Subset of CASECC for current loop

Parameters: APP

NSKIP

Input-character-no default. Analysis type. ‘CEIG’

Complex eigenvalue

‘FREQ’

Frequency response

‘TRAN’

Transient response

‘NONL’

Nonlinear static or transient

‘SLIC’

Slice a contiguous subset of CASECC records into CASEXX; that is, NOLOOP number of records starting with the NSKIP-th record.

‘COMM’

Extract a slice of contiguous subset records, beginning at the NSKIP-th record, with the same Case Control command set identification numbers for command names specified in CASCOMi.

Input/output-integer-default=1. CASECC record counter or nonlinear transient loop identification number Input: ≤0

Skip one record on CASECC

>0

Number of records to skip on CASECC to reach the current subset of CASECC

Output: -1

No more cases

>0

and APP‘NONL’: Indicates the number of records to skip on CASECC to reach the next subset of CASECC.

>0

and APP=‘NONL’: Indicates that there are more CASECC records to process and NSKIP must be incremented in the DMAP.

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Output-integer-default=-1. Looping test flag -1

No DMAP looping is required.

1

DMAP looping is required.

LINC

Output-integer-default=0. Number of load increments for this subcase. Used in nonlinear static analysis only (APP=‘NONL’and IMETHOD=0).

GMAFLG

Input-integer-default=0. Test control flag for changes in the set identification numbers specified for the SDAMPING, K2PP, M2PP, B2PP, and TFL commands. Used only when APP=‘FREQ’or ‘CEIG’

LGDISP

MSCHG

TESTNEG

IMETHOD

0

Do not ignore changes (default).

1

Ignore changes.

Determines if large displacement effects are included in nonlinear solutions 106, 129, 153, and 159. SOLs 601 and 701 support LGDISP = +1 or -1 only. +1

All nonlinear element types that have a large displacement capability will have large displacement effects (updated element coordinates and follower forces).

-1

No large displacement effects will be considered.

2

Follower force effects will be ignored but large displacement effects will be considered.

≥0

The differential stiffness is computed for the linear elements and added to the differential stiffness of the nonlinear elements.

Output-integer-default=0. Boundary condition change flag. Used in nonlinear static analysis only (APP=‘NONL’and IMETHOD=0). -1

If MPC and SPC Case Control commands for this subcase are the same as those in the immediately preceding subcase.

1

If MPC or SPC commands are different.

Output-integer-default=-2. Load increment method flag. Used in nonlinear static analysis only (APP=‘NONL’and IMETHOD=0). -2

Standard

1

Controlled increment

Input/output-integer-default=0. Nonlinear transient analysis flag. Input:

9-40

0

Nonlinear static analysis (default)

0

Nonlinear transient analysis

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Output (nonlinear transient only):

CASCOMi

-1

Auto or TSTEP method (NLTRD module)

2

ADAPT method (NLTRD2 module)

Input-character-default=’ ’ Case Control command names. See APP=‘COMM’

Remarks: The method of operation depends upon APP and IMETHOD. APP=‘CEIG’: Complex eigenvalue analysis CASE

CASECC,/ CASEXX/ APP/S,N,NSKIP/S,N,NOLOOP//GMAFLG $

The first NSKIP records (subcases) on CASECC are skipped. The next record is read and copied onto CASEXX and an attempt is made to read the next record of CASECC. If this is not possible, NSKIP is set to -1 and, if this is the first entry into CASE, NOLOOP is set to -1. If the next record was read successfully and GMAFLG=0, the set identification numbers specified for the K2PP, M2PP, B2PP, TFL, and SDAMPING Case Control commands are compared with the previous subcase. If they all agree, this record is copied onto CASEXX and the process is nskiped. If they do not agree, NSKIP is incremented by 1 and NOLOOP is set to 1 and module is exited. APP=‘FREQ’: Frequency response CASE

CASECC,PSDL/ CASEXX/ APP/S,N,NSKIP/S,N,NOLOOP//GMAFLG $

Processing is the same as complex eigenvalue analysis, except that the set identification numbers specified for the FREQUENCY Case Control command is also compared. If the RANDOM command is specified, the selected set is read from PSDL and a list of subcase identification numbers referenced by the RANDPS Bulk Data entry images is made. If some subcases referenced by RANDPS Bulk Data entry images have not been output on CASEXX, CASE terminates with User Fatal Message 3033. APP=‘TRAN’: Linear transient response CASE

CASECC,/ CASEXX/ APP/S,N,NSKIP/S,N,NOLOOP $

The first NSKIP records (subcases) on CASECC are skipped. The next record is read and copied onto CASEXX and an attempt is made to read the next record of CASECC. If this is not possible, NSKIP is set to -1 and, if this is the first entry into CASE, NOLOOP is set to -1. APP=‘NONL’and IMETHOD=0: Nonlinear static analysis CASE

CASECC,MPT/ CASEXX/ APP/S,N,NSKIP//S,N,LINC/LGDISP/S,N,MSCHG/S,N,TESTNEG $

The first NSKIP records on CASECC are skipped. The next record is read and copied onto CASEXX. MSCHG is set to indicate whether the MPC or SPC set identification numbers have changed since the previous subcase. NINC is set equal to the value in the NINC field on the selected NLPARM Bulk Data entry image. If there is an associated NLPCI Bulk Data entry image, the controlled increment method is being used, and the TESTNEG parameter is set to

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indicate this. TEMPERATURE(INITIAL) and TEMPERATURE(LOAD) commands are checked for proper specification. If LGDISP>0 and ESE output is requested, INTOUT on the NLPARM bulk data entry must be set to “YES” for all subcases. If not, ESE output will be turned off. APP=‘NONL’and IMETHOD0: Nonlinear transient response CASE

CASECC,MPT/ CASEXX/ APP/S,N,NSKIP//////S,N,IMETHOD $

IMETHOD is set according to the METHOD field of the selected TSTEPNL Bulk Data entry image in MPT. NSKIP is set to the loop identification number.

Examples: 1.

Extract the load and subcase identification numbers and a parameter value from each subcase. SOL 100 COMPILE USERDMAP ALTER 2 TYPE PARM,,I,N,NSKIP $ TYPE PARM,,I,Y,MYPRM $ NSKIP=0 $ INITIALIZE DO WHILE ( NSKIP>=0 ) $ CASE CASECC,/CASE1/’TRAN’/S,N,NSKIP $ PVT PVT,CASE1/ $ PARAML CASE1//’DTI’/1/1//S,N,SUBID $ PARAML CASE1//’DTI’/1/4//S,N,ILOAD $ MESSAGE //’ SUBID=’/SUBID/’ MYPRM=’/MYPRM/ ’ ILOAD=’/ILOAD $ ENDDO $ CEND SUBCASE 101 PARAM,MYPRM,1 LOAD=111 SUBCASE 102 PARAM,MYPRM,-6 LOAD=222 SUBCASE 103 PARAM,MYPRM,4 LOAD=333 SUBCASE 104 PARAM,MYPRM,22 LOAD=444 SUBCASE 105 PARAM,MYPRM,-3 LOAD=555 SUBCASE 106 PARAM,MYPRM,77 LOAD=666 BEGIN BULK ENDDATA

2.

Extract Case Control records 10, 11, and 12. CASE CASECC,/CASE10/‘SLIC‘/10/3 $

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3.

Extract Case Control records with the same MPC, SPC, and SUPORT set identification numbers beginning at the NSKIP-th record. CASE CASECC,/CASEBC/‘COMM‘/S,N,NSKIP/ //////‘MPC‘/‘SPC‘/‘SUPO’$

9.28 CEAD Complex or unsymmetric eigenvalue analysis Given that [M], [B] and [K] are mass, damping, and stiffness, solve the equation:

or

for the eigenvalues p and the associated right eigenvectors {f} or left eigenvectors {fL}.

Format: CEAD

KXX,BXX,MXX,DYNAMIC,CASECC,VDXC,VDXR/ CPHX,CLAMA,OCEIG,LCPHX,CLAMMAT/ S,N,NEIGV/UNUSED2/SID/METH/EPS/ND1/ALPHAJ/OMEGAJ/ MAXBLK/IBLK/KSTEP/NDJ $

Input Data Blocks: KXX

Stiffness matrix. Usually KHH or KDD.

BXX

Viscous damping matrix. Usually BHH or BDD.

MXX

Mass matrix. Usually MHH or MDD.

DYNAMIC

Table of Bulk Data entry images related to dynamics.

CASECC

Table of Case Control command images.

VDXC

Partitioning vector with 1.0 at rows corresponding to null columns in KDD, BDD, and MDD.

VDXR

Partitioning vector with 1.0 at rows corresponding to null rows in KDD, BDD, and MDD.

Output Data Blocks: CPHX

Complex eigenvector matrix. Usually CPHH or CPHD.

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CLAMA

Complex eigenvalue summary table.

OCEIG

Complex eigenvalue extraction report.

LCPHX

Left-handed complex eigenvector matrix (Lanczos only). Usually LCPHH or LCPHD.

CLAMMAT

Diagonal matrix with complex eigenvalues on the diagonal. See Remark 8.

Parameters: NEIGV

Output-integer-no default. NEIGV indicates the number of eigenvalues found. If none were found, NEIGV is set to -1.

UNUSED2

Input-integer-default=1. Unused.

SID

Input-integer-default=0. Alternate set identification number. If SID=0, the set identification number is obtained from the CMETHOD command in CASECC and used to select the EIGC entry in DYNAMIC. If SID>0, the CMETHOD command is ignored and the EIGC entry is selected by this parameter value. Applicable for all methods If SID0) selects all items under version 4 for all values of SEID greater than 0 except 2. See “WHERE and CONVERT Clauses” WHERE and CONVERT Clauses for a further description. The default for VERSION and PROJECT is the current version and project. See also Remark 1.

Remarks: 1. The where-expr has the following rules: If the where-expr specifies a colname that is not assigned to the data block or parameter, none of that data block or parameter is deleted. For example, given that SPC is not a qualifier for KGG, the following DBDELETE statement does not delete any KGG: DBDELETE DATABLK=KGG WHERE(SPC=10)$

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If the where-expr does not specify a colname that is assigned to the data block (or parameter), the current value of the qualifier is assumed. For example, given that SEID is a qualifier for KAA, the following DBDICT statements are equivalent: SPC=10 $ DBDELETE DATABLK=KAA $

or DBDELETE DATABLK=KAA WHERE(SPC=10) $

The WILDCARD keyword can be added in order to wildcard all qualifiers not already specified in where-expr. For example, to delete all KAA where SPC=10 and regardless of MPC, SEID, and so on.: DBDELETE DATABLK=KAA WHERE(SPC=10 AND WILDCARD) $

Note: WILDCARD applies only to qualifiers and not colnames like PROJECT, PROJECT, VERSION, CDATE, and so on. 2. The data block and parameter names in datablk-list and param-list cannot be alias names specified on the subDMAP argument list. datablk-list and param-list must specify the name of the data block or parameter as defined in the NDDL.

9.45 DBDICT Prints database directory tables •

Data blocks described by an NDDL DATABLK statement

•

Parameters described by an NDDL PARAM statement

•

All unique paths (KEYs) and their qualifiers values

•

Qualifiers and their current values

•

Data blocks not described by an NDDL DATABLK statement

•

Parameters not described by an NDDL PARAM statement

•

Project and version information

Basic Format: The basic format of DBDICT specifies which tables to print and prints all items (data blocks and parameters) found in the directory. Also, the attributes (colnames) to be printed and the print format are predefined. Note that more than one table can be specified on the same DBDICT statement. DBDICT

[DATABLK PARAM PROJVERS QUALCURR QUALIFIERS]

Examples: DBDICT DBDICT PARAM PROJVERS

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Full Format: The full format permits the selection of items by name and/or by the WHERE describer. The full format also permits the attributes to be printed using the SELECT describer. In addition, the print format can be specified with the SORT, FORMAT, and LABEL describers. Note that the full format allows the specification of only a single table on a DBDICT statement.

SELECT(colname[- ’col-label’]. . . ), FORMAT

(FWIDTH = w [.d] LWIDTH = k

DWIDTH = w [.d]

COLSPACE = c

AWIDTH = a

IWIDTH = i,

VALUE = w,

colname = col-width, . . .),

Describers: DATABLK

Print the data blocks. datablk-list specifies a list of NDDL-defined data blocks separated by commas. If LOCAL is specified, the non-NDDL-defined data blocks are printed.

PARAM

Print the parameter table. param-list specifies a list of parameters separated by commas. If LOCAL is specified, the non-NDDL-defined parameters are printed.

PROJVERS

Print the project-version table.

QUALIFIERS

Print the qualifier table.

QUALCURR

Print the current values of the qualifiers. SORT is ignored.

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where-expr

Logical expression that specifies the desired values of colnames described below. For example, WHERE(VERSION = 4 AND SEID 2 AND SEID >0) selects all items under version 4 for all values of SEID greater than 0 except 2. See “WHERE and CONVERT Clauses” for a further description. The default for VERSION is the current version and PROJECT is the current project. The default for qual is * which is all qualifier values found on the database. See Remark 12.

SELECT

Specifies a list of column names to be printed. The order of the specified colnames is printed from left to right. If colname is not specified, all columns are printed.

colname

Column name. Colname specifies a particular attribute of the database item; such as data block name (NAME), creation date (CDATE), number of blocks (SIZE), or qualifier name (SEID, SPC, etc.). The allowable colnames are given in the Remarks.

col-label

The label to printed above the column identified by colname. The default for col-label is the colname. col-label cannot be specified for colnames: QUALSET, QUALALL, and TRAILER.

FWIDTH = w.d

Specifies the default width for single precision real numbers in real and complex qualifiers. (Integers: w >0 and d>0, Default = 12.5).

DWIDTH = w.d

Specifies the default width for double precision real numbers in real and complex qualifiers. (Integers: w > 0 and d > 0, Default = 17.10).

AWIDTH = a

Specifies the default width for character string qualifiers. Character strings are printed with enclosing single quotation marks, even if the string is blank. (Integer > 0, Default = 8.)

IWIDTH = i

Specifies the default width for integer qualifiers. (Integer > 0, see Remarks for defaults.)

LWIDTH = k

Specifies the default width for logical qualifiers. Logical values are printed as either “T” for TRUE or “F” for FALSE. (Integer >0, Default = 1.)

COLSPACE = c

Specifies the default number of spaces between columns. (Integer > 0, see Remarks for defaults).

VALUE = w

Specifies the default width for parameter values. The values are printed as character strings with left justification. (Integer>0, Default=40.)

col-width

The print width of the data under colname or qual-name. For real numbers, specify w.d where w is the width of the field and d is the number of digits in the mantissa. For integers and character strings, specify w where w is the width of the field. col-width cannot be specified for colnames: QUALSET, QUALALL, and TRAILER.

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SORT

Specifies how the rows are sorted. The sort based on ASCII sequence and is performed in order according to each colname specified in the list. A “D” following the colname causes the sort to be in descending order. An “A” following the colname causes the sort to be in ascending order. Colnames QUALSET, QUALALL, and TRAILER cannot be specified under SORT. Each colname specified in SORT must be separated by commas.

page-title

A title to be printed on each page of the directory output.

RIGHT, CENTER, LEFT

Print justification of the page title.

Remarks: 1. DBDICT prints seven different tables according to a default or user-defined format. The tables are: Describer

Description

Default page-title

See remark

DATABLK

Data blocks described by a NDDL DATABLK statement

NDDL DATABLOCKS

2

PARAM

Parameters described by a NDDL PARAM statement

NDDL PARAMETERS

3

QUALCURR

Current Qualifiers and their values

CURRENT QUALIFIERS

4

QUALIFIERS

Qualifiers and their values for each key number

QUALIFIERS

5

DATABLK(LOCAL)

Data blocks not described by a NDDL DATABLK statement

LOCAL DATABLOCKS

6

PARAM(LOCAL)

Parameters not described by a NDDL PARAM statement

LOCAL PARAMETERS

7

PROJVERS

Project-Version

PROJECT-VERSION

8

If DBDICT is specified without any describers, the NDDL Data Blocks Table are printed. See Remark 2. In an FMS statement, DATABLK(LOCAL) and PARAM(LOCAL) produce no output, and QUALCURR produces the default values specified on the NDDL QUAL statement. The defaults and allowable colnames for SELECT, FORMAT, SORT, and LABEL depend on the table. The defaults are described in the following remarks and tables. 2. The default print of the NDDL Data Blocks Table is obtained by: DBDICT

or DBDICT DATABLK

and is equivalent to:

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DBDICT DATABLK , SELECT(NAME,DATABASE,DBSET,PROJNO=’PROJ’,VERSION=’VERS’,CDATE, CTIME, SIZE,KEY,PURGED=’PU’,EQUIVD=’EQ’, POINTER=’FILE’,QUALSET) , FORMAT(NAME=8,DBSET=8,CDATE=6,CTIME=6,SIZE=5, KEY=4 ,PURGED=4,EQUIVD=4,POINTER=8, IWIDTH=5,COLSPACE=1) , SORT(PROJNO=A,VERSION=A,DBSET=A,NAME=A) , LABEL(’NDDL DATABLOCKS’ CENTER)

and looks like:

Listing 9-1. DBDICT PARAM Example The table below gives the allowable colnames along with a description that can be specified in the FORMAT, SELECT, and SORT describers. Column name

Default column width

Default column label

Description

PROJECT

40

PROJECT NAME

Project name defined by PROJECT statement

PROJNO

4

PROJ NO

Project number associated with PROJECT

VERSION

4

VERSION

Version number

CDATE

6

CDATE

Creation Date

CTIME

6

CTIME

Creation Time

NAME

8

NAME

Parameter name

DATABASE

8

DATABASE

MASTER DBset name

DBSET

8

DBSET

DBset name

RDATE

6

RDATE

Revision Date

RTIME

6

RTIME

Revision Time

SIZE

5

SIZE

Number of blocks

qual-name

See Note

qualifier name

Qualifier name

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Column name

Default column width

Default column label

Description

KEY

4

KEY

Key number

TRLi

8

TRLi

i-th word in the trailer

TRAILER

8

TRLi

All 10 trailer words

EXTNAME

8

EXTNAME

Extended name

EQUIVD

4

EQ

Equivalenced flag

PURGED

4

PU

Purged flag

EQFLAG

4

EF

Scratch equivalenced flag

SCRFLAG

4

SF

Scratch DBSET flag

POINTER

8

POINTER

Directory pointer

DBENTRY

8

DBENTRY

Database entry pointer

FEQCHAIN

8

FEQCHAIN

Forward equivalence chain

BEQCHAIN

8

BEQCHAIN

Backward equivalence chain

DBDIR20

9

DBDIR(20)

Directory word 20

QUALALL

See Note

qualifier name

All qualifiers

QUALSET

See Note

qualifier name

Predefined subset of all qualifiers

Note Default widths for qualifiers are DWIDTH=17.10, IWIDTH=5, LWIDTH=1, AWIDTH=8, and FWIDTH=12. 3. The default print of the NDDL parameter table is obtained by: DBDICT PARAM

and is equivalent to: DBDICT PARAM, SELECT(NAME,DATABASE,DBSET,PROJNO=’PROJ’,VERSION=’VERS’,CDATE,CTIME, KEY,VALUE,QUALSET), FORMAT(NAME=8,DATABASE=8,DBSET=8,CDATE=6,CTIME=6, KEY=4,VALUE=40,IWIDTH=5,COLSPACE=1), SORT(PROJNO=A,VERSION=A,DBSET=A,NAME=A), LABEL(’NDDL PARAMETERS’ CENTER)

and looks like:

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Listing 9-2. DBDICT PARAM Example The table below gives the allowable colnames along with a description that can be specified in the FORMAT, SELECT, and SORT describers. Column name

Default column width

Default column label

Description

PROJECT

40

PROJECT NAME

Project name defined by PROJECT statement

PROJNO

5

PROJ

Project number associated with PROJECT

VERSION

4

VERS

Version number

CDATE

6

CDATE

Creation Date

CTIME

6

CTIME

Creation Time

NAME

8

NAME

Parameter name

DATABASE

8

DATABASE

MASTER DBset name

DBSET

8

DBSET

DBset name

RDATE

6

RDATE

Revision Date

RTIME

6

RTIME

Revision Time

POINTER

8

POINTER

Directory pointer

VALUE

40

VALUE

Parameter value

KEY

4

KEY

Key number

qual-name

See Note

qualifier name

Qualifier name

QUALALL

See Note

qualifier name

All qualifiers

QUALSET

See Note

qualifier name

Predefined subset of all qualifiers

Note Default widths for qualifiers are DWIDTH=17.10, AWIDTH=8, IWIDTH=5, LWIDTH=1, and FWIDTH=12.5.

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4. The default print of the Qualifier Table is obtained by: DBDICT QUALIFIERS

and is equivalent to: DBDICT QUALIFIERS , SELECT(KEY QUALALL) , FORMAT(DWIDTH=17.10 AWIDTH=8 IWIDTH=5 LWIDTH=1 , FWIDTH=12.5 COLSPACE=2) SORT(KEY=A) , LABEL(’QUALIFIERS’ CENTER )

and looks like:

Listing 9-3. DBDICT QUALIFIERS Example QUALALL selects all qualifiers to be printed. The qualifiers are printed in alphabetic order. QUALSET selects only the qualifiers SEID, PEID, SPC, MPC, LOAD, and METH to be printed. The table below gives the allowable colnames along with a description that can be specified in the FORMAT, SELECT, and SORT describers. QUALALL and QUALSET cannot be specified in the FORMAT or SORT describers. The qualifier names and values are not printed one per row, but rather from left to right as one logical line that is allowed to wrap after 132 columns. Column name

Default column width

Default column label

Description

KEY

5

KEY

Key number

qual-name

See Note

qualifier name

Qualifier name

QUALALL

See Note

qualifier name

All qualifiers

QUALSET

See Note

qualifier name

Predefined subset of all qualifiers

Note Default widths for qualifiers are DWIDTH=17.10, IWIDTH=5, LWIDTH=1, and FWIDTH=12.5. AWIDTH defaults to the length specified on the QUAL statement in the NDDL sequence.

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5. The default print of the current qualifier values table is obtained by: DBDICT QUALCURR

and is equivalent to: DBDICT QUALCURR SELECT(QUALALL), FORMAT(AWIDTH=8,IWIDTH=5,LWIDTH=1,COLSPACE=2), LABEL=(’CURRENT QUALIFIERS’ CENTER)

and looks like:

Listing 9-4. DBDICT QUALCURR Example The table below gives the allowable colnames along with a description that can be specified in the SELECT describers. Column name

Default column width

Default column label

Description

qual-name

See Note

qualifier name

Qualifier name

QUALALL

See Note

qualifier name

All qualifiers

QUALSET

See Note

qualifier name

Pre-defined subset of all qualifiers

Note Default widths for qualifiers are DWIDTH=17.10, IWIDTH=5, LWIDTH=1, and FWIDTH=12.5. AWIDTH defaults to the length specified on the QUAL statement in the NDDL sequence. Note: DBDICT QUALCURR Colnames. 6. The default print of the local data block table is obtained by: DBDICT DATABLK(LOCAL)

and is equivalent to: DBDICT DATABLK(LOCAL), SELECT(NAME,SUBDMAP,SIZE=’BLOCKS’,PURGED=’PU’, EQUIVD=’EQ’,POINTER,TRL1,TRL2,TRL3,TRL4, TRL5,TRL6,TRL7), FORMAT(NAME=8,SUBDMAP=8,IWIDTH=8,COLSPACE=2), SORT(NAME=A) LABEL(’LOCAL DATABLOCKS’ CENTER)

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and looks like:

Listing 9-5. DBDICT DATABLK(LOCAL) Example TRLi specifies the data block trailer word i where 1 ≤ i ≤ 10. TRAILER selects all 10 data block trailer words. The table below gives the allowable colnames along with a description that can be specified in the FORMAT, SELECT, and SORT describers. Column name

Default column width

Default column label

Description

NAME

8

NAME

Parameter name

SUBDMAP

8

SUBDMAP

SubDMAP name

SIZE

8

BLOCKS

Number of blocks

EQUIVD

8

EQ

Equivalenced flag

PURGED

8

PU

Scratch flag

POINTER

8

POINTER

Directory pointer

TRLi

8

TRLi

i-th word in the trailer

TRAILER

8

TRLi

All 10 trailer words

EXTNAME

8

EXTNAME

Extended name

7. The default print of the local parameter table is obtained by: DBDICT PARAM(LOCAL)

and is equivalent to: DBDICT PARAM(LOCAL) SELECT(NAME,SUBDMAP,VALUE), FORMAT(COLSPACE=4,VALUE=40,AWIDTH=8), SORT(NAME=A) LABEL(’ LOCAL PARAMETERS’ CENTER)

and looks like:

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Listing 9-6. DBDICT PARAM(LOCAL) Example. The table below gives the allowable colnames along with a description that can be specified in the FORMAT, SELECT, and SORT describers. Column name

Default column width

Default column label

Description

NAME

8

NAME

Parameter name

SUBDMAP

8

SUBDMAP

SubDMAP name

VALUE

40

VALUE

Parameter name

8. The default print of Project Version Table is obtained by: DBDICT PROJVERS

and is equivalent to: DBDICT PROJVERS , SELECT(PROJECT=’PROJECT NAME’,PROJNO, VERSION ,DELFLG=’DELETED’ , CDATE=’CREATION DATE’ CTIME=’CREATION TIME’) , FORMAT(PROJECT=40,PROJ=10,VERS=10,DELFLG=7, COLSPACE=1 ,CDATE=13,CTIME=13) , LABEL(’PROJECT-VERSION’,CENTER) SORT(PROJNO=A,VERSION=A)

and looks like:

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Listing 9-7. DBDICT PROJVERS Example The table below gives the allowable colnames along with a description that can be specified in the FORMAT, SELECT, and SORT describers. Column name

Default column width

Default column label

Description

PROJECT

40

PROJECT NAME

Project name defined by PROJECT statement

PROJNO

10

PROJ NO

Project number associated with PROJECT

VERSION

10

VERSION

Version number

DELFLG

7

DELETED

Flag indicating whether this project/version has been deleted by the RESTART NOKEEP or DBCLEAN statements

CDATE

13

CREATION DATE

Creation Date

CTIME

13

CREATION TIME

Creation Time

CDATE is printed as YYMMDD where YY, MM, and DD are the year, month, and date, respectively. CTIME is HHMMSS where HH, MM, and SS are the hour, minute, and second, respectively. 9. If a parameter or qualifier value is defined to be a character string, the value is printed with enclosing single quotation marks. Blank strings are also printed with single quotation marks. 10. If a given qualifier is not in the path of a given data block or parameter, blank spaces are printed. 11. A line wraps if additional columns need to be printed and not enough space is available on the output (which is assumed to be 132). The first column of each additional line is to be indented by the width of the first column printed for the entry. 12. The where-expr has the following rules: •

If the where-expr specifies a colname that is not assigned to the data block or parameter, no directory information is printed for that data block or parameter. For example, given that SPC is not a qualifier for KGG, the following DBDICT statement produces no output: DBDICT DATABLK=KGG WHERE(SPC=10) $

•

If the where-expr does not specify a colname that is assigned to the data block (or parameter), the qualifier is wildcarded. For example, given that SEID is a qualifier for KAA, the following DBDICT statements are equivalent: DBDICT DATABLK=KAA $

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DBDICT DATABLK=KAA WHERE(SEID = *) $

Examples: 1. Print the Project Version Table with a title. DBDICT PROJVERS SORT(PROJNO,VERSION), LABEL(’PROJECT VERSION TABLE’ LEFT) $

2. Print a directory of all data blocks qualified with PEID = 10 or SEID = 10. Print columns for the NAME and DBSET, and the qualifiers SPC, MPC, and LOAD. DBDICT DATABLK SELECT(NAME,SPC,MPC,LOAD,DBSET,SIZE, SEID,PEID) , SORT(NAME,SIZE=D) WHERE( SEID=10 OR PEID=10) $

9.46 DBEQUIV Equivalences (or copies) NDDL data blocks and parameters Equivalences (or copies) NDDL data blocks and parameters based upon a qualifiers in a CONVERT clause. An optional WHERE and can be specified for a more selective equivalence.

Format:

Describers: datablk-list

Specifies a list of data blocks separated by commas. The default is *, which selects all data blocks. The equivalenced data block can be renamed by specifying a slash after the old name followed by the new name. For example, if KLL is to be renamed to KLL1, DATABLK=(KLL/KLL1) is specified.

param-list

Specifies a list of parameters separated by commas. The default is *, which selected all parameters. The equivalenced parameter can be renamed by specifying a slash after the old name followed by the new name. For example, if LUSETS is to be renamed to LUSET, PARAM=(LUSETS/LUSET) is specified.

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where-expr

Logical expression that specifies the desired values of colnames described in Table 2 under the DBDICT statement. If where-expr is true, the named items are equivalenced. For example, WHERE(VERSION=4 AND SEID2 AND SEID>0) selects all items under version 4 for all values of SEID greater than 0 except 2. See WHERE and CONVERT Clauses” for a further description. The default for VERSION and PROJECT is the current version and project. See Remark 1 for more information.

convert-expr

Modifies the values for PROJECT, VERSION, DBSET, and qualifiers selected by the where-expr. The format of convert-expr is: PROJECT=project-expr;VERSION=version-expr; DBSET=DBsetname;quali=qual-expri[;...]

For example, CONVERT (SEID=100+SEID; SPC=102). See “WHERE and CONVERT Clauses” for a further discussion on WHERE and CONVERT clauses. The default action for VERSION and PROJECT is to convert to the current version-ID and current project-ID. But if either PROJECT or VERSION is specified in the convert-expr, both must be specified. OVRWRT NOOVRWRT

RESTART

By default (that is, NOOVRWRT), duplicate data blocks or parameters on the created by DBEQUIV cause a fatal message. A duplicate means that a data block or parameter has not only the same name but also the same qualifier values, PROJECT, VERSION, and DBSET as the primary data block or parameter. If OVRWRT is specified, the primary data block is overwritten. By default, data blocks and parameters created by DBEQUIV cannot be output again in a subsequent DMAP module. If RESTART is specified, the selected data blocks and parameters can be overwritten once.

Remarks: 1. The where-expr has the following rules: If the where-expr specifies a colname that is not assigned to the data block or parameter, none of that data block or parameter is equivalenced. For example, given that SPC is not a qualifier for KGG, the following DBEQUIV statement does not equivalence any KGG: DBEQUIV DATABLK=KGG WHERE(SPC=10) CONVERT(SPC=20) $

If the where-expr does not specify a colname that is assigned to the data block (or parameter), the current value of the qualifier is assumed. For example, given that SEID is a qualifier for KAA, the following DBEQUIV statements are equivalent: SPC=10 $ DBEQUIV DATABLK=KAA CONVERT(SPC=20) $

or DBEQUIV DATABLK=KAA WHERE(SPC=10) CONVERT(SPC=20) $

The WILDCARD keyword can be added in order to wildcard all qualifiers not already specified in where-expr. For example, to equivalence all KAA where SPC=10 and regardless of MPC, SEID, and so on: DBEQUIV DATABLK=KAA WHERE(SPC=10 AND WILDCARD) CONVERT(SPC=20) $

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Note WILDCARD applies only to qualifiers and not colnames like PROJECT, PROJNO, VERSION, CDATE, and so on. 2. The data block and parameter names in datablk-list and param-list cannot be alias names specified on the subDMAP argument list. datablk-list and param-list must specify the name of the data block or parameter as defined in the NDDL.

9.47 SubDMAP DBFETCH Fetch data blocks stored by DBSTORE Retrieves user-specified data blocks on the database previously stored with CALL DBSTORE.

Format: CALL DBFETCH

/DB1,DB2,DB3,DB4,DB5/Q1/Q2/ FLAG/0/S,SUCCESS $

Input Data Blocks: None.

Output Data Blocks: DBi

Data blocks to be fetched. See Remark 3.

Parameters: Q1

Integer-input-no default. First qualifier.

Q2

Integer-input-no default. Second qualifier.

FLAG

Integer-input-no default. Name flag: 0 means fetch DBi with name DBi. 1 means drop the first character of DBi before searching the directory.

SUCCESS

Integer-output-no default. SUCCESS = -1 means all data blocks were successfully retrieved. SUCCESS = 0 means otherwise.

Remarks: 1. All parameters must be specified even if they are not used or the default value is desired. 2. DBi is equivalenced to the database data block named ZUZR11 qualified with ZNAME = DBi, ZUZR1 = Q1, ZUZR2 = Q2, ZUZR3 = 0. 3. If DBi appears on the SUBDMAP statement, the actual name of the data block to be stored on the database is the name that appears on the “highest” CALL statement that contains DBi. DIAG 47 can be specified so that the actual name is printed to the F06 file.

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4. If call DBFETCH is being used to obtain data blocks created in a previous run, the RESTART or DBLOCATE FMS statement must be specified. If DBLOCATE is used, DATABLK = * or DATABLK = (ZUZR11) must be specified on the DBLOCATE statement.

Example: Fetch data block named A (name flag = 1 drops the character E) and assign local name as EA. CALL DBFETCH /EA,,,,/1/1/1/0/S,EXIST $

9.48 SubDMAP DBMGR Functions on data blocks stored by DBSTORE Performs functions on items stored on the database with this subDMAP and CALL DBSTORE.

Format: CALL DBMGR

//OPT/P2/P3/P4/P5/P6/DB1/DB2/DB3/DB4/DB5 $

1. Directory print Print the contents of the database directory.

Format: CALL DBMGR

//2/0/0/0/0/0/ ’ ’/’ ’/’

’/’

’/’

’ $

Input Data Blocks: None.

Output Data Blocks: None.

Parameters: None. 2. Data block deletion Deletes up to five data block(s) previously stored with CALL DBSTORE.

Format: CALL DBMGR

//5/Q1/Q2/0/0/0/DB1/DB2/DB3/DB4/DB5 $

Parameters: Q1

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Q2

Integer-input-no default. Second qualifier of DBi.

DBi

Character-input-no default. Names of data blocks to be deleted

3. Data block equivalence Assign up to four alias names to one to four data blocks.

Format: CALL DBMGR

//7/QP1/QP2/QS1/QS2/0/ DBP/DBS1/DBS2/DBS3/DBS4 $

Parameters: QP1

Integer-input-no default. First qualifier of primary data block (DBP).

QP2

Integer-input-no default. Second qualifier of primary data block (DBP).

QS1

Integer-input-no default. First qualifier of secondary data block (DBSi).

QS2

Integer-input-no default. Second qualifier of secondary data block (DBSi). DBP Character-input-no default. Primary data block name.

DBSi

Character-input-no default. Secondary data block names to be equivalenced to DBP.

4. Data block rename Rename and/or modify the qualifier values of a data block previously stored with CALL DBSTORE.

Format: //9/QO1/QO2/QN1/QN2/0/ DBOLD/DBNEW/’ ’/’

CALL DBMGR

’ $

Input Data Blocks: None.

Output Data Blocks: None.

Parameters: QO1

Integer-input-no default. First qualifier of previously stored data block (DBOLD).

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QO2

Integer-input-no default. Second qualifier of previously stored data block (DBOLD).

QN1

Integer-input-no default. First qualifier of new name of data block (DBNEW).

QN2

Integer-input-no default. Second qualifier of new name of data block (DBNEW).

DBOLD

Character-input-no default. Name of the previously stored data block.

DBNEW

Character-input-no default. New name of the previously stored data block.

5. Store character string Store up to five character strings with qualifiers.

Format: CALL DBMGR

//10/Q1/Q2/0/0/0/STR1/STR2/STR3/STR4/STR5 $

Parameters: Q1

Integer-input-no default. First qualifier of STRi.

Q2

Integer-input-no default. Second qualifier of STRi.

STRi

Character-input-no default. Strings up to 8 characters in length.

6. Test for presence of a data block or a character string Test for the presence of a data block previously stored by CALL DBSTORE or a character string previously stored by CALL DBMGR (OPT=10).

Format: CALL DBMGR

//11/Q1/Q2/0/S,PRES1/S,PRES2/ DB1/DB2/’ ’/’ ’ $

Parameters: Q1

Integer-input-no default. First qualifier of DBi.

Q2

Integer-input-no default. Second qualifier of DBi.

PRESi

Integer-output-no default. 0 means DBi not present. -1 means DBi present.

DBi

Character-input-no default. Character strings or the names of data blocks.

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Remarks: 1. All parameters must be specified even if they are not used or the default value is desired. Unused integer parameters can be set to 0 and unused character parameters to ’ ’ (a string with 5 blanks). 2. If data blocks exist when storing, renaming or equivalencing, they are overwritten. 3. If CALL DBMGR is to be used in restart runs with the structured solution sequences (SOLs 101 through 200), PUTSYS(1, 109) should be specified immediately preceding CALL DBMGR and PUTSYS(0, 109) should be specified immediately following CALL DBMGR.

9.49 DBSTATUS Checks status of up to ten data blocks

Format: DBSTATUS

DB1,DB2,DB3,DB4,DB5,DB6,DB7,DB8,DB9,DB10// S,N,NODB1/S,N,NODB2/S,N,NODB3/S,N,NODB4/S,N,NODB5/ S,N,NODB6/S,N,NODB7/S,N,NODB8/S,N,NODB9/S,N,NODB10 $

Input Data Blocks: DBi

Any data block (matrix or table)

Output Data Blocks: None.

Parameters: NODBi

Output-integer-default=-1. Status of the DBi-th data block: -1

Not generated

0

Empty

1

Generated

10

Offline and empty

11

Offline and generated

Remarks: 1. Trailing commas in the input data block list can be omitted without warning. For example the following statement: DBSTATUS KAA,,,,,,,,,//S,N,NOKAA $

can be shortened to:

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DBSTATUS KAA//S,N,NOKAA $

2. DBSTATUS is similar to PARAML DB//‘PRES’with expanded capability for empty and offline data blocks; that is, PARAML returns -1 for empty data blocks and fatally terminates for offline data blocks.

9.50 SubDMAP DBSTORE Stores data blocks on the database Stores user-specified data blocks on the database. Data blocks can only be retrieved by CALL DBFETCH.

Format: CALL DBSTORE

DB1,DB2,DB3,DB4,DB5/DUMMY/Q1/Q2/DBSET/COND $

Input Data Blocks: DBi

Data blocks to be stored. See Remark 5.

Output Data Blocks: DUMMY

A dummy output data block is required to guarantee that the DBSTORE subdmap is executed when SYSTEM(109) = 0 (alternatively, see Remark 4). Otherwise, the output data block name may be left blank.

Parameters: Q1

Integer-input-no default. First qualifier of DBi.

Q2

Integer-input-no default. Second qualifier of DBi.

DBSET

Character-input-no default. The dbset-name to store DBi. The dbset-name must be padded with blanks to 5 characters in length; for example, ’DBDN ’.

COND

Integer-input-no default. Conditional store flag. COND = 0 means store and COND ≠ 0 means do not store.

Remarks: 1. All parameters must be specified even if they are not used or the default value is desired. Unused integer parameters can be set to 0. If DBSET is blank; that is, ’ ’ (a string with 5 blanks), DBi is stored on DBset DBALL. 2. DBi is stored under the database data block named ZUZR11 qualified with ZNAME = DBi, ZUZR1 = Q1, ZUZR2 = Q2, ZUZR3 = 0 on DBset = DBSET. 3. DBSET should not be ’SCRATCH’ or refer to a scratch dbset.

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4. If CALL DBSTORE is to be used in restart runs with the structured solution sequences (SOLs 101 through 200), PUTSYS(1, 109) should be specified just before CALL DBSTORE and PUTSYS(0, 109) just after. See Example 1. Another way to force execution, one without changing the value of system cell 109 or specifying an output block, is to use an actual parameter for COND, instead of an integer, together with the S,N prefix (See Example 3). This can be used as an alternative to specifying a DUMMY output block in non-restart runs where DBSTORE is called. 5. If DBi appears on the SUBDMAP statement, the actual name of the data block to be stored on the database is the name that appears on the “highest” CALL statement that contains DBi. DIAG 47 can be specified so that the actual name is printed to the F06 file.

Examples: 1. Store data block B on dbset DB100. PUTSYS(1, 109) $ deactivate restart skipping CALL DBSTORE B,,,,//2/2/’DB100’/0 $ PUTSYS(0, 109) $ activate restart skipping

2. The following example computes five variations on a basic matrix [K + liM][X] = [B], where K, B, and M are input via DMI Bulk Data entries and (li, i = 1,5) are input via DTI,LAMLST entries. In the first loop, the matrix KPLM is formed and decomposed and its factors, L and U, stored. In the second loop, the factors are fetched and, along with B, input to the FBS module to solve for X. SOL 100 COMPILE USERDMAP ALTER 2 $ TYPE PARM,,I,N,LOOPCNT=1,SING=0 $ TYPE PARM,,CHAR8,N,BX $ BLANK STRING TYPE PARM,,CS,N,LAMC $ DMIIN DMI,DMINDX/K,M,B,,,,,,, $ DTIIN DTI,DTINDX/LAMLST,,,,,,,,, $ MATPRN K,M,B/ $ DO WHILE (LOOPCNT-1) $ PARAML LAMLST//’DTI’/1/LOOPCNT/S,N,LAMBDA $ LAMC=CMPLX(LAMBDA) $ ADD K,M/KPLM//LAMC $ DECOMP KPLM/L,U/-1/////S,N,SING $ IF (SING>-1) THEN $ CALL DBSTORE L,U,,,//0/LOOPCNT/BX/0 $ LOOPCNT=LOOPCNT+1 $ ENDIF $ ENDDO $ $ IF (SING>-1) THEN $ CALL DBMGR //2/0/0/0/0/0/BX/BX/BX/BX/BX $ LOOPCNT=1 $ DO WHILE (LOOPCNT2 AND SEID>0) selects all items under version 4 for all values of SEID greater than 0 except 2. See “WHERE and CONVERT Clauses” and Remark 6.

Remarks: 1. DBVIEW is a nonexecutable statement defined only at compilation. It is not affected by IF ( ) THEN or DO WHILE blocks. Where-expr, however, is evaluated dynamically for the current values of data-block qualifiers at the module where view-name is specified for input. 2. DBVIEW must be specified prior to the first occurrence of the use of the view-name. It can be specified only as an input data block to a DMAP module. 3. If the data-block is “not generated” or if no data blocks satisfy the where-expr, the view-name is considered as “not generated.” Also, if the where-expr contains a qualifier that is not in the path of the data-block, the view-name is not generated. 4. view-name is recognized only in the current subDMAP. 5. A view-name that results in more than one data block is also called a family. If a family is specified as input to a module that does not use families, the first data block stored is the one that is used.

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6. The values assigned to qualifiers not specified in the where-expr are taken from current values. “AND WILDCARD” can be specified in the where-expr to indicate that unspecified qualifiers do not have to match their current values to satisfy the DBVIEW statement. 7. A comma can be used in place of the spaces shown under Format to continue the DBVIEW statement on more than one line. For example, DBVIEW UGX=UG, (WHERE SEID=10 AND, SPC=20, AND VERSION=5) $

Examples: 1. The following DBVIEW statement creates a view-name of KAA data blocks called KAA10 for the path qualifier (see the PATH NDDL-Statement) SEID = 10 and for the current values of the remaining KAA path qualifiers. DBVIEW KAA10 = KAA (WHERE SEID=10) $

2. The following DBVIEW statement creates a view-name of the data block BULK, which is stored under the version referenced on the RESTART FMS statement and gives it the virtual name BULKR to differentiate it from the current data block BULK. PROJVER //’RESTART’/S,N,RESPROJ/S,N,RESVER/ S,N,EXISTS $ DBVIEW BULKR = BULK (WHERE VERSION=RESVER AND PROJNO=RESPROJ) $

9.52 DCMP Matrix decomposition with extended diagnostics Decompose a square matrix [A] into upper and lower triangular factors [U ] and [L] and diagonal matrix [D]. DCMP is identical to DECOMP, but also provides extended diagnostics. [A] = [L] [U] for unsymmetric [A] [A] = [L][D][L]T for symmetric [A]

Format: DCMP

USET,SIL,EQEXIN,A,PARTVEC,EQMAP/ LD,U,LSEQ/ S,N,KSYM/CHOLSKY/BAILOUT/MAXRATIO/SETNAME/F1/DECOMP/ DEBUG/THRESH/S,N,MINDIAG/S,N,DET/S,N,POWER/S,N,SING/ S,N,NBRCHG/S,N,ERR/LMTROWS $

Input Data Blocks: USET

Degree-of-freedom set membership table

SIL

Scalar index list

EQEXIN

Equivalence between external and internal numbers

A

A square matrix (real or complex, symmetric or unsymmetric)

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PARTVEC

Partitioning vector specified when A is a partition of SETNAME. Its rowsize is indicated by SETNAME. A is the zero-th partition from PARTVEC.

EQMAP

Table of degree-of-freedom global-to-local maps for domain decomposition

Output Data Blocks: LD

Nonstandard lower triangular factor [L] and diagonal matrix [D] or Cholesky Factor. [LD] also contains [D] for symmetric decomposition.

U

Upper triangular factor or high ratios matrix. If A is unsymmetric, U is the nonstandard upper triangular factor of [A] or the Cholesky factor. If A is symmetric and the value of system cell 166 includes the value of 8, U contains the contains the "high ratio terms of the factor diagonal ratios." See Remark 4.

LSEQ

Resequencing matrix based on internal resequencing of A.

Parameters: KSYM

CHOLSKY

Input/output-integer-default=1. 1

Use symmetric decomposition (default).

0

Use unsymmetric decomposition.

-1

Use decomposition consistent with form of [A]. KSYM is reset to 0 or 1 consistent with actual decomposition type.

3

Use symmetric partial decomposition.

Input-integer-default=0. If KSYM=1 or KSYM=-1 and [A] is symmetric: 1

Use Cholesky decomposition.

0

Use standard decomposition (default).

If KSYM=3, CHOLSKY is set to the number of degrees of freedom in the o-set. BAILOUT

Input-integer-default=0. If BAILOUT≥0, the module exits with an error message if the factor-to-diagonal ratio exceeds MAXRATIO. If BAILOUT≤-1, the module continues with a warning message if the factor-to-diagonal ratio exceeds MAXRATIO.

MAXRATIO

Input-real-default=1.E5. See the BAILOUT and ERR parameter.

SETNAME

Input-character-default=‘H’. One or two letters indicating the set membership of [A].

F1

Input-real-default = 0.0. Tolerance for suppressing numbers of small magnitude. Matrix elements with magnitudes less than F1 are set to zero.

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DECOMP

Input-integer-default=-1. See the “DECOMP” module.

DEBUG

Input-integer-default=-1. See the “DECOMP” module.

THRESH

Input-integer-default=-6. See the “DECOMP” module.

MINDIAG

Output-real double precision-default=0.0D0. See the “DECOMP” module.

DET

Output-complex-default=(0.0,0.0). See the “DECOMP” module.

POWER

Output-integer-default=0. See the “DECOMP” module.

SING

Output-integer-default=0. See the “DECOMP” module.

NBRCHG

Output-integer-default=0. See the “DECOMP” module.

ERR

Output-integer-default=-1. If BAILOUT=-1, this parameter always remains at zero. If BAILOUT=0 and the factor-to-diagonal ratio is negative or greater than MAXRATIO, ERR is reset to -1.

LMTROWS

Input-integer-default=0. Number of Lagrange Multipliers appended to the A matrix. These rows are excluded from the internal reordering in the DCMP module.

Remarks: 1. This module performs all of the functions of the DECOMP module and responds to the same system cells. However, the DCMP module default for KSYM is 1 instead of -1, which is the default for DECOMP. All Remarks given for the DECOMP module also apply to the DCMP module. 2. If given unsymmetric matrices (“Form 1"), the mechanism diagnostics are not provided. The module is then functionally equivalent to the DECOMP module. 3. Data blocks USET, SIL, and PARTVEC and parameter SETNAME are required for the most efficient method of decomposition. PARTVEC is only required if A is not the same size as SETNAME. If data blocks USET and SIL are not available, SETNAME could be set as “NONE” for more efficient method of decomposition without grid compression. 4. If A is symmetric, U contains the "MATRIX/FACTOR DIAGONAL RATIO values printed under UWM 4698. The mathematical definition of U is Diag(A) = Ad, a vector. Diag(T) = Dd, a vector. In some circumstances T is not a diagonal matrix. The high ratio test being defined here has no validity in the regions where there are off-diagonal terms (2 by 2 pivots), so those rows are ignored in this testing. The ratio is defined as Vi = Adi/Ddi Regions where the model is approaching singularity have small Ddi terms. They are divided into Adi to non-dimensionalize them, and checked against a quality parameter value named MAXRATIO. The default value for MAXRATIO is 1.E7, but you can change its value. Terms less than MAXRATIO are set to zero in Vi. If any terms remain, the matrix is identified as

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singular, and various warning and fatal messages can appear, depending on the context in which the DCMP module is being called. This vector can be used to better identify singularities and provide other actions when they are being approached. This feature is used in normal modes analysis, where points with high ratios are automatically constrained to ground, to make the eigensolution more stable.

Example: Inspect the numerical conditioning of the [Mmaa] matrix. If the matrix is poorly conditioned, diagnostics are produced. DCMP USET,SIL,EQEXIN,MMAA,/LAA,UAA,/////’A’ $ DIAGONAL LAA/DLAA $ MATPRN DLAA/$

9.53 DDR2 Computes displacements due to mode acceleration Improves accuracy of modal transient or frequency response displacements by computing displacements due to mode acceleration.

Format: DDR2

USETD,UD,PD,KDD,BDD,MDD,OL,UNUSED,LLL,DM/ UD1,UE,PD1/ APP/NOUE/UNUSED1/UNUSED2 $

Input Data Blocks: USETD

Degree-of-freedom set membership table for p-set

UD

Solution matrix for the d-set. Displacements only in frequency response. Displacements, velocities, and accelerations in transient response.

PD

Dynamic load matrix for the d-set

KDD

Stiffness matrix for the d-set

BDD

Damping matrix for the d-set

MDD

Mass matrix for the d-set

OL

Transient response time output list or frequency response frequency output list

LLL

Lower triangular factor/diagonal for the l-set

DM

Rigid body transformation matrix for the r-set to the l-set

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Output Data Blocks: UD1

Improved solution matrix for the d-set

UE

Improved solution matrix for the e-set (extra points)

PD1

Equivalent load vector for mode acceleration computations for the a-set

Parameters: APP

Input-character-no default. Analysis type. ‘TRAN’: transient response ‘FREQ’: frequency response

NOUE

Input-integer-default=-1. The number of extra points.

UNUSED1

Input-integer-default=-1. Unused.

UNUSED2

Input-integer-default=-1. Unused.

Remarks: 1. The solution matrix, UD1, can also be used to improve the data recovery output; such as, stress, strain, and so on. 2. USETD, UD, PD, MDD, OL, and LLL cannot be purged. 3. DM cannot be purged if support degrees-of-freedom exist. 4. For transient analysis, the velocities and accelerations (every second and third column in UD) are unchanged in UD1. 5. DDR2 uses a static approximation for the effect of the higher modes.

Method: The equivalent load vector is computed:

Equation 9-6. For a transient analysis problem {ud}, { }, and {üd} are given explicitly. For frequency response analysis,

Equation 9-7.

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Equation 9-8. where w is the forcing frequency and {ud} is the complex response vector. w comes from PPF. The vector {Pad} is the sum of applied loads and inertia loads due to the motion of the system approximated by its lower modes. The static solution using these loads provides a better answer for displacements. If extra points are present,

Equation 9-9.

Equation 9-10. {ue} is placed in data block UEVF. Subroutines CALCV and SSG2A perform this calculation. If supports are present,

Equation 9-11.

Equation 9-12. Solve for {uaa}:

Equation 9-13. This is accomplished in subroutine FBSDRV. If supports are present,

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Equation 9-14. otherwise, {uaa} = {ual}.Subroutine SDR1B performs this calculation. If extra points are present,

Equation 9-15. Note: If the problem type is transient, {uad} must be merged with { }, and {üd}.

9.54 DDR2N Computes displacements due to the new method of mode acceleration Improves accuracy of modal transient or frequency response displacements by computing displacements due to the new method of mode acceleration.

Format: DDR2N

UHF,KHH,BHH,MHH,PHDH,OL,CONMODS,YS, EAMACC,EAMVEL,EAMDIS,LDATTMOD,PFFTAB/ UD1/ APP $

Input Data Blocks: UHF

Solution matrix for the h-set. Displacements only in frequency response. Displacements, velocities, and accelerations in transient response.

KHH

Stiffness matrix for the h-set

BHH

Damping matrix for the h-set

MHH

Mass matrix for the h-set

PHDH

Mode shape matrix for (d-set) – (e-set)

OL

Transient response time output list or frequency response frequency output list

CONMODS Constraint modes

YS

Enforced motion

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EAMACC

Equivalent mass attachment modes

EAMVEL

Equivalent viscous damping attachment modes

EAMDIS

Equivalent structural damping attachment modes

LDATTMOD Load attachment modes PFFTAB

Table values for applied loads

Output Data Blocks: UD1

Solution matrix for the d-set

Parameters: APP

Input-character-no default. Analysis type. ‘TRAN’: transient response ‘FREQ’: frequency response

Remarks: 1. The solution matrix, UD1, may be used to improve the data recovery output; such as, stress, strain, and so on. 2. UHF, KHH, MHH, PHDH and OL cannot be purged. 3. CONMODS and YS cannot be purged if enforced motion exists.

Method: The dynamic equations of motion can be written as

Equation 9-16. where

= mass, viscous damping, stiffness, and structural damping matrices.

uf = absolute displacements of the f-set dof = effective external forces in which Pf = loads applied to the f-set dof us = enforced motion applied to the s-set dof

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The displacements can be calculated by rewriting equation 9-16 into the following format:

Equation 9-17. Velocities and accelerations are still recovered directly from the normal modes responses as:

Equation 9-18.

Equation 9-19. where

= matrix of normal modes

= matrix of constraint modes of enforced motion dof = = vector of modal velocities = vector of modal accelerations Substituting equations 9-18 and 9-19 into equations 9-17, displacements can be calculated by:

Equation 9-20. where

= =

matrix of attachment modes due to applied forces = matrix of equivalent mass attachment modes

= =

matrix of equivalent viscous damping attachment modes

= =

matrix of equivalent structural damping attachment modes

= Ω= =

diagonal matrix of m-th natural frequency

m=

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c=

(in general, not diagonal)

=

(in general, not diagonal)

If rigid body modes exist, the responses can be calculated by including the rigid body motion term

into equation 9-20,

where

= matrix of rigid body modes

= modal displacements of rigid body modes.

9.55 DDRMM Performs matrix method data recovery. Computes data recovery items (stress, displacements, forces, strains, forces) directly from the modal solution in frequency response, transient response, or scaled response spectra analysis using the matrix method.

Format: DDRMM

CASECC,UH,OL,IUG,IQG,IES,IEF,XYCDB,IUG1,IQG1,IES1,IEF1,UHD/ OUG,OQG,OES,OEF,UNUSED5/ OPTION/NOCOMP/PEXIST/ACOUSTIC/ACOUT/PREFDB/SEID/APP $

Input Data Blocks: CASECC

Table of Case Control command images.

UH

Solution matrix for the h-set (modal degrees-of-freedom). Modal displacements only in frequency response. Modal displacements, velocities, and accelerations in transient response.

OL

Transient response time output list or frequency response frequency output list.

IUG

Table of displacements due to unit modal displacement in SORT1 or SORT2 format.

IQG

Table of single point forces of constraint due to unit modal displacement in SORT1 or SORT2 format.

IES

Table of element stresses or strains due to unit modal displacement in SORT1 or SORT2 format. For strains, NOCOMP must be set to 3.

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IEF

Table of element forces due to unit modal displacement in SORT1 or SORT2 format.

XYCDB

Table of x-y plotting commands.

IUG1

Table of displacements due to unit modal displacement in SORT1. Required only for the sparse data recovery in SORT2 format.

IQG1

Table of single point forces of constraint due to unit modal displacement in SORT1 format. Required only for the sparse data recovery in SORT2 format.

IES1

Table of element stresses or strains due to unit modal displacement in SORT1 format. Required only for the sparse data recovery in SORT2 format.

IEF1

Table of element forces due to unit modal displacement in SORT1 format. Required only for the sparse data recovery in SORT2 format.

UHD

Modal velocities solution matrix for the h-set (modal degrees-of-freedom). Required only for frequency response.

Output Data Blocks: OUG

Table of displacements in SORT1 or SORT2 format

OQG

Table of single point forces of constraint SORT1 or SORT2 format

OES

Table of element stresses or strains in SORT1 or SORT2 format

OEF

Table of element forces in SORT1 or SORT2 format

UNUSED5

Unused and can be purged

Parameters: OPTION

Input-character-default=‘ABS’ Response summation method for scaled response spectra analysis only. Possible values are: ‘ABS’

Absolute

‘SRSS’

Square root of the sum of the squares

‘NRL’

Naval Research Laboratory (new)

‘NRLO’

Naval Research Laboratory (old)

NOCOMP

Input-integer-default=0. Set to 3 if IES is element strains.

PEXIST

Input-logical-default=FALSE. Set to TRUE if p-elements are present.

ACOUSTIC

Input-integer-default=0. Fluid-structure analysis flag. 0

No fluid elements exist.

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1

Penalty or fluid acoustic elements exist.

2

Fluid/structure coupling exists.

Input-character-default=‘PEAK’ Type of acoustic pressure output in fluid-structural analysis. ‘RMS’

Root-mean-square

‘PEAK’

Peak

PREFDB

Input-real-default=1.0. Peak pressure reference for pressure level in units of dB or dBA.

SEID

Input-integer-default=0. Superelement identification number. When APP=’DDAM’ this value is an integer 1,2 or 3 to indicate if X,Y or Z results are stored in the output data blocks.

APP

Input-character-default=’ ‘. Analysis type. For modal complex eigenvalue analysis, set to ‘CEIG’; for DDAM analysis, set to ‘DDAM’; otherwise, leave blank.

Remarks: 1. If UH is a real matrix and OL is purged, a scaled response spectra analysis is assumed. 2. OUG, OQG, OES, and OEF are suitable for printing or punching by the OFP module. 3. SDR2 is used to compute IUG, IQG, IES, and IEF, which are results due to a unit modal displacement (eigenvector).

9.56 DECOMP Matrix decomposition To decompose a square matrix [A] into upper and lower triangular factors [U] and [L] and diagonal matrix [D].

Format: DECOMP

9-104

A/LD,U,LSEQ/S,N,KSYM/CHOLSKY/S,N,MINDIAG/S,N,DET/ S,N,POWER/S,N,SING/S,N,NBRCHG/S,N,MAXRAT/DECOMP/ DEBUG/THRESH $

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Input Data Block: A

Square matrix (real or complex; symmetric, or unsymmetric, or indefinite symmetric).

Output Data Blocks: LD

Lower triangular factor [L] and diagonal matrix [D] or Cholesky Factor. [LD] also contains [D] for symmetric decomposition.

U

Upper triangular factor or trapezoidal factor for partial decomposition. (See Remark 4.)

LSEQ

Resequencing matrix based on internal resequencing of A.

Parameters: KSYM

CHOLSKY

Input/output-integer-default=-1. 1

Use standard decomposition.

0

Use unsymmetric decomposition.

-1

Use decomposition consistent with form of [A]. KSYM is reset to 0 or 1 consistent with actual decomposition type (default).

3

Use symmetric partial decomposition. Sparse method is not available with partial decomposition.

Input-integer-default=0. If KSYM = 1 or KSYM = -1 and [A] is symmetric: 1

Use Cholesky decomposition.

0

Use standard decomposition (default). If KSYM = 3, CHOLSKY is set to the number of degrees of freedom in the o-set.

MINDIAG

Output-real double precision-default = 0.0D0. The norm of the minimum diagonal term of [U].

DET

Output-complex single precision-default=(0.0,0.0). The scaled value of the determinant of [A]. See the POWER parameter. DET is not applicable to sparse methods. See Remark 1.

POWER

Output-integer-default=0. Integer POWER of 10 by which DET should be multiplied to obtain the determinant of [A]. In other words, the determinant of [A] is equal to DET*10POWER. POWER is not applicable to sparse methods. See Remark 1.

SING

Output-integer-default=0. SING is set to -1 if [A] is singular. See Remark 3.

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NBRCHG

Output (for symmetric decomposition only)-integer-default=0. NBRCHG is the number of negative terms on the diagonal.

MAXRAT

Output (for symmetric decomposition only)-real-default=0.0. MAXRAT is the maximum value of the ratio of the matrix diagonal to the factor diagonal.

DECOMP

Input-integer-default=-1. Controls operation of module for exceptional conditions as defined in the following table. If DECOMP > 0, DECOMP overrides the value specified on NASTRAN SYSTEM(69) statement. DECOMP

Action

0 or -1

Print up to 50 messages for null columns and zero diagonals (non-sparse method only).

1

Terminate execution when first null column is encountered.

2

Suppress printing of message when a null column is encountered (non-sparse method only).

4

Terminate execution when first zero diagonal term is encountered.

8

Suppress printing of message when a zero diagonal term is encountered (non-sparse method only).

16

Place 1.0 in diagonal position for all null columns and proceed with the decomposition.

32

Stop the decomposition when zero diagonal terms are encountered.

64

Exit after execution of preface for symmetric decomposition.

DEBUG

Input-integer-default=-1. Passive column logic control. DEBUG is used only by non-sparse method. See the NX Nastran Numerical Methods User’s Guide and Remark 8.

THRESH

Input-integer-default=-6. Power of 10 defining the pivoting threshold for unsymmetric decomposition. Row pivoting is done if any value on the factor diagonal is less than 10THRESH. Siemens PLM Software recommends using THRESH = -2 for indefinite matrices because accuracy is improved even though execution time is increased.

Remarks: 1. By default, the DECOMP module uses sparse matrix methods. See the NX Nastran Numerical Methods User’s Guide. a. The DECOMP parameter options 0, -1, 2, and 8 are ignored with the sparse method. b. The precision of A must be equivalent to the machine precision.

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c.

Cholesky decomposition is not supported under this method; that is, the parameter CHOLSKY = 1 is ignored.

d. NASTRAN statement system cell 166 selects options for the sparse method. 0

No action

1

If insufficient core is encountered, switch to conventional decomposition and continue (default)

2

Print diagnostics

4

Do not issue fatal message if maximum ratios are exceeded. The maximum ratios are replaced by 1.0.

2. Nonstandard triangular factor matrix data blocks are used to improve the efficiency of the back substitution process in module FBS. 3. if the value of 16 is specified for the DECOMP parameter, SING is set to one if unit values are placed on the diagonal. 4. if KSYM = 3, the [A] matrix is decomposed through the first n degrees of freedom, where n is the value provided by the CHOLSKY parameter. The resulting trapezoidal factor is output as [L] and the remaining undecomposed partition of the [A] matrix, with contributions from the first n degrees of freedom added, is output as [U ]. 5. Cholesky factors (matrix form 10) can be used for all standard matrix operations; for example, ADD, MPYAD, and so on. All other factors are packed, nonstandard data blocks as described in Remark 2 and cannot be processed by other matrix modules except where noted. 6. The output triangular and trapezoidal matrices has the following forms in the matrix trailer: Form

Factor type

Matrix type

4

Lower triangle

Symmetric or unsymmetric

5

Upper triangle

Unsymmetric only

10

Cholesky

Symmetric only

11

Trapezoidal

Symmetric only

13

Lower triangular

Sparse symmetric

15

Lower or upper triangular

Sparse unsymmetric

7. In decomposing symmetric matrices, [A] = [L] [D] [L]T, the diagonal factor [D] is stored in the diagonal of the [LD] matrix output. The [U ] = [L]T factor is not output for this case. 8. Matrices with zero diagonal terms can be reliably solved if the corresponding leading minor is nonzero. A more conservative course is to take a fatal error exit when zero diagonals occur, regardless of the value of the leading minor. This action is obtained by setting DECOMP = 32.

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Chapter 9

9. Parallel sparse decomposition is selected with the NASTRAN statement keyword PARALLEL (or SYSTEM (107)). To obtain optimal performance, Siemens PLM Software also recommends that the SEQP module be used with parameter NEWSEQ = 2.

Examples: 1. Solve [A][X] = [B]. DECOMP FBS MATPRN

A/L,U,/ $ L,U,B/X/ $ X// $

2. Form [K] = [G]T[A][G]. Then decompose [K] into [L] [L]T assuming that [K] is a symmetric matrix. SMPYAD DECOMP

G,A,G,,,/K/3////1////6 $ K/L,,/ $

3. Calculate following:

using partial decomposition, form [Loo] given the

•

NOOSET integer parameter defining the size of [Koo].

•

NOASET integer parameter defining the size of [Kaa] and [Koa].

•

NOFSET = NOOSET + NOASET $ FORM PARTITIONING VECTOR MATGEN ,/VFOX/6/NOFSET/NOOSET/NOASET $ $ MERGE O-SET AND A-SET WITH A-SET LAST MERGE KOO,KAO,KOA,KAAB,VFOX,/KFFX/-1/0/6 $ $ PARTIALLY DECOMPOSE KFFX DECOMP KFFX/LFO,KAA,/3/NOOSET $ PARTN LFO, ,VFOX/LOO, LAO, ,/1 $

9.57 DELETE Deletes data blocks

Format: DELETE

/DB1,DB2,DB3,DB4,DB5 $

Input Data Blocks: None.

Output Data Blocks: DBi

Any table or matrix.

Parameters: None.

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Remarks: 1. Any or all data blocks can be purged. 2. The output from previous module rule does not apply.

Example: DELETE

/A,B,C,, $

9.58 DIAGONAL Extracts diagonal from matrix or raises matrix to a power Extracts the diagonal elements from a matrix, raises each term to a specified power, and outputs a vector (column matrix) or a rectangular matrix.

Format: DIAGONAL

A/B/OPT/POWER $

Input Data Block: A

OPT ≠ ‘WHOLE’ means A is a square or diagonal matrix (real or complex). OPT = ’WHOLE’ means A is a rectangular matrix (real or complex).

Output Data Block: B

Real vector (column matrix) or a rectangular matrix containing the terms of A raised to a power

Parameters: OPT

Input-character-default=‘COLUMN’ Type of matrix output. ’COLUMN’

Extract the diagonal elements of square matrix A into vector B (if A is complex, only the real part is extracted) and raise the elements to the exponent POWER.

‘SQUARE’

Extract the diagonal elements of square matrix A into diagonal matrix B (if A is complex, extract only the real part) and raise the elements to the exponent POWER.

’WHOLE’

Copy rectangular matrix A into rectangular matrix B and raise the elements to the exponent POWER. If A is complex and POWER1.0, extract only the real part. However, if POWER=1.0, B contains the magnitude of the elements.

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’MAGCOL’

Extract the magnitude of the diagonal elements of square matrix A into vector B and raise the elements to the exponent POWER.

’MAGSQ’

Extract the magnitude of the diagonal elements of square matrix A into diagonal matrix B and raise the elements to the exponent POWER.

’CMPCOL’

Extract the diagonal elements of complex square matrix A into complex vector B.

’CMPSQ’

Extract the diagonal elements of complex square matrix A into complex diagonal matrix B.

Input-real single precision-default=1. Exponent to which the real part or the magnitude of each element is raised. See Remarks.

Remarks: 1. OPT = ’COLUMN’ or ’SQUARE’ provides exactly the same functions, except that the output using COLUMN is a vector, and the output using SQUARE is a square diagonal matrix. Both options process only the real part of the diagonal terms of the input matrix. If POWER = 0, unit column or the identity matrix of the dimension of the input matrix is produced. This is an efficient method for producing these useful DMAP tools. OPT = ’WHOLE’ operates on all terms of the input matrix to produce an output matrix of the same dimension. Sparse factor matrices (form = 11, 13, or 15) are not supported with OPT = ’WHOLE’. Each term is processed independently. 2. OPT = ’WHOLE’ operates on all terms of the input matrix to produce an output matrix of the same dimension. Sparse factor matrices (form = 11, 13, or 15) are not supported with OPT = ’WHOLE’. Each term is processed independently. If POWER = 0, all nonzero terms of [A] produce unit terms in [B]. Zero terms in [A] produces zero terms in [B]. This is a means for producing Boolean matrices. [A] can be either real or complex. If POWER = 1.0, [B] is a real matrix with terms that are the absolute value of the terms of [A]. If [A] is complex, [B] contains the magnitude

of the terms of [A].

3. For fractional values of POWER and OPT = ’WHOLE’, all elements must be nonnegative. For OPT = ’COLUMN’ or ’SQUARE’ all diagonal elements must be nonnegative. 4. For whole number values of POWER, only real [A] matrices are allowed. The sign of the terms of [A] are properly preserved. 5. If an illegal operation is requested, a warning message is produced, and [B] is purged. 6. For OPT=’MAGCOL’, [B] is a real vector obtained by extracting the magnitude of the diagonal terms of [A] and raising them to the exponent POWER. For OPT=’MAGSQ’, [B] is a real diagonal matrix obtained by extracting the magnitude of the diagonal terms of [A] and raising them to the exponent POWER. If POWER=0, all nonzero diagonal terms of [A] produce unit terms in [B]. Zero terms in [A] produce zero terms in [B].

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Examples: 1. Extract the diagonal terms from LOO and KOO, form the ratio of factor diagonal to diagonal terms, and print terms less than 10-3. DIAGONAL DIAGONAL ADD MATMOD ADD MATGPR

LOO/LOOD/’COLUMN’/1. $ KOO/KOOD $ LOOD,KOOD/LOVERK///2 $ LOVERK,,,,/BIGLOVRK,/2////1.E-3 $ LOVERK,BIGLOVRK/DIFF//-1.0 $ BGPDT,USET,,DIFF//’H’/’O’ $

2. Obtain the absolute value of a matrix [A] DIAGONAL A/AA/’WHOLE’ $.

9.59 DISDCMP Performs distributed decomposition Performs distributed decomposition which includes the parallel elimination of boundary nodes and summation of global Schur complement

Format: DISDCMP

USET,SIL,EQEXIN,SCHUR,unused5,EQMAP/ LBB,DSFDSC,SCHURS/ HLPMETH/UNUSED2/UNUSED3/UNUSED4/UNUSED5/ UNUSED6/UNUSED7/UNUSED8/UNUSED9/UNUSED10/ UNUSED11/UNUSED12/UNUSED13/UNUSED14/UNUSED15 $

Input Data Blocks: USET

Degree-of-freedom set membership table

SIL

Scalar index list

EQEXIN

Equivalence between external and internal numbers

SCHUR

Local Schur complement matrix in sparse factor format

Unused5

Unused and can be purged

EQMAP

Table of degree-of-freedom global-to-local maps for domain decomposition

Output Data Blocks: LBB

Distributed boundary matrix factor in sparse factor format (contains the local panels of the fronts).

DSFDSC

Distributed boundary matrix factor.

SCHURS

Sum of all SCHUR matrices from all processors.

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Parameters: HLPMETH

Input-integer-default=1. Processing option. >0

Summation ONLY.

=0

Complete boundary decomposition (default).

Unused2

Input-integer-default=0. Unused and can be left unspecified.

Unused3

Input-integer-default=0. Unused and can be left unspecified.

Unused4

Input-real-default=1.E5. Unused and can be left unspecified.

Unused5

Input-character-default=‘H’ Unused and can be left unspecified.

Unused6

Input-real-default=0.0. Unused and can be left unspecified.

Unused7

Input-integer-default=-1. Unused and can be left unspecified.

Unused8

Input-integer-default=-1. Unused and can be left unspecified.

Unused9

Input-integer-default=-6. Unused and can be left unspecified.

Unused10

Input-real double precision-default=0.D0. Unused and can be left unspecified.

Unused11

Output-complex-default=(0.0,0.0). Unused and can be left unspecified.

Unused12

Input-integer-default=0. Unused and can be left unspecified.

Unused13

Input-integer-default=0. Unused and can be left unspecified.

Unused14

Input-integer-default=0. Unused and can be left unspecified.

Unused15

Input-integer-default=-1. Unused and can be left unspecified.

9.60 DISFBS Performs distributed forward-backward substitution

Format: DISFBS

LBB,DSFDSC,EQMAP,UABAR/ UA,PABAR,LOO/ HLPMETH $

Input Data Blocks: LBB

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DSFDSC

Table description of boundary sparse factor matrix

EQMAP

Table of degree-of-freedom global-to-local maps for domain decomposition

UABAR

Local updated rectangular ("loads") matrix

Output Data Blocks: UA

Global boundary solution for distributed decomposition

PABAR

Summed up updated rectangular ("loads") matrix for distributed decomposition

LOO

Merged boundary sparse factor matrix for distributed decomposition

Parameters: HLPMETH

Input-integer-default=0. Processing option. >0

Summation only

0

Complete distributed forward-backward substitution (default)

4

Summation operation and merging of distributed sparse boundary factor matrix

Remarks: LBB and DSFDSC can be purged.

9.61 DISOFPM Collects and merges OFP data blocks Collects and merges OFP data blocks from the slave processors to the master processor.

Format: DISOFPM

OFP1,OFP2,OFP3,OFP4,OFP5,OFP6,OFP7,OFP8/ OFP1M,OFP2M,OFP3M,OFP4M,OFP5M,OFP6M,OFP7M,OFP8M/ MAXBUFF $

Input Data Blocks: OFPi

OFP tables in SORT1 (or SORT2) format

Output Data Blocks: OFPiM

Merged OFP tables in SORT1 (or SORT2) format

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Parameters: MAXBUFF

Input-integer-default=250000. Maximum buffer size in words given to each processor for the merging process.

Remarks: 1. For SORT1, OFPiM are merged according to normal OFP order of element type, subcase number, and element identification number. 2. The type and order of data blocks across all DISOFPM/DISOFPS calls must correspond; for example, if the element stress OFP data block appears in the first input of the second call to DISOFPS, the element stress data block must also appear in the first input and output of the second call to DISOFPM.

9.62 DISOFPS Send OFP data blocks Send OFP data blocks from the slave processors to the master processor.

Format: DISOFPS

OFP1,OFP2,OFP3,OFP4,OFP5,OFP6,OFP7,OFP8 $

Input Data Blocks: OFPi

OFP tables in SORT1 (or SORT2) format

Output Data Blocks: None.

Parameters: None.

Remarks: 1. OFPi can be purged. However if OFPi is not purged, the corresponding OFPiM cannot be purged on the DISOFPS and DISOFPM statements. 2. The type and order of data blocks across all DISOFPM/DISOFPS calls must correspond; for example, if the element stress OFP data block appears in the first input of the second call to DISOFPS, the element stress data block must also appear in the first input and output of the second call to DISOFPM.

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9.63 DISOPT Performs appropriate discrete optimization problems Performs the approximate discrete optimization problem using design variables, constraints, responses, and sensitivity information, Design of Experiments (DOE), conservative discrete design, rounding-up, and rounding-down approaches.

Format: DISOPT

XINIT,DESTAB,CONSBL*,DPLDXI*,XZ, DXDXI,DPLDXT*,DEQATN,DEQIND,DXDXIT, PLIST2*,OPTPRMG,R1VALRG,RSP2RG,R1TABRG, CNTABRG,DSCMG,DVPTAB*,PROPI*,CONS1T, OBJTBG,COORDO,CON,SHPVEC,DCLDXT, TABDEQ,EPTTAB*,DBMLIB,BCON0,BCONXI, BCONXT,DNODEL,RR2IDRG,RESP3RG,DISTAB/ XO,CVALO,R1VALO,R2VALO,PROPO, R3VALO/ OBJIN/S,N,OBJOUT/PROTYP/UNUSED4/UNUSED5/ UNUSED6/UNUSED7/UNUSED8/UNUSED9/UNUSED10/ UNUSED11/UNUSED12/UNUSED13 $

Input Data Blocks: XINIT

Matrix of initial values of the design variables

DESTAB

Table of design variable attributes

CONSBL*

Matrix family of constant property values

DPLDXI*

Matrix family of coefficients in the property to independent design variable relationship

XZ

Matrix containing the constant portion of the dependent to independent design variable linking relationship

DXDXI

Matrix relating linked and independent design variables

DPLDXT*

Matrix family of transpose of DPLDXI.

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

DXDXIT

Matrix transponse of DXDXI

PLIST2*

Table family of type two properties on DVPREL2 Bulk Data entries

OPTPRMG

Table of optimization parameters

R1VALRG

Matrix initial values of the retained first level responses

RSP2RG

Table of attributes of the retained second level responses

R1TABRG

Table of attributes of the retained first level responses

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CNTABRG

Table of retained constraint attributes

DSCMG

Unnormalized design sensitivity matrix

DVPTAB*

Table family of attributes of the designed properties by internal property identification number order

PROPI*

Matrix family of initial property values

CONS1T

Matrix transpose of relationship between dependent and independent design variables

OBJTBG

Design objective table. Objective attributes with retained response identification number.

COORDO

Updated (optimized) Table of designed coordinate values

CON

Matrix of constants that relates design variables and design coordinates.

SHPVEC

Matrix of basis vectors – coefficients relating designed grid coordinates and design variables

DCLDXT

Matrix of coefficients in the grid to independent design variable relationship

TABDEQ

Table of unique design variable identification numbers

EPTTAB*

Table family of designed property attributes

DBMLIB

Table of designed beam library data

BCON0

Table of constant terms in the beam section constraint relationship

BCONXI

Matrix relating beam library constraints to the independent design variables

BCONXT

Matrix transpose of BCONXI

DNODEL

Table of designed node list

RR2IDRG

Table of retained referenced type two response identification list

RESP3RG

Table of retained third level responses in RESP3 tabl

DISTAB

Table of discrete optimization value sets

Output Data Blocks: XO

Matrix of final (optimized) values of the design variables

CVALO

Matrix of final (optimized) constraint values

R1VALO

Matrix of final (optimized) values of the retained first level responses

R2VALO

Matrix of final (optimized) values of the second level responses

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PROPO

Matrix of final (optimized) property values

R3VALO

Matrix of final (optimized) values of the third level responses

Parameters: OBJIN

Input-real-no default. Initial objective value.

OBJOUT

Output-real-no default. Final objective value.

PROTYP

Input-integer-default=0. Designed property type code.

UNUSEDi

Input-integer-default=0. Unused.

Remarks: None.

9.64 DISUTIL Broadcast data blocks between slave and master processors Broadcast data blocks between master and slave processors for parallel processing. Additional processing can occur on the master processor.

Format: Format for DISMETH=1 or 2: DISUTIL

B,X,R,EQMAP/ EPSSE/ NSKIP/S,N,EPSI/1 or 2 $

Format for DISMETH=3 on master processor: DISUTIL

DB,,,////3 $

Format for DISMETH=3 on slave processor: DISUTIL

,,,,/DB///3 $

Format for DISMETH=4 or 5: DISUTIL

RESMAX,RESMAX0,CASECC,HEADCNTL////4 or 5 $

Format for DISMETH=6: DISUTIL

UG,SPCPART,,EQMAP/UGG///6 $

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Format for DISMETH=7: DISUTIL

PG,SPCPART,,EQMAP/PGG///7 $

Format for DISMETH=8 or 9 on master processor: DISUTIL

MATS,,,////-8, 8, or 9 $

Format for DISMETH=8 or 9 on slave processor: DISUTIL

MATS,,,////-8, 8, or 9 $

Input Data Blocks: B

Rectangular matrix which is the local load vector (with local values in local a-set)

X

Solution of the equation [A][X]=[B] which is the local solution matrix (with global values in local a-set)

R

Residual matrix which is local (with local or global values in local a-set)

EQMAP

Table of degree-of-freedom global-to-local maps for domain decomposition

DB

Any data block to be broadcast from the master to the slave processors

RESMAX

Resultant or maxima matrix

RESMAX0

Resultant or maxima matrix for residual structure

CASECC

Table of Case Control command images

HEADCNTL

List of integer codes for header print control

UG

Displacement matrix in g-set for the current processor (local)

SPCPART

Partitioning vector for domain decomposition

GEQMAP

Table of grid based local equation map indicating which grid resides on which processors/partitions for domain decomposition

MATS

Any matrix on slave processors

Output Data Blocks: EPSSE

Table of epsilon and external work

UGG

Displacement matrix in g-set for all processors (global)

PGG

Force matrix in g-set for all processors (global)

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DB

Any data block to be broadcast from the master to the slave processors

MATM

Any matrix on master processor

Parameters: NSKIP

Input-integer-default=1. Record number in CASECC corresponding to the first subcase of the current boundary condition.

EPSI

Output-integer-default=1. Static solution error ratio flag. Set to -1 if the error ratio is greater than 1.E-3.

DISMETH

Input-integer-default=1. Method. 1

Compute epsilons and external works assuming a-set components of RUF are local values (which occurs in a direct solution).

2

Compute epsilons and external works assuming a-set components of RUF are global values (which occurs in a in iterative solution).

3

Broadcast table or matrix from master to slaves.

4

Broadcast VECPLOT resultant output from slaves to master and combine on master.

5

Broadcast VECPLOT maxima output from slaves to master and combine on master.

6

Broadcast displacement matrices from slaves to master and merge into global displacement matrix on master.

7

Broadcast force matrices from slaves to master and add/merge into global force matrix on master.

8, -8

Broadcast any matrix from slaves to master and add all matrices on master. Siemens PLM Software recommends DISMETH=8 for dense matrices and -8 for sparse matrices.

9

Broadcast any matrix from slaves to master and append columnwise all matrices on master.

Remarks: 1. All executions of DISUTIL must be synchronized across all processors. 2. EPSSE can be purged. EPSSE contains: a. Sequential number of subcases b. Superelement (domain) identification number c. Epsilon error ratio

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d. Strain energy (external work) 3. RESMAX0 can be purged on the slave processors. 4. UGG cannot be purged on the master processors. 5. For DISMETH=8 or 9, MATS and MATM must be in machine precision.

9.65 DIVERG Performs aerostatic divergence analysis Performs aerostatic divergence analysis: determines physically meaningful complex eigenvalues and saves the eigenvectors that correspond to the divergence roots.

Format: DIVERG

CLAMA,DYNAMIC,CASEA,EDT,CPHL,LCPHL/ DIVDAT,DCPHL,DLCPHL/ IMACHNO/LPRINT $

Input Data Blocks: CLAMA

Table of Bulk Data entry images related to dynamics. Contains the EIGC Bulk Data entries.

DYNAMIC

Table of Bulk Data entry images related to dynamics. Contains the EIGC Bulk Data entries.

CASEA

A single record (subcase) of CASECC for aerodynamic analysis. Specifies the DIVERG and CMETHOD command set identification numbers.

EDT

Table of Bulk Data entry images related to aerostatic and divergence analysis.

CPHL

Complex eigenvector matrix in the l-set

LCPHL

Left-handed complex eigenvector matrix in the l-set

Output Data Blocks: DIVDAT

Table of divergence data.

DCPHL

Complex eigenvectors associated with the divergence eigenvalues extracted from the real part of eigenvectors associated with the divergence eigenvalues.

DLCPHL

Left-handed complex eigenvectors associated with the divergence eigenvalues extracted from the real part of left-handed eigenvectors associated with the divergence eigenvalues.

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Parameters: IMACHNO

Input-integer-no default. Mach number multiplied by 1000 and specified as an integer.

LPRINT

Input-logical-default=TRUE. Print flag for divergence analysis.

Remarks: Divergence eigenvalues are the eigenvalues with a purely imaginary part or with a negligible real part. Only the first NROOT number of divergence eigenvalues are extracted, where NROOT is specified by the DIVERG Bulk Data entry.

Example: Excerpt from subDMAP DIVERGRS: FILE DIVERG

DIVDTX=APPEND/PHIDRX=APPEND/PHIDLX=APPEND $ CLAMAD,DYNAMICS,CASEA,EDT,PHIR,PHIL/ DIVDAT,PHIDR,PHIDL/ IMACHNO/LPRINT $ OUTPUT DIVERGENCE RESULTS APPEND DIVDAT, /DIVDTX/2 $ APPEND DIVERGENCE INFORMATION APPEND PHIDR, /PHIDRX/2 $ APPEND RIGHT EIGENVECTORS APPEND PHIDL, /PHIDLX/2 $ APPEND LEFT EIGENVECTORS

9.66 DMIIN Inputs DMI entries to DMAP. Input matrices referenced on DMI Bulk Data entries.

Format: DMIIN

DMI,DMINDX/DMI1,DMI2,DMI3,DMI4,DMI5,DMI6,DMI7, DMI8,DMI9,DMI10/PARM1/PARM2/PARM3/PARM4/PARM5/ PARM6/PARM7/PARM8/PARM9/PARM10/NAME1/NAME2 $

Input Data Blocks: DMI

Table of all matrices specified on DMI Bulk Data entries.

DMINDX

Index into DMI.

Output Data Blocks: DMIi

Matrix data blocks with names that appear in field 2 of the DMI entries (for example, the DMI matrix called DMI1 is output on data block DMI1). See Remark 3.

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Parameters: PARMi

Output-logical-default = FALSE. If the i-th output data block is generated, PARMi=TRUE.

NAME1

Input-character-default = “ “. If NAME1 is specified, read the DMI matrix associated with NAME1 instead of the name DMI1.

NAME2

Input-character-default = “ “. If NAME2 is specified, read the DMI matrix associated with NAME2 instead of the name DMI2.

Remarks: 1. The input data blocks DMI and DMINDX are output from the preface module IFP. 2. Any output data block can be purged. 3. If the output data blocks are specified on a CALL statement and the DMIIN module is specified in the subDMAP referenced by the CALL statement, the data block name specified on the CALL statement must be the same as the name specified on the DMIIN module.

Example: Assume the Bulk Data contains three DMI matrices named A, B, and C. The following DMAP instruction creates the data blocks A and C. Matrix B is ignored. DMIIN

DMI,DMINDX/A,C,,,,,,,,/S,N,YESA/S,N,YESC $

9.67 DOM6 Calculates sensitivity of all retained constraints Calculates sensitivity of all retained constraints with respect to independent design variables.

Format: DOM6

XINIT,DPLDXI*,CONSBL*,R1VALRG,R2VALRG,DSCMG,RSP2RG, DEQATN,PLIST2*,DEQIND,DXDXIT,DCLDXT,COORD,DESTAB, dVPTAB*,TABDEQ,EPTTAB*,DBMLIB,DPLDXT*,DNODEL,RR2IDR, RSP3RG,R3VALRG/ DSCM2/ PROTYP/UNUSED2/UNUSED3/UNUSED4/UNUSED5/UNUSED6/ UNUSED7/UNUSED8/UNUSED9/UNUSED10/UNUSED11/UNUSED12 $

Input Data Blocks: XINIT

Matrix of initial values of the design variable

DPLDXI*

Family of matrices of coefficients in the property to independent design variable relationship

CONSBL*

Family of matrices of constant property values

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R1VALRG

Matrix of initial values of the retained first level responses

R2VALRG

Matrix of initial values of the retained second level responses

DSCMG

Unnormalized design sensitivity matrix

RSP2RG

Table of attributes of the retained second level responses

DEQATN

Table of DEQATN Bulk Data entry images.

PLIST2*

Family of tables of type two properties on DVPREL2 Bulk Data entries

DEQIND

Index table to DEQATN data block.

DXDXIT

Matrix of coefficients in the design variable linking relationship

DCLDXT

Matrix of coefficients in the grid to design variable relationship

COORD

Matrix of initial or final designed coordinate values, COORDO or COORDN

DESTAB

Table of design variable attributes

DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order

TABDEQ

Table of unique design variable identification numbers

EPTTAB*

Family of tables of designed property attributes

DBMLIB

Table of designed beam library data

DPLDXT*

Family of matrix transposes of DPLDXI

DNODEL

Table of designed and non-designed locations

RR2IDR

Table of retained referenced type two response identification list

RSP3RG

Table of attributes of the retained third level responses

R3VALRG

Matrix of initial values of the retained third level responses

Output Data Blocks: DSCM2

Normalized design sensitivity coefficient matrix

Parameters: PROTYP

Input-integer-default=0. Designed property type code. 1

DVPRELi entries exist

2

DVCRELi entries exist

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UNUSEDi

4

DVMRELi entries exist

>0

For combinations, add above values

Input-integer-default=0. Unused.

9.68 DOM9 Performs the approximate optimization problem Performs the approximate optimization problem using design variables, constraints, responses and sensitivity information.

Format: XINIT,DESTAB,CONSBL*,DPLDXI*,XZ, DXDXI,DPLDXT*,DEQATN,DEQIND,DXDXIT, PLIST2*,OPTPRMG,R1VALRG,RSP2RG,R1TABRG, CNTABRG,DSCMG,DVPTAB*,PROPI*,CONS1T, OBJTBG,COORDO,CON,SHPVEC,DCLDXT, TABDEQ,EPTTAB*,DBMLIB,BCON0,BCONXI, BCONXT,DNODEL,RR2IDR,RESP3RG,CVALRG/ XO,CVALO,R1VALO,R2VALO,PROPO,R3VALO/ OBJIN/S,N,OBJOUT/PROTYP/PROPTN/UNUSED1/ UNUSED2/UNUSED3/UNUSED4/UNUSED5/UNUSED6/ UNUSED7/UNUSED8/UNUSED9/UNUSED10 $

DOM9

Input Data Blocks: XINIT

Matrix of initial values of the design variable

DESTAB

Table of design variable attributes

CONSBL*

Family of matrices of constant property values

DPLDXI*

Family of matrices of coefficients in the property to independent design variable relationship.

XZ

Matrix containing the constant portion of the dependent to independent design variable linking relationship

DXDXI

Matrix relating linked and independent design variables

DPLDXT*

Family of matrix transposes of DPLDXI

DEQATN

Table of DEQATN Bulk Data entry images. Output by IFP.

DEQIND

Index table to DEQATN data block. Output by IFP.

DXDXIT

Matrix transpose of DXDXI

PLIST2*

Family of tables of type two properties on DVPREL2 Bulk Data entries

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OPTPRMG

Table of optimization parameters

R1VALRG

Matrix of initial values of the retained first level responses

RSP2RG

Table of attributes of the retained second level responses

R1TABRG

Table of attributes of the retained first level responses

CNTABRG

Table of retained constraint attributes

DSCMG

Unnormalized design sensitivity matrix

DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order

PROPI*

Family of matrices of initial property values

CONS1T

Matrix transpose of relationship between dependent and independent design variables

OBJTBG

Design objective table. Objective attributes with retained response identification number.

COORDO

Updated (optimized) table of designed coordinate values

CON

Matrix of constants that relates design variables and design coordinates

SHPVEC

Matrix of basis vectors – coefficients relating designed grid coordinates and design variables

DCLDXT

Matrix of coefficients in the grid to independent design variable relationship

TABDEQ

Table of unique design variable identification numbers.

EPTTAB*

Family of tables of designed property attributes

DBMLIB

Table of designed beam library data

BCON0

Table of constant terms in the beam section constraint relationship

BCONXI

Matrix relating beam library constraints to the independent design variables

BCONXT

Matrix transpose of BCONXI

DNODEL

Table of designed and non-designed locations

RR2IDR

Table of retained referenced type two response identification list

RESP3RG

Table of attributes of the retained third level responses

CVALRG

The global data block for retained constraint values.

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Output Data Blocks: XO

Matrix of final (optimized) values of the design variables

CVALO

Matrix of final (optimized) constraint values

R1VALO

Matrix of final (optimized) values of the retained first level responses

R2VALO

Matrix of final (optimized) values of the second level responses

PROPO

Matrix of final (optimized) property values

R3VALO

Matrix of final (optimized) values of the third level responses

Parameters: OBJIN

Input-real-no default. Initial objective value.

OBJOUT

Output-real-no default. Final objective value.

PROTYP

Input-integer-default=0. Designed property type code. 1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

>0

For combinations, add above values

PROPTN

Input-integer-default=0. In order to support a pre-Version 68 capability, if PROPTN=-1, an EPT data block which is based on the values and the property to design variable relations is produced.

UNUSEDi

Input-integer-default=0. Unused.

9.69 DOM10 Prints initial and final results for design optimization In design optimization, prints the initial and final results for the approximate optimization problem.

Format: DOM10

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DESTAB,XINIT,X0,CNTABRG,CVALRG,CVALO,DVPTAB*, PROPI*,PROPO*,R1TABRG,R1VALRG,R1VALO,RSP2RG, R2VALRG,R2VALO,OPTPRMG,OBJTBG,DRSTBLG,TOL1,FOL1, FRQRPRG,DBMLIB,BCON0,BCONXI,WMID,RSP3RG,R3VALRG, R3VALO,EDT// DESCYCLE/DESMAX/OBJIN/OBJOUT/EIGNFREQ/PROTYP/ RESTYP $

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

Input Data Blocks: DESTAB

Table of design variable attributes

XINIT

Matrix of initial values of the design variable

XO

Matrix of final (optimized) values of the design variables

CNTABRG

Table of retained constraint attributes

CVALRG

Matrix of initial constraint values

CVALO

Matrix of final (optimized) constraint values.

DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order

PROPI*

Family of matrices of initial property values

PROPO*

Family of matrices of final (optimized) property values

R1TABRG

Table of attributes of the retained first level responses

R1VALRG

Matrix of initial values of the retained first level responses

R1VALO

Matrix of final (optimized) values of the retained first level responses

RSP2RG

Table of attributes of the retained second level responses

R2VALRG

Matrix of initial values of the retained second level responses

R2VALO

Matrix of final values of the second level responses

OPTPRMG

Table of optimization parameters

OBJTBG

Design objective table. Objective attributes with retained response identification number.

DRSTBLG

Table containing the number of retained responses for each subcase for each of the response types

TOL1

Transient response time output list truncated by the OTIME Case Control command

FOL1

Frequency response frequency output list truncated by the OFREQ Case Control command

FRQRPRG

Table containing the number of first level retained responses per response type and per frequency or time step

DBMLIB

Table of designed beam library data

BCON0

Table of constant terms in the beam section constraint relationship

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BCONXI

Matrix relating beam library constraints to the independent design variables

WMID

Table of weight as a function of material identification number

RSP3RG

Table of attributes of the retained third level responses

R3VALRG

Matrix of initial values of the retained third level responses

R3VALO

Matrix of final values of the third level responses

EDT

Table of bulk data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

Output Data Blocks: None.

Parameters: DESCYCLE

Input-integer-default=0. Design cycle analysis counter or flag. -1

Initial execution of DOM10

-2

Final execution of DOM10

>0

Design cycle number

DESMAX

Input-integer-default=0. Maximum allowed design optimization iteration number.

OBJIN

Input-real-default=0.0. Initial objective value.

OBJOUT

Input-real-default=0.0. Final objective value.

EIGNFREQ

Input-integer-default=0. Eigenvalue/frequency response type flag.

PROTYP

RESTYP

9-128

1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

Input-integer-default=0. Designed property type code. 1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

>0

For combinations, add above values

Input-integer-default=0. Optimization results flag.

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

0

Approximate model

1

Exact analysis for fully stessed design optimization

Examples: Excerpt from subDMAP DESOPT for initial execution: DBVIEW TOLV=OLI WHERE (SOLAPP=‘MTRAN‘) $ DBVIEW FOLV=OLI WHERE (SOLAPP=‘MFREQ’OR SOLAPP=‘DFREQ‘) $ IF ( DESCYCLE=1 ) DOM10 DESTAB,XINIT,,CNTABRG, CVALRG, , DVPTAB,PROPI,,R1TABRG,R1VALRG,, RSP2RG,R2VALRG,,OPTPRMG,OBJTBG,DRSTBLG, TOLV,FOLV,FRQRPRG,DBMLIB,BCON0,BCONXI,WMIDG// -1/DESMAX/OBJIN//EIGNFREQ $

Excerpt from subDMAP DESOPT for intermediate executions: DOM10

DESTAB,XINIT,XO,CNTABRG, CVALRG, CVALO, DVPTAB,PROPI,PROPO,R1TABRG,R1VALRG,R1VALO, RSP2RG,R2VALRG,R2VALO,OPTPRMG,OBJTBG,DRSTBLG, TOLV,FOLV,FRQRPRG,DBMLIB,BCON0,BCONXI,WMIDG// DESCYCLE/DESMAX/OBJIN/OBJOUT/EIGENFREQ $

Excerpt from subDMAP EXITOPT for final execution: DBVIEW FOL1V=FOL1 WHERE(WILDCARD) $ DBVIEW TOL2V=TOL2 WHERE(WILDCARD) $ IF ( CNVFLG=2 OR DESCYCL1=DESMAX OR OPTEXIT=6 ) DOM10, DESTAB,XVAL,,CNTABRG, CVALRG, , DVPTAB,PROPI,,R1TABRG,R1VALRG,, RSP2RG,R2VALRG,,OPTPRMG,OBJTBG,DRSTBLG, TOL2V,FOL1V,FRQRPRG,DBMLIB,BCON0,BCONXI,WMIDG// -2/DESMAX/OBJIN//EIGNFREQ $

9.70 DOM11 Updates geometry and element properties in design optimization

Format: DOM11

EPT,EPTTAB*,PROPO*,XO,DESTAB,CSTM,BGPDT, DESGID,COORDO,CON,SHPVEC,GEOM1,GEOM2,MPT,DMATCK, DIT,MFRDEP/ EPTN,COORDN,GEOM1N,GEOM2N,MPTN,DITN/ DESCYCLE/PROTYP $

Input Data Blocks: EPT

Table of Bulk Data entry images related to element properties

EPTTAB*

Family of tables of designed property attributes

PROPO*

Family of matrices of final (optimized) property values

XO

Matrix of final (optimized) values of the design variables

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DESTAB

Table of design variable attributes

CSTM

Table of coordinate system transformation matrices

BGPDT

Basic grid point definition table

DESGID

Table of designed grid coordinate attributes

COORDO

Table of designed coordinate values

CON

Matrix of constants that relates design variables and design coordinates

SHPVEC

Matrix of basis vectors – coefficients relating designed grid coordinates and design variables

GEOM1

Table of Bulk Data entry images related to geometry

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

MPT

Table of Bulk Data entry images related to material properties

DMATCK

Table of designed material consistency check

DIT

Direct input tables containing also TABLEDi bulk data for use herein

MFRDEP

Table for frequency dependent properties that can be designed

Output Data Blocks: EPTN

Updated (optimized) EPT

COORDN

Updated (optimized) COORDO

GEOM1N

Updated (optimized) GEOM1

GEOM2N

Updated (optimized) GEOM2

MPTN

Updated (optimized) MPT

DITN

Direct input tables with modified TABLEDi for updated values of designed frequency dependent properties

Parameters: DESCYCLE

Input-integer-default=0. Design cycle analysis counter.

PROTYP

Input-integer-default=0. Designed property type code.

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DVPRELi entries exist

2

DVCRELi entries exist

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4

DVMRELi entries exist

>0

For combinations, add above values

Remarks: The DOM11 module performs the following functions: 1. Creates the COORDN data block at the beginning of each iteration and updates property and shape data blocks EPTN and GEOM1N at the end of each iteration. 2. Writes iteration information to the punch file. 3. Punches updated GRID and DESVAR entries.

Example: Excerpt from subDMAP PREDOM: DOM11 EPT,EPTTAB,PROPI,XINIT,DESTAB,,, DESGID,COORDO,CON,SHPVEC,,,,,,/ EPTNN,COORDN,JUNKL,,,/0/0 $

Initial: DOM11 EPT,EPTTAB,PROPI,XINIT,DESTAB,CSTM,BGPDT, DESGID,COORDO,CON,SHPVEC,,,,,,/ EPTNNX,COORDN,,,,/0 $

Final: DOM11 EPT,EPTTAB,PROPO,XO,DESTAB,CSTM,BGPDT, DESGID,COORDO,CON,SHPVEC,GEOM1,,,,,/ EPTN,COORDN,GEOM1N,,,/DESCYCLE $

9.71 DOM12 Performs soft and hard convergence checks in design optimization. Outputs updated optimization data into the punch file, and prints final optimization results.

Format: DOM12

XINIT,XO,CVAL,PROPI*,PROPO*,OPTPRM,HIS, DESTAB,GEOM1N,COORDO,EDOM,MTRAK,EPT,GEOM2,MPT, EPTTAB*,DVPTAB*,XVALP,GEOM1P, R1TABRG,R1VALRG,RSP2RG,R2VALRG,PCOMPT,OBJTBG, ALBULK,AMLIST,DIT/ HISADD,OPTNEW,DBCOPT,DESNEW/ DESCYCLE/OBJIN/OBJOUT/S,N,CNVFLG/CVTYP/OPTEXIT/ DESMAX/MDTRKFLG/DESPCH/DESPCH1/MODETRAK/ EIGNFREQ/DSAPRT/PROTYP/BADMESH/XYUNIT/FSDCYC $

Input Data Blocks: XINIT

Matrix of initial values of the design variables

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XO

Matrix of final (optimized) values of the design variables

CVAL

Matrix of constraint values, CVALO or CVALRG

PROPI*

Family of matrices of initial property values

PROPO*

Family of matrices of final (optimized) property values

OPTPRM

Table of optimization parameters

HIS

Table of design iteration history

DESTAB

Table of design variable attributes

GEOM1N

Updated (optimized) Table of Bulk Data entry images related to geometry

COORDO

Matrix of designed coordinate values

EDOM

Table of Bulk Data entries related to design sensitivity and optimization

MTRAK

Table of updated DRESP1 Bulk Data entry images corresponding to the new mode numbering

EPT

Table of Bulk Data entry images related to element properties

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

MPT

Table of Bulk Data entry images related to material properties

EPTTAB*

Family of tables of designed property attributes

DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order

XVALP

XVAL table from previous iteration

GEOM1P

GEOM1 table from previous design iteration

R1TABRG

Table of attributes of the retained first level responses

R1VALRG

Matrix of initial values of the retained first level responses

RSP2RG

Table of attributes of the retained second level responses

R2VALRG

Matrix of initial values of the retained second level responses

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry

OBJTBG

Overall (global) objective function data block

ALBULK

Family of data blocks for bulk files for the original analysis/design model as well as for all auxiliary models, if any

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AMLIST

List of auxiliary model identification numbers

DIT

Direct input tables containing also TABLEDi bulk data for use herein

Output Data Blocks: HISADD

Table of design iteration history for current design cycle

OPTNEW

Updated table of optimization parameters

DBCOPT

Design optimization history table for post-processing

DESNEW

Update table of design variable attributes

Parameters: DESCYCLE

Input-integer-default=0. Design cycle analysis counter.

OBJIN

Input-real-default=0.0. Initial objective value.

OBJOUT

Input-real-default=0.0. Final objective value.

CNVFLG

Output-integer-default=0. Design optimization convergence flag.

CVTYP

0

No convergence is achieved.

1

Soft convergence is achieved.

2

Hard convergence is achieved.

Input-integer-default=0. Type of convergence test. 1

Soft convergence is to be checked.

2

Hard convergence is to be checked.

3

Final iteration histories are to be printed.

OPTEXIT

Input-integer-default=0. Design optimization termination option. See OPTEXIT description in the NX Nastran Quick Reference Guide.

DESMAX

Input-integer-default=0. Maximum allowed design optimization iteration number.

MDTRKFLG

Input-integer-default=0. Mode tracking status flag. 0

Mode tracking was successful.

1

Mode tracking was unsuccessful.

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DESPCH

Input-integer-default=0. Punch control for updated DESVAR, DREPS1 and GRID Bulk Data entries. See DESPCH description in the NX Nastran Quick Reference Guide.

DESPCH1

Input-integer-default=6. Punch output type flag. 0

None

1

Designed analysis property entries.

2

All of the entries of the type as long as at least one property entry is designed for the type.

4

Design model entries.

0 For combinations, sum above values.

MODETRAK

EIGNFREQ

>0

Indicates large field format.

0

Mode tracking is requested.

Input-integer-default=0. Eigenvalue/frequency response type flag. 1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

DSAPRT

Input-logical-default=FALSE. DSAPRT Case Control command print flag.

PROTYP

Input-integer-default=0. Designed property type code. 1

DVPRELi entries exist.

2

DVCRELi entries exist.

4

DVMRELi entries exist.

>0

For combinations, add above values.

BADMESH

Input-logical-default=FALSE. Bad geometry was detected.

XYUNIT

Input-integer-default=0. Fortran unit number to which the DOM12.

FSDCYC

Input-logical-default=FALSE. Fully stressed design cycle flag. Set to TRUE if this is a fully stressed design cycle.

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Examples: 1. Excerpt from subDMAP DESOPT following hard convergence: DBVIEW XPREV=XINIT DBVIEW PROPPV=PROPI DBVIEW HISPV=HIS

(WHERE DESITER=DESCYCLP) $ (WHERE DESITER=DESCYCLP AND DPTYPE=*) $ (WHERE DESITER=DESCYCLP) $

DOM12 XPREV,XINIT,CVALRG,PROPPV,PROPIF,OPTPRMG, HISPV,DESTAB,,,EDOM,MTRAK,EPT,GEOM2,MPT, EPTTABF,DVPTABF,,,,,,,,,,,/ HISADD,NEWPRM,,NEWDES/ DESCYCLE/OBJPV/OBJIN/S,N,CNVFLG/2/OPTEXIT// MDTRKFLG/DESPCH/DESPCH1/MODETRAK/EIGNFREQ/ DSAPRT/PROTYP $ APPEND HISADD,/HISX/2 $ EQUIVX HISX/HIS/-1 $ DBSTATUS NEWPRM,NEWDES//S,N,NONEWP/S,N,NONEWD $ IF ( NONEWP>0 ) EQUIVX NEWPRM/OPTPRMG/-1 $ IF ( NONEWD>0 ) EQUIVX NEWDES/DESTAB/-1 $

2. Excerpt from subDMAP DESOPT following soft convergence: DBVIEW DBVIEW DBVIEW DBVIEW

PROPIF =PROPI PROPOF=PROPO EPTTABF =EPTTAB DVPTABF =DVPTAB

WHERE (DPTYPE=*) $ (WHERE DPTYPE = *) WHERE (DPTYPE=*) $ WHERE (DPTYPE=*) $

DOM12 XINIT,XO,CVALO,PROPIF,PROPOF,OPTPRMG,HIS,DESTAB, GEOM1N,COORDO,,,EPT,GEOM2,MPT,EPTTABF,DVPTABF,,,,,,,,,,,/ HISADD,NEWPRM,,NEWDES/ DESCYCLE/OBJIN/OBJOUT/S,N,CNVFLG/1/OPTEXIT// MDTRKFLG/DESPCH/DESPCH1/MODETRAK/EIGNFREQ//PROTYP $ APPEND HISADD,/HISX/2 $ EQUIVX HISX/HIS/-1 $

3. Excerpt from subDMAP EXITOPT for termination: IF ( CNVFLG>0 OR DESCYCL1=DESMAX OR OPTEXIT>3 OR DSPRINT OR DSUNFORM OR DSEXPORT OR MODETRAK>0 OR BADMESH ) DOM12, ,XVAL,,,PROPOF,,HIS,DESTAB,GEOM1,COORDO,EDOM,MTRAK, EPT,GEOM2,MPT,EPTTABF,DVPTABF,XVALP,GEOM1P,,,,,,,,,/ ,,DBCOPT,/ DESCYCL1///CNVFLG/3/OPTEXIT/DESMAX/MDTRKFLG/ DESPCH/DESPCH1/MODETRAK/EIGNFREQ/DSAPRT/PROTYP/ BADMESH/XYUNIT $

9.72 DOPFS Performs optimization of the fully stressed design

Format: DOPFS

R1TABRG,CNTABRG,DESELM,DVPTAB*,CVALRG, PROPI,OPTPRMG,DPLDXT*,CONSBL*,DESTAB, XINIT,DPLDXI*,PLIST2*,DEQIND,DEQATN, EPTTAB*,DBMLIB,XZ,DXDXI,DXDXIT/ XO,PROPO $

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Input Data Blocks: R1TABRG

Table of attributes of the retained first level (direct) responses

CNTABRG

Table of retained constraint attributes

DESELM

Table of designed elements

DVPTAB*

Table family of attributes of the designed properties by internal property identification number order

CVALRG

Matrix of initial constraint values

PROPI

Matrix of initial property values

OPTPRMG

Table of optimization parameters

DPLDXT*

Matrix family of transpose of DPLDXI

CONSBL*

Matrix family of constant property values

DESTAB

Table of design variable attributes

XINIT

Matrix of initial values of the design variables

DPLDXI*

Matrix family of coefficients in the property to independent design variable relationship

PLIST2*

Table family of type two properties on DVPREL2 Bulk Data entries

DEQIND

Index table to DEQATN data block

DEQATN

Table of DEQATN Bulk Data entry images

EPTTAB*

Table family of designed property attributes

DBMLIB

Table of designed beam library data

XZ

Matrix containing the constant portion of the dependent to independent design variable linking relationship

DXDXI

Matrix relating linked and independent design variables

DXDXIT

Matrix transpose of DXDXI.

Output Data Blocks: XO

Matrix of final (optimized) values of the design variables

PROPO

Matrix of final (optimized) property values

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Remarks: None.

9.73 DOPR1 Preprocesses design variables and designed property values

Format: DOPR1

EDOM,EPT,DEQATN,DEQIND,GEOM2,MPT,CASEXX,DIT/ DESTAB,XZ,DXDXI,DTB,DVPTAB*,EPTTAB*,CONSBL*, DPLDXI*,PLIST2*,XINIT,PROPI*,DSCREN,DTOS2J*, OPTPRM,CONS1T,DBMLIB,BCON0,BCONXI,DMATCK,DISTAB, CASETM,SPAN23,MFRDEP/ S,N,MODEPT/S,N,MODGEOM2/S,N,MODMPT/DPEPS/ S,N,PROTYP/S,N,DISVAR $

Input Data Blocks: EDOM

Table of Bulk Data entries related to design sensitivity and optimization.

EPT

Table of Bulk Data entry images related to element properties.

DEQATN

Table of DEQATN Bulk Data entry images.

DEQIND

Index table to DEQATN data block.

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points.

MPT

Table of Bulk Data entry images related to material properties.

CASEXX

The main case control data block.

DIT

Direct input tables containing also TABLEDi bulk data for use herein.

Output Data Blocks: DESTAB

Table of design variable attributes.

XZ

Matrix containing the constant portion of the dependent to independent design variable linking relationship.

DXDXI

Matrix relating linked and independent design variables.

DTB

Table of constants from the DTABLE Bulk Data entry.

DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order.

EPTTAB*

Family of tables of designed property attributes.

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CONSBL*

Family of matrices of constant property values.

DPLDXI*

Family of matrices of coefficients in the property to independent design variable relationship.

PLIST2*

Family of tables of type two properties on DVPREL2 Bulk Data entries.

XINIT

Matrix of initial values of the design variables.

PROPI*

Family of matrices of initial property values.

DSCREN

Table of constants from the DSCREEN Bulk Data entry.

DTOS2J*

Family of tables identifying independent design variables and property.

OPTPRM

Table of optimization parameters.

CONS1T

Matrix transpose of relationship between dependent and independent design variables.

DBMLIB

Table of designed beam library data.

BCON0

Table of constant terms in the beam section constraint relationship.

BCONXI

Matrix relating beam library constraints to the independent design variables.

DMATCK

Table of designed material consistency check.

DISTAB

Table of discrete optimization value sets.

CASETM

Superelement frequency set & dynamic load updated CASEXX data block.

SPAN23

Table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

MFRDEP

Table for frequency dependent properties that can be designed.

Parameters: MODEPT

Output-logical-default=FALSE. Analysis model element property modification flag. When the flag is set to TRUE, the design model overrides element properties in the analysis model.

MODGEOM2

Output-logical-default=FALSE. Analysis model connectivity modification flag. When the flag is set to TRUE,the design model overrides connectivity in the analysis model.

MODMPT

Output-logical-default=FALSE. Analysis model material property modification flag. When the flag is set to TRUE, the design model overrides material properties in the analysis model.

DPEPS

Input-real-default=1.0E-4. Tolerance for design model override of analysis model properties. See further description in the NX Nastran Quick Reference Guide.

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PROTYP

Input-integer-default=0. Designed property type code.

DISVAR

1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

>0

For combinations, add above values

Output-logical-default=FALSE. Discrete optimization variable flag. Set to TRUE if discrete optimization design variables are specified.

9.74 DOPR2 Preprocesses the shape design variables and the shape basis vectors

Format: DOPR2

EDOM,BGPDT,CSTM,BASVEC,DESTAB,DXDXI,XINIT, CASECC,AMLIST,DVIDS/ DESGID,COORDO,SHPVEC,DCLDXT,CON,DTOS4J,DESVCP, CASEP,DNODEL/ LUSET/NOUGD/PEXIST/DVGRDN $

Input Data Blocks: EDOM

Table of Bulk Data entries related to design sensitivity and optimization

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

BASVEC

Auxiliary displacement matrix

DESTAB

Table of design variable attributes

DXDXI

Matrix relating linked and independent design variables

XINIT

Matrix of initial values of the design variables

CASECC

Table of Case Control command images

AMLIST

List of auxiliary model identification numbers

DVIDS

List of shape variable identification numbers to be used for the boundary dvgrid option

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Output Data Blocks: DESGID

Table of designed grid coordinate attributes

COORDO

Matrix of initial designed coordinate values at the beginning of each design cycle

SHPVEC

Matrix of basis vectors – coefficients relating designed grid coordinates and design variables

DCLDXT

Matrix of coefficients in the grid to design variable relationship

CON

Matrix of constants that relates design variables and design coordinates

DTOS4J

Designed grid perturbation vector in basic coordinate system

DESVCP

Global shape basis vector matrix with incorporation of DLINK relations with extra columns for property/dummy variables

CASEP

Residual superelement Case Control table for plotting basis vectors

DNODEL

Table of designed and non-designed locations

Parameters: LUSET

Input-integer-default=0. The number of degrees-of-freedom in the g-set.

NOUGD

Input-integer-default=-1. Flag for external input of auxiliary model displacement matrix. If NOUGD>0, the matrix exists.

PEXIST

Input-logical-default=FALSE. Set to TRUE if p-elements are present.

DVGRDN

Input-character-default=‘NO’ Flag for skipping basis vector components associated with all GRIDNs in DESVCP. If DVGRDN=‘YES‘, components are skipped.

Remarks: 1. BASVEC can be DBLOCATE‘d or internally generated. 2. CON is an offset vector that ensures that the geometry at the beginning of a design cycle is the same as that in the analysis model. It is in the basic coordinate system.

Examples: Excerpt from subDMAP DESOPT: DOPR2 EDOM,BGPDT,CSTM,BASVEC,DESTAB,DXDXI,XINIT,CASEXX, AMLIST,DVIDS/ DESGID,COORDO,SHPVEC,DCLDXT,CON,DTOS4J,DESVCP,CASEP/ LUSET/NOUGD/PEXIST/DVGRDN $

Excerpt from subDMAP PREDOM: DOPR2

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CASEXX,,/ DESGID,COORDO,SHPVEC,DCLDXT,CON,DTOS4J,DESVCP,CASEP/ LUSET/NOUGD $

Excerpt from subDMAP SCSHBV: DOPR2 EDOMSX,BGPDTS,CSTMS,,DESTAB,DXDXI,XINIT,CASEXX,,/ DESGID,COORDO,SHPVEC,DCLDXT,CON,DTOS4J,DESVCPS,CASEP/ LUSETS/NOUGD/PEXIST/DVGRDN $

9.75 DOPR3 Preprocesses DCONSTR, DRESP1, DRESP2, and DRESP3 Bulk Data entries per analysis type and superelement. Creates tables related to the design objective and a Case Control table for recovering design responses.

Format: DOPR3

CASE,EDOMS,DTB,ECT,EPT,DESTAB,EDT,FRLF,DEQIND, DEQATN,DESGID,DVPTAB,VIEWTB,OINT,PELSET,DFRFNC, TSPAN23,DIT,EDOM/ OBJTAB,CONTAB,R1TAB,RESP12,RSP1CT,FRQRSP,CASEDS, OINTDS,PELSETDS,DESELM,RESP3,TNSPAN23,SPAN1RG, FRLTMP/ DMRESD/S,N,DESGLB/S,N,DESOBJ/S,N,R1CNT/S,N,R2CNT/ S,N,CNCNT/SOLAPP/SEID/S,N,EIGNFREQ/PROTYP/DSNOKD/ SHAPES/S,N,R3CNT/PRESENS3 $

Input Data Blocks: CASE

Table of Case Control commands for the current analysis type and superelement.

EDOMS

Table of Bulk Data entries related to design sensitivity and optimization for current superelement.

DTB

Table of constants from the DTABLE Bulk Data entry.

ECT

Element connectivity table.

EPT

Table of Bulk Data entry images related to element properties.

DESTAB

Table of design variable attributes.

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

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FRLF

Complex or real eigenvalue summary table, transient response time output list, or frequency response frequency output list. Output by FRLG, TRLG, CEAD, and READ. However, with Version 6.0, for frequency response, this is no longer the same as the previous OL data block, but is now the full data block for the frequency sets data for the current cycle, together with a header record listing the frequency sets.

DEQIND

Index table to DEQATN.

DEQATN

Table of DEQATN Bulk Data entry images.

DESGID

Table relating the designed grid coordinates and a reduced basis vector.

DVPTAB

Table of attributes of the designed properties by internal property identification number order. Output by DOPR1.

VIEWTB

View information table, contains the relationship between each p-element and its view-elements and view-grids.

OINT

P-element output control table. Contains OUTPUT Bulk Data entries. Output by IFP.

PELSET

P-element set table, contains SETS DEFINITIONS.

DFRFNC

Table of frequency functions records (see bulk data input DTI,DFRFNC).

TSPAN23

Temporary copy of SPAN23, the table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

DIT

Table of TABLEij Bulk Data entry images.

EDOM

Global table of Bulk Data entries related to design sensitivity and optimization.

Output Data Blocks: OBJTAB

Design objective table for a given analysis type and superelement. Objective attributes with retained response identification number.

CONTAB

Table of constraint attributes.

R1TAB

Table of first level (DRESP1 Bulk Data entry) attributes.

RESP12

Table of second level responses.

RSP1CT

Table of the count of type 1 responses per response type per subcase in R1TAB.

FRQRSP

Table of the count of type 1 frequency/time responses per response type per frequency or time step.

CASEDS

Case control table for the data recovery of design responses.

OINTDS

P-element output control table for constrained elements.

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PELSETDS

P-element set table for constrained elements.

DESELM

Table of designed elements.

RESP3

Table of third level responses.

TNSPAN23

DOPR3 module updated temporary copy of SPAN23, the table for DRSPAN related DRESP2 and DRESP3, and referenced DRESP1.

SPAN1RG

Global table of DRSPAN related DRESP1 information.

FRLTMP

A composite FRL data block containing only the relevant records from each FRL data block in multiple subcase, multiple frequency set, frequency response analysis, relevant when the PRESENS3 parameter is TRUE. (See the parameter list.)

Parameters: DMRESD

Input-integer-default=-1. Design model flag. If set to -1, the design model is limited to the residual structure.

DESGLB

Output-integer-default=0. DESGLB Case Control command set identification number.

DESOBJ

Output-integer-default=0. DESOBJ Case Control command set identification number.

R1CNT

Input/output-integer-default=0. Counter for type 1 responses in data block R1TAB.

R2CNT

Input/output-integer-default=0. Counter for type 2 responses in data block RESP12.

CNCNT

Input/output-integer-default=0. Counter for constraints in CONTAB.

SOLAPP

Input-character-no default. Design optimization analysis type.

SEID

Input-integer-default=-1. Superelement identification number.

EIGNFREQ

Output-integer-default=0. Eigenvalue/frequency response type flag.

PROTYP

1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

Input-integer-default=0. Designed property type code. 1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

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>0

For combinations, add above values

DSNOKD

Input-real-default=0.0. Scale factor on the differential stiffness matrix in buckling design sensitivity analysis. Usually specified as a user parameter.

SHAPES

Input-logical-no default. Shape optimization Bulk Data entry presence flag. Must be TRUE if DVGRID, DVSHAP, or DVBSHAP Bulk Data entries are present.

R3CNT

Input/output-integer-default=0. Counter for type 3 responses in the RESP3 table.

PRESENS3

Logical parameter that is TRUE when one or more of FREQ3, FREQ4, or FREQ5 types of bulk data exist.

Remarks: 1. DOPR3 must be executed in two nested DMAP loops based on every analysis type and superelement. See subDMAP PRESENS for an example. 2. R1CNT, R2CNT, and CNCNT are accumulations of the number of records in R1TAB, RESP12, and CONTAB.

9.76 DOPR4 Creates design sensitivity tables for property and/or shape variables

Format: DOPR4

DTOS2J*,DTOS4J,DESTAB/ TABDEQ,DTOS2K*,DTOS4K/ PROTYP $

Input Data Blocks: DTOS2J*

Family of tables identifying independent design variables and property

DTOS4J

Designed grid perturbation vector in basic coordinate system

DESTAB

Table of design variable attributes

Output Data Blocks: TABDEQ

Table of unique design variable identification numbers

DTOS2K*

Family of tables. These tables are the same as DTOS2J* except that the dvid in each entry refers to the position of an internal design variable ID in the first TABDEQ record.

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DTOS4K

Same as DTOS4J except that the ID in each five-word entry is the position of an internal design variable ID in the first TABDEQ record.

Parameters: PROTYP

Input-integer-default=0. Designed property type code. 1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

>0 For combinations, add above values

9.77 DOPR5 Updates design sensitivity tables

Format: DOPR5

XINIT,EPTTAB*,PROPI*,DESTAB,DTOS2K*,DTOS4K, TABDEQ,DELBSH,GEOM4,DESGID,DVPTAB*,DBMLIB/ DTOS2*,DTOS4,DELBSX,DBMLIBU/ STPSCL/S,N,RGSENS/PROTYP $

Input Data Blocks: XINIT

Matrix of initial values of the design variables

EPTTAB*

Family of tables of designed property attributes

PROPI*

Family of matrices of initial property values

DESTAB

Table of design variable attributes

DTOS2K*

Family of tables. These tables are the same as DTOS2J* except that the dvid in each entry refers to the position of an internal design variable ID in the first TABDEQ record.

DTOS4K

Same as DTOS4J except that the ID in each five-word entry is the position of an internal design variable ID in the first TABDEQ record.

TABDEQ

Table of unique design variable identification numbers

DELBSH

Matrix of finite difference shape step sizes

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

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DESGID

Table of designed grid coordinate attributes

DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order

DBMLIB

Table of designed beam library data

Output Data Blocks: DTOS2*

Family of tables which are the same as DTOS2K* except that the PREF in each entry is the product of a DPLDXI element and the corresponding design variable value.

DTOS4

Same as DTOS4K except that the last three words in each entry contain the product of those in DTOS4K and the shape step size.

DELBSX

Updated DELBSH, where the numerical zero terms are replaced by a prescribed small value.

DBMLIBU

Modified DBMLIB data block updated for current values of designed PBARL/PBEAML dimensions.

Parameters: STPSCL

Input-real-default=1.0. Shape step size scaling factor.

RGSENS

Output-logical-default=FALSE. Rigid element sensitivity flag.

PROTYP

Input-integer-default=1. Designed property type code. 1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

>0 For combinations, add above values

9.78 DOPR6 Generates tables relating to grid perturbations

Format: DOPR6

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DTOS4,GPECT,EQEXIN,DESGID,EST,GEOM4,MIDLIS/ DGTAB,ESTDVS,TABEVS/ RSONLY/RGSENS $

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Input Data Blocks: DTOS4

Table relating design variable to grid perturbation

GPECT

Grid point element connection table

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

DESGID

Table of designed grid coordinate attributes

EST

Element summary table

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

MIDLIS

Table of pairs of user-supplied material property identification numbers (MIDs) and internal baseline MIDs

Output Data Blocks: DGTAB

Table relating DTOS4 records and designed grid data

ESTDVS

EST with grid design variable perturbations

TABEVS

Cross reference table between ESTDVS records and element/ design variable identification numbers

Parameters: RSONLY

Input-logical-no default. Residual structure only flag. FALSE : Superelements are specified. TRUE : Superelements are not specified.

RGSENS

Input-logical-default=FALSE. Rigid element sensitivity flag.

Remarks: 1. DOPR6 prepares tables to generate new stiffness matrix, mass matrix, load vector, and so on, taking into account shape design variable perturbations, that is, K+DELTAK, M+DELTAM and so on. This is accomplished by generating an EST for all elements which are referred to by design variables. The generated EST is in the same ascending order as the original EST. TABEVS is a cross reference table between the generated EST (ESTDVS) and the original EID/design variables. 2. DOPR6 also retains those designed grids which are not associated with any structural elements but are referenced by a rigid element.

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9.79 DOPRAN Preprocess RMS responses in design optimization.

Format: DOPRAN

DYNAMIC,DIT,OL,R1TCSC,BGPDT,CASEMR/ RMSTAB,CFSAB,PPVR/ LUSET $

Input Data Blocks: DYNAMIC

Table of Bulk Data entry images related to dynamics, specifically RANDPS

DIT

Table of TABLEij Bulk Data entry images, specifically TABRND1

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list

R1TCSC

Table of first level (direct) (DRESP1 Bulk Data entry) attributes. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then R1TCSC is per such subcase batch.

BGPDT

Basic grid point definition table

CASEMR

Table of Case Control commands for the current analysis type and superelement. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then CASEMR is per such subcase batch.

Output Data Blocks: RMSTAB

Table of RMS responses

CFSAB

Matrix of spectral densities – weighting factors for RMS calculations

PPVR

Partitioning vector for random responses

Parameters: LUSET

Input-integer-default=-1. The number of degrees-of-freedom in the g-set.

Remarks: None.

9.80 DPD Creates tables from Bulk Data entry images specified for dynamic analysis

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Format: DPD

DYNAMIC,GPL,SIL,USET,{CASECC/SLT},PG,PKYG,PBYG,PMYG,YG,{SLT/UNUSED}/ GPLD,SILD,USETD,TFPOOL,DLT,PSDL,RCROSSL,NLFT,TRL, EED,EQDYN/LUSET/S,N,LUSETD/S,N,NOTFL/S,N,NODLT/ S,N,NOPSDL/DATAREC/ S,N,NONLFT/S,N,NOTRL/S,N,NOEED/UNUSED10/S,N,NOUE/ UNUSED12/SEID $

Input Data Blocks: DYNAMIC

Table of Bulk Data entry images related to dynamics

GPL

External grid/scalar point identification number list

SIL

Scalar index list

USET

Degree-of-freedom set membership table for g-set

{CASECC/SLT}

Table of case control command images when CASECC. Table of static loads when SLT. (This legacy use will be modified in future versions by moving SLT completely to position 11 in the input data blocks list.)

PG

Static load matrix for the g-set

PKYG

Matrix of equivalent static loads due to enforced displacement for the g-set

PBYG

Matrix of equivalent static loads due to enforced velocity for the g-set

PMYG

Matrix of equivalent static loads due to enforced acceleration for the g-set

YG

Matrix of enforced displacements or temperatures for the g-set

{SLT/UNUSED} Table of static loads SLT when CASECC is used for the fifth data block. (The existing positions of CASECC, SLT, or lack thereof, in the various DPD call statements in the code are fixed, and may not be changed at user option.)

Output Data Blocks: GPLD

External grid/scalar/extra point identification number list. (GPL appended with extra point data.)

SILD

Scalar index list for p-set. (SIL appended with extra point data.)

USETD

Degree-of-freedom set membership table for p-set. (USET appended with extra point data.)

TFPOOL

Table of TF Bulk Data entry images

DLT

Table of dynamic loads

PSDL

Power spectral density list

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RCROSSL

Table of RCROSS Bulk Data entry images

NLFT

Nonlinear Forcing function table

TRL

Transient response list

EED

Table of eigenvalue extraction parameters

EQDYN

Equivalence table between external and internal grid/scalar/extra point identification numbers. (EQEXIN appended with extra point data.)

Parameters: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

LUSETD

Output-integer-no default. The number of degrees-of-freedom in the p-set.

NOTFL

Output-integer-no default. The number of transfer function Bulk Data entries. Set to -1 if no sets are defined.

NODLT

Output-integer-no default. Set to 1 if dynamics loads Bulk Data entries are processed, -1 otherwise. 1 also means that DLT is created.

NOPSDL

Output-integer-no default. Set to 1 if random analysis Bulk Data entries are processed, -1 otherwise. 1 also means that PSDL is created.

DATAREC

Input-integer-default=0. Data recovery flag. If DATAREC>0, DPD does not perform UFM 2071 checks for DELAY and DPHASE, which are not needed in data recovery.

UNUSED6

Input-integer-default=0. Unused.

NONLFT

Output-integer-no default. Set to 1 if nonlinear forcing function Bulk Data entries are processed, -1 otherwise. 1 also means that PSDL is created.

NOTRL

Output-integer-no default. Set to 1 if transient time step parameter Bulk Data entries are processed, -1 otherwise. 1 also means that TRL is created.

NOEED

Output-integer-no default. Set to 1 if eigenvalue extraction Bulk Data entries are processed, -1 otherwise. 1 also means that EED is created.

UNUSED10

Input-integer-no default. Unused.

NOUE

Output-integer-no default. Number of extra points. Set to -1 if there are no extra points.

UNUSED12

Input-integer-default=0. Unused.

SEID

Input-integer-default=0. Superelement identification number.

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Remarks: 1. DPD is the principal data processing module for dynamics analysis. New tables are assembled to account for any extra points in the model and the additional displacement sets used in dynamics. 2. DYNAMIC can be purged if TFPOOL, DLT, PSDL, NLFT, TRL, and EED are also purged. PG cannot be purged if static loads are referenced by dynamic loads via the LSEQ Bulk Data entry. 3. USET, SIL, GPL, GPLD, and SILD can be purged if USETD, DLT, and EED are purged.

9.81 DRMH1 Converts data recovery tables to matrices and associated directory tables Converts data recovery tables (for example, displacements, stresses, strains, forces, SPCforces, and MPCforces) to matrices and associated directory tables. Similar to the DRMS1 module.

Format: DRMH1

OFP1,OFP2,OFP3,OFP4/ TOFP1,MOFP1,TOFP2,MOFP2,TOFP3,MOFP3,TOFP4,MOFP4/ NCOL/NULLROW/TRL5T1/TRL5T2/TRL5T3/TRL5T4 $

Input Data Blocks: OFPi

Output table in SORT1 format usually created by the SDR2 module

Output Data Blocks: TOFPi

Directory table for MOFPi

MOFPi

Matrix form of the i-th output table

Parameters: NCOL

Input-integer-default=0. Number of columns (that is; subcases, modes, time steps or frequencies) desired in the output matrices. By default, all data records are converted into the output matrices. If NCOL is less than the number of data records in the input table, the first NCOL records are converted and the remaining records are ignored.

NULLROW

Input-integer-default=1. Flag to insert null rows in the output matrices for nonlinear quantities. See Remark 1. 0: Insert null rows. Compatible with DRMS1 output format 1: Do not insert null rows. Required for DRMH3 processing

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Output-integer-default=0. Specifies value for the fifth word in TOFPi‘s trailer.

Remarks: 1. DRMH1 is a similar to the DRMS1 module except that only the linear quantities (for example, axial stress) are output to the matrix. However, if NULLROW=0, null rows are inserted for the nonlinear quantities (for example, margin-of-safety). 2. DRMH1 converts tables with complex numbers to a matrix. However, the matrix contains complex numbers. As a result, only the item codes specified in the real side of the plot code tables are utilized. 3. The DRMH3 module performs the inverse operation: convert matrices into OFP tables

Example: In SOL 108, we want to double the stress output in the OES1 table. SOL 108 MALTER ’, ETC. DATA RECOVERY, SORT1’(,-1) DRMH1 OES1,,,/TES,MES,,,,,, $ ADD5 MES,,,,/MES2/2. $ DRMH3 TES,MES2,,,,,,,OL2,CASEDR/OES12,,,/APP1 $ OFP OES12/ $ CEND

9.82 DRMH2 Creates partitioning vector to properly align external superelement OTMs with system solution.

Format: DRMH2

BGPDTS,USET/PARTV/S,N,NOPARTV $

Input Data Blocks: BGPDTS

Basic grid point definitions table for external superelement.

USET

DOF set definition table for external superelements.

Output Data Blocks: PARTV

Partitioning vector.

Parameters: NOPARTV

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Input-integer-no default. Partitioning vector existence flag. -1 = PARTV not created; external superelement OTMs are already correct 0 = PARTV created; external superelement OTMs need to be realigned

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Remarks: 1. All data blocks are required.

Example: Partition displacements OTM. DRMH2 BGPDTS,USET/PARTV/S,N,NOPARTV $ IF (NOPARTV>-1) THEN $ FILE MUG1X=APPEND $ PARTN MUG1,PARTV,/MUG1G,,MUG1S,/1 $ APPEND MUG1G,MUG1S/MUG1X $ ELSE $ EQUIVX MUG1/MUG1X/ALWAYS $ ENDIF $

In the example, MUG1X is then used in the call to DRMH3.

9.83 DRMH3 Partitions tables for each superelement Converts data recovery matrices and associated directory tables (DRMH1 module outputs) to SORT1 formatted tables suitable for printing by the OFP module or processing by other modules; for example, DDRMM and SDR3.

Format: DRMH3

TOFP1,MOFP1,TOFP2,MOFP2,TOFP3,MOFP3,TOFP4,MOFP4, OL,CASECC/ OFP1,OFP2,OFP3,OFP4/ APP/DTM1/DTM2/DTM3/DTM4 $

Input Data Blocks: TOFPi

Directory table for MOFPi

MOFPi

Matrix form of the i-th output table

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list. Output by FRLG, TRLG, CEAD, and READ. May also be output by MODACC, if truncated via the OFREQ and OTIME Case Control commands.

CASECC

Table of Case Control command images

Output Data Blocks: OFPi

Output table in SORT1 format. Identical in format to data blocks created by the SDR2 module.

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Parameters: APP

Input-character-default=‘STATICS’ Analysis type. Allowable types are: ‘STATICS’ : statics ‘REIG’ : normal modes ‘CEIGEN’ : complex modes ‘FREQRESP’: frequency response ‘TRANRESP’: transient response

DTMi

Input-integer-default=0. Mode acceleration based displacement matrix flag. If DTMi0, MOPFi is a mode acceleration based displacement matrix and, therefore, velocities and accelerations are not output to OFPi. For APP=‘TRANRESP‘, MOFPi must have only one column per time step instead of the usual three.

Remarks: 1. If CASECC is purged, all input data blocks are converted. Otherwise, the inputs are converted based on the output commands specified in CASECC. 2. If the number of entries in a matrix does not match the associated table, the following occurs: If the number of rows (output quantities; for example, stresses) does not match, a warning message is printed with the identification of the matrix and table name. If the number of columns (for example, subcases or mode) does not match, a warning message is printed and the module continues. This allows you to combine modal results using any desired method into a single set of results (or more) and not be required to modify the table.

Example: See the “DRMH1” module description.

9.84 DRMS1 Data recovery by mode superposition, Phase 1 To compute output transformation matrices for displacements, SPC forces, stresses, and element forces. The input data blocks are the type generated by the SDR2 module and formatted for the OFP module.

Format: DRMS1

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OFP1,OFP2,OFP3,OFP4/ TOFP1,MOFP1,TOFP2,MOFP2,TOFP3,MOFP3,TOFP4,MOFP4/ NCOL $

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Input Data Blocks: OFPi

Output table in SORT1 format. Usually created by the SDR2 module.

Output Data Blocks: TOFPi

Directory table for MOFPi.

MOFPi

Matrix form of the i-th output table.

Parameters: NCOL

Input-integer-default=0. Number of columns (that is; subcases, modes, time steps or frequencies) desired in the output matrices. By default, all data records will be converted into the output matrices. If NCOL is less than the number of data records in the input table, the first NCOL records are converted and the remaining records are ignored.

Remarks: 1. SDR2 output data blocks (OFPi) are input data blocks for this module. Module DRMS1 generates the output transformation matrix (MOFPi) and associated directory table (TOFPi) from each of the input data blocks. 2. There are some data in OFPi for the output transformation that cannot be given linear combination operations, such as margins of safety and principal stresses. This irrelevant data is eliminated from the output transformation matrix. Components that are retained in the matrix MOFPi are indicated in the table of element stress output data description. 3. All the output transformation matrices have as many columns as the number of modes or loading conditions specified in PARAM, NCOL. Each column contains all the relevant components of GRIDs (T1, T2, and so on) or elements (sx, sy, and so on) for all the GRIDs or elements retained in the input data blocks. 4. Directory tables contain the mapping information as follows: •

RECORD 0 - Header record, indicating: – Type of data (Φ, q, s, or F) – Format code (real, real/imaginary or magnitude/phase)

•

RECORD 1 - Identification of the columns, providing: – Column numbers of the associated matrix – Natural frequencies (fn)

•

RECORD 2 - Identification of the rows, providing: – Type code of points or elements – Identification number of points or elements – Number of components of the point or element retained in the associated matrix – Starting row number of the point or element with reference to the associated matrix. See the OES, OEF, OUG, and OQG table descriptions in “+”.

•

Matrix trailer output, indicating the size of the associated matrix

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9.85 DSABO Incorporates element property design variable perturbations Incorporates element property design variable perturbations into tables required for stiffness, mass, damping, and load generation.

Format: DSABO

ECT,EPT,EST,DTOS2*,ETT,DIT,MPT,DMATCK,PCOMPT, DBMLIBU/ ESTDVP,MPTX,EPTX,TABEVP,MIDLIS,ESTDVM,PCOMPTX, FRQDPV/ S,N,PROPOPT/DELTAB/PROTYP/PEXIST $

Input Data Blocks: ECT

Element connectivity table

EPT

Table of Bulk Data entry images related to element properties

EST

Element summary table

DTOS2*

Family of tables. These tables are the same as DTOS2K* except that the PREF in each entry is the product of a DPLDXI element and the corresponding design variable value.

ETT

Element temperature table

DIT

Table of TABLEij Bulk Data entry images

MPT

Table of Bulk Data entry images related to material properties

DMATCK

Table of designed material consistency check

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry

DBMLIBU

Modified DBMLIB data block updated for current values of designed PBARL/PBEAML dimensions

Output Data Blocks: ESTDVP

EST with element property design variable perturbations

MPTX

MPT with design variable perturbations

EPTX

EPT with design variable perturbations

TABEVP

Cross-reference table between ESTDVP records and element and design variable identification numbers

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MIDLIS

Table of pairs of user-supplied material property identification numbers (MIDs) and internal baseline MIDs

ESTDVM

EST with updated material property identification numbers

PCOMPTX

PCOMPT with design variable perturbations

FRQDPV

Table of frequencies matching the perturbed elements summary table (ESTDV) when frequency dependent properties are designed

Parameters: PROPOPT

Output-integer-default=0. Property optimization flag. Set to 1 if element properties are defined as design variables.

DELTAB

Input-real-no default. Relative finite difference move parameter as specified on the DOPTPRM Bulk Data entry and stored in the OPTPRM data block.

PROTYP

Input-integer-default=0. Designed property type code.

PEXIST

1

DVPRELi entries exist

2

DVCRELi entries exist

4

DVMRELi entries exist

>0

For combinations, add above values

Input-logical-default=FALSE. P-element flag. Set to TRUE if p-elements are present.

Remarks: 1. The main purpose of module DSABO is to prepare tables that generate a new stiffness matrix, mass matrix, load vector, and so on, while taking into account the design variable perturbations, that is, K + DELTAK, M + DELTAM, and so on. These calculations are completed by generating an EST for all elements. These ESTs are referred to by the design variables and are in the same ascending order as the original EST. The EPT portion of the generated EST includes all the perturbations necessary to build K + DELTAK, M + DELTAM, and so on. EMG and SSG1 use ESTDV to generate K + DELTAK, M + DELTAM and P + DELTAP due to temperature effects. DSVG1 and DSVG2 then calculate DELTAK * u, DELTAP and so on. 2. If central difference is requested, DSABO must be executed for the backward tables. For example, in subDMAP PSLGDV, DSABO is used as follows: DSABO

ECTS,EPTS,EST,DTOS2,ETT,DIT,MPTS,,,/ ESTDVP,MPTX,EPTX,TABEVP,,,,/ S,N,PROPOPT/DELTAB $ IF ( CDIFX=‘YES’) THEN $ DELTABX=-DELTAB $ DSABO ECTS,EPTS,EST,DTOS2,ETT,DIT,MPTS,,,/ ESTDVPB,MPTXB,EPTX,TABEVP,,,,/ S,N,PROPOPT/DELTABX $

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ENDIF $ CDIFX=‘yes‘

9.86 DSAD Processes tables related to design sensitivity response evaluation, constraint screening and load case deletion.

Format: DSAD

RSPCSC,R1TCSC,R12CSC,OBJCSC,CONCSC, BLAMA,LAMA,CLAMA,DIVTAB,AUXTAB,STBTAB, FLUTAB,OUG1DS,OES1DS,OSTR1DS,OEF1DS, OEFITDS,OES1CDS,OSTR1CDS,OQG1DS,DSCREN, XINIT,COORDN,OL,FRQRSP,CASEER, CASERS,UGX,OPTPRM,DVPTAB*,PROPI*, BGPDT,DNODEL,WGTM,ONRGYDS, GLBTABDS,GLBRSPDS,R3CSC,RMSTAB,RMSVAL,SPAN1RG, OUGPSD1,DYNAMICS,SABFIL/ R1VAL,R2VAL,RSP2R,R2VALR,CVAL, CVALR,OBJTBR,CNTABR,R1TABR,R1VALR, DRSTBL,FRQRPR,UGX1,AUG1,R1MAPR, R2MAPR,CASDSN,CASDSX,DRDUG,DRDUTB, CASADJ,LCDVEC,RR2IDR,R3VAL,R3VALR,RESP3R,RMSTABR, RMSVALR,SPANSV,SPANSVG/ WGTS/VOLS/S,N,OBJVAL/S,N,NR1OFFST/S,N,NR2OFFST/ S,N,NCNOFFST/APP/DMRESD/SEID/DESITER/ EIGNFREQ/S,N,ADJFLG/PEXIST/MBCFLG/RGSENS/ PROTYP/AUTOADJ/FSDCYC/S,N,NR3OFFST/INREL $

Input Data Blocks: RSPCSC

Table of the count of type 1 responses per response type per subcase in R1TAB. Output by DOPR3. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then RSPCSC is per such subcase batch.

R1TCSC

Table of first level (DRESP1 Bulk Data entry) attributes. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then R1TCSC is per such subcase batch.

R12CSC

Table of second level responses. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then R12CSC is per such subcase batch.

OBJCSC

Design objective table for a given analysis type and superelement. Objective attributes with retained response identification number. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then OBJCSC is for the appropriate batch.

CONCSC

Table of constraint attributes. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then CONCSC is per such subcase batch.

BLAMA

Buckling eigenvalue summary table

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LAMA

Normal modes eigenvalue summary table

CLAMA

Complex eigenvalue summary table

DIVTAB

Table of aerostatic divergence data for all subcases

AUXTAB

Table of aerodynamic extra point identification numbers, displacements, labels, type, status, position and hinge moments for all subcases

STBTAB

Table of aerostatic stability derivatives for all subcases

FLUTAB

Flutter summary table for all subcases

OUG1DS

Table of displacements in SORT1 format for design responses

OES1DS

Table of element stresses in SORT1 format for design responses

OSTR1DS

Table of element strains in SORT1 format for design responses

OEF1DS

Table of element forces, excluding non-composite elements, in SORT1 format for design responses

OEFITDS

Table of composite element failure indices for design responses

OES1CDS

Table of composite element stresses in SORT1 format for design responses

OSTR1CDS

Table of composite element strains in SORT1 format for design responses.

OQG1DS

Table of single point forces-of-constraint in SORT1 format for design responses

DSCREN

Table of constants from the DSCREEN Bulk Data entry

XINIT

Matrix of initial values of the design variables

COORDN

Matrix of initial or final designed coordinate values

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list. Output by FRLG, TRLG, CEAD, and READ.

FRQRSP

Table of the count of type 1 frequency/time responses per response type per frequency or time step.

CASEER

Case Control table for the data recovery of design responses. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then CASEER is per such subcase batch.

CASERS

Case Control table for the data recovery of design responses

UGX

Matrix of analysis model displacements in g-set or p-set

OPTPRM

Table of optimization parameters

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DVPTAB*

Family of tables of attributes of the designed properties by internal property identification number order

PROPI*

Family of matrices of initial property values

BGPDT

Basic grid point definition table

DNODEL

Table of designed and non-designed locations

WGTM

Table of 6x6 rigid body mass matrix

ONRGYDS

Table of element strain energies in SORT1 format for design responses

GLBTABDS

Global results correlation table

GLBRSPDS

Global results matrix

R3CSC

Table of third level responses. When multiple batches of frequency response subcases with different boundary conditions and/or frequency sets exist, then R3CSC is per such subcase batch.

RMSTAB

Table of RMS responses

RMSVAL

Matrix of initial RMS values

SPAN1RG

Global table of DRSPAN related DRESP1 information.

OUGPSD1

Table of displacements in SORT1 format for the PSD function.

DYNAMICS

Table of bulk data entry images related to dynamics for the current superelement.

SABFIL

Table of SOL 200 related information regarding the RANDPS data, frequency responses, and load PSD values associated with constrained PSD responses.

Output Data Blocks: R1VAL

Matrix of initial values of the retained first level responses

R2VAL

Matrix of initial values of the retained second level responses

RSP2R

Table of retained second level responses in RESP12

R2VALR

Matrix of retained second level responses

CVAL

Matrix of constraint values

CVALR

Matrix of retained constraint values

OBJTBR

Table of design objective attributes with retained response identification number

CNTABR

Table of retained constraint attributes

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R1TABR

Table of retained first level (DRESP1 Bulk Data entry) attributes

R1VALR

Matrix of retained type one responses

DRSTBL

Table containing the number of retained responses for each subcase for each of the response types

FRQRPR

Table containing the number of first level retained responses per response type and per frequency or time step

UGX1

Copy of UGX matrix with null columns in place of the deleted responses

AUG1

Displacement matrix in g-set for aerostatic analysis

R1MAPR

Table of mapping from original first level retained responses

R2MAPR

Table of mapping from original second level retained responses

CASDSN

Case Control table with unneeded analysis subcase(s) deleted, excluding static aeroelastic subcases

CASDSX

Case Control table with unneeded analysis subcase deleted

DRDUG

Matrix of adjoint loads for the g-set

DRDUTB

Table of adjoint load attributes

CASADJ

Case Control table associated with adjoint method

LCDVEC

Partitioning vector for load case deletion. The row size is the same number of columns in UGX and ones for columns which are retained in UGX1. LCDVEC is intended for partitioning of analysis results related to inertia relief and SPCforces.

RR2IDR

Table of retained referenced type two response identification list

R3VAL

Matrix of initial values of the retained third level responses

R3VALR

Matrix of initial values of the retained third level responses

RESP3R

Table of retained third level responses in RESP3

RMSTABR

Table of retained RMS responses in RMSTAB

RMSVALR

Matrix of initial values of the retained RMS responses in RMSVAL

SPANSV

Relevant DRSPAN related internal DRESP1 IDs and their values for the current DSAD call.

SPANSVG

Global form of SPANSV, containing information from all DSAD calls in the analysis types loop.

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Parameters: WGTS

Input-real-default=0.0. Total weight of analysis model.

VOLS

Input-real-default=0.0. Total volume of analysis model.

OBJVAL

Output-real-default=0.0. Objective value.

NR1OFFST

Input/output-integer-default=0. Counter for retained type 1 responses. The value is initialized to 1 and is incremented by the number of records in R1TABR.

NR2OFFST

Input/output-integer-default=0. Counter for retained type 2 responses. The value is initialized to 1 and is incremented by the number of records in RSP2R.

NCNOFFST

Input/output-integer-default=0. Counter for retained constraints. The value is initialized to 1 and is incremented by the number of records in CNTABR.

APP

Input-character-default=’ ’ Analysis type. Allowable values are: ‘STATICS’: statics= ‘FREQRESP’: frequency response ‘TRANRESP’: transient respsonse

DMRESD

Input-integer-default=-1. Design model flag. If set to -1, the design model is limited to the residual structure.

SEID

Input-integer-default=0. Superelement identification number.

DESITER

Input-integer-default=0. Design optimization iteration number.

EIGNFREQ

Input-integer-default=0. Eigenvalue/frequency response type flag.

ADJFLG

1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

Output-integer-default=0. Adjoint sensitivity method flag. 0

No adjoint sensitivity

1

Adjoint sensitivity for static analysis

2

Adjoint sensitivity for frequency response analysis

PEXIST

Input-logical-default=FALSE. P-element existence flag. Set to TRUE if p-elements are present.

MBCFLG

Input-logical-default=FALSE. Multiple boundary condition in static analysis flag. Set to TRUE if multiple boundary conditions are specified in static analysis.

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RGSENS

Input-logical-default=FALSE. Rigid element sensitivity flag.

PROTYP

Input-integer-default=0. Designed property type code. 1

1: DVPRELi entries exist

2

2: DVCRELi entries exist

4

4: DVMRELi entries exist

>0

>0: For combinations, add above values

AUTOADJ

Input-character-no default. Adjoint sensitivity automatic selection flag. If set to ‘YES‘, adjoint sensitivity is automatically selected if appropiate. Usually input via user parameter.

FSDCYC

Input-logical-default=FALSE. Fully stressed design cycle flag. Set to TRUE if this is a fully stressed design cycle.

NR3OFFST

Input/output-integer-default=0. Counter for retained type 3 responses. The value is initialized to 1 and is incremented by the number of records in RESP3R.

INREL

Input/output-integer-default=0. Controls the calculation of inertia relief or enforced acceleration in SOLs 101, 105, and 200. See INREL parameter definition in the Quick Reference Guide for details.

Remarks: 1. DSAD first extracts the response quantities that are defined as type one responses in the design model. The type two responses are evaluated followed by the objective and any constraints associated with either response type. The constraints and corresponding responses are screened and load case deletion is performed. 2. DSAD is intended to be executed for each analysis type and superelement. Therefore many of the inputs, outputs, and data blocks are qualified by superelement and/or analysis type. See subDMAP DESCON for an example.

9.87 DSADJ Creates sensitivity of grid responses Creates sensitivity of grid responses with respect to design variables based on the combination of adjoint and analysis solution matrices and element sensitivity data. Applicable in frequency response or static analysis only.

Format: DSADJ

XDICTDS,XELMDS,BGPDT,CSTM,XDICTX,XELMX,UGX,ADJG, DRDUTB,DSPT1,FRQDPV/ ADELX/ NOK4GG/WTMASS/XTYPE/CDIF/COUPMASS/SHAPEOPT $

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Input Data Blocks: XDICTDS

Perturbed element matrix dictionary table

XELMDS

Table of perturbed element matrices

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

XDICTX

Baseline element matrix dictionary table or backward perturbed element matrix dictionary if CDIF=‘YES’

XELMX

Baseline element matrices or backward perturbed element matrices if CDIF=‘YES’

UGX

Matrix of analysis model displacements in g-set or p-set

ADJG

Adjoint sensitivity displacement matrix in the g-set or p-set

DRDUTB

Table of adjoint load attributes

DSPT1

Design sensitivity processing table

FRQDPV

Table of frequencies matching the perturbed elements summary table (ESTDV) when frequency dependent properties are designed

Output Data Blocks: ADELX

Matrix of adjoint sensitivities

Parameters: NOK4GG

Input-integer-default=-1. Structural damping generation flag. -1

Do not generate

0

Generate

WTMASS

Input-real-default=1.0. Specifies scale factor on structural mass matrix.

XTYPE

Input-integer-default=0. Type of element matrix data:

CDIF

0

Stiffness

1

Damping

2

Mass

Input-character-no default. Finite difference scheme. ‘YES’

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‘NO’ COUPMASS

SHAPEOPT

Forward

Input-integer-default=0. Coupled mass generation flag. -1

Lumped

0

Coupled

Input-integer-default=0. Shape optimization flag. Set to 1 if shape optimization is activated.

9.88 DSAE Merges tables to evaluate responses for the perturbed configuration Merges tables for the two sets of design variables in order to evaluate responses for the perturbed configuration for each load case and for each design variable.

Format: DSAE

ESTDVP,ESTDVS,TABEVP,TABEVS,TABDEQ/ ESTDV2,TABEV2 $

Input Data Blocks: ESTDVP

EST with element property design variable perturbations

ESTDVS

EST with grid design variable perturbations

TABEVP

Cross-reference table between ESTDVP records and element and design variable identification numbers

TABEVS

Cross reference table between ESTDVS records and element and design variable identification numbers

TABDEQ

Table of unique design variable identification numbers

Output Data Blocks: ESTDV2

Merged EST with grid and element property design variable perturbations

TABEV2

Merged cross reference table of TABEVP and TABEVS

Parameters: None.

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Remarks: 1. TABEV2 is in the ascending alphanumeric EST sort. IVEIDs are assigned to ensure that internal element IDs are unique and in ascending order. 2. For purposes of computational efficiency, the sizing design variables have been split into two sets. The first set consists of those design variables which affect the stiffness and mass matrices, for example, the cross-sectional area of a rod, thickness of a plate, and so on. The second set consists of those variables which can affect the responses, but have no effect on stiffness and mass matrices, for example, recovery points in a beam or plate. 3. If central difference is requested, DSAE must be executed for the backward tables. For example, in subDMAP PSLGDV, DSAE is used as follows: DSAE

ESTDVP,ESTDVS,TABEVP,TABEVS,TABDEQ/ ESTDV2F,TABEV2 $ IF ( CDIFX=‘YES’) DSAE, ESTDVPB,ESTDVS,TABEVP,TABEVS,TABDEQ/ ESTDV2B,TABEV2 $

9.89 DSAF Generates tables incorporating effect of retained first level responses Generates element summary and temperature tables that incorporate the effect of retained first level responses.

Format: DSAF

R1TABR,EST,ESTDV2,TABEV2,ETT,MIDLIS,KELM,KDICT, PTELEM,KELMDS,KDICTDS,PTELMDSX,ECT,VELEM,VELEMN/ ESTDCN,TABECN,ETTDCN,KELMDCN,KDICTDCN,PTELMDCN, VELEMDCN/ NDVTOT/PESE $

Input Data Blocks: R1TABR

Table of retained first level (DRESP1 Bulk Data entry) attributes

EST

Element summary table

ESTDV2

Merged element summary table with grid and element property design variable perturbations

TABEV2

Merged cross reference table of TABEVP and TABEVS

ETT

Element temperature table

MIDLIS

Table of pairs of user-supplied material property identification numbers (MIDs) and internal baseline MIDs

KELM

Table of element matrices for stiffness, heat conduction, differential stiffness, or follower stiffness

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KDICT

KELM dictionary table

PTELEM

Table of thermal loads in the elemental coordinate system

KELMDS

Table of perturbed element stiffness matrices. If CDIF=‘YES‘, this is the forward perturbed element matrix dictionary.

KDICTDS

Perturbed element stiffness matrix dictionary table. If CDIF=‘YES, this is the forward perturbed element matrix dictionary.

PTELMDSX

Table of thermal loads in the elemental coordinate system for the central, forward, or backward perturbed configuration.

ECT

Element connectivity table

VELEM

Table of element lengths, areas, and volumes

VELEMN

Table of element lengths, areas, and volumes for the perturbed configuration

Output Data Blocks: ESTDCN

Element summary table which incorporates combined constraints and design variables

TABECN

Table of relationship between internal identification numbers of constraints in ESTDCN and elements and responses in R1TABR

ETTDCN

Table of design variable and constraint internal identification numbers for the effects of temperature

KELMDCN

Table of element matrices for stiffness, heat conduction, differential stiffness, or follower stiffness which incorporates combined constraints and design variables

KDICTDCN

KELM dictionary table which incorporates combined constraints and design variables

PTELMDCN

Table of thermal loads in the elemental coordinate system which incorporates combined constraints and design variables

VELEMDCN

Table of element lengths, areas, and volumes which incorporates combined constraints and design variables

Parameters: NDVTOT

Input-integer-default=0. Number of unique referenced design variables.

PESE

Input-integer-default=0. Element strain energy flag for static analysis.

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9.90 DSAH Generates data blocks required for DSAL module Generates data blocks required for the DSAL module to compute sensitivities.

Format: DSAH

DRSTBL,R1TABR,CASDSN,TABECN,BLAMA*,LAMA*,OL,DIVTAB, FRQRPR,VIEWTBDS,CASERS,CSNMB,BUG*,PHG*,GEOM2,GEOM3, FRQRMF,DFFDNF,CASEFREQ/ DBUG,DPHG,CASEDSF,LBTAB,BDIAG,LFTAB,COGRID,COELEM, DSEDV,OINTDSF,PELSDSF,DGEOM2,DGEOM3/ APP/DMRESD/NDVTOT/ADJFLG/SEID/DSNOKD/S,N,NNDFRQ $

Input Data Blocks: DRSTBL

Table containing the number of retained responses for each subcase for each of the response types. Output by DSAD

R1TABR

Table of retained first level (DRESP1 Bulk Data entry) attributes

CASDSN

Case Control table with unneeded analysis subcase(s) deleted, excluding static aeroelastic subcase

TABECN

Table of relationship between internal identification numbers of constraints in ESTDCN and elements and responses in R1TABR

BLAMA*

Family of buckling eigenvalue summary tables

LAMA*

Family of normal modes eigenvalue summary tables

OL

Transient response time output list or frequency response frequency output list

DIVTAB

Table of aerostatic divergence data for all subcases

FRQRPR

Table containing the number of first level retained responses per response type and per frequency or time step

VIEWTBDS

View information table, contains the relationship between each p-element and its view-elements and view-grids for the perturbed model

CASERS

Case Control table for the residual structure and a given analysis type

CSNMB

Case Control table for a given superelement and all analysis types

BUG*

Family of buckling eigenvector matrices in the g-set

PHG*

Family of normal modes eigenvector matrices in the g-set

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

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GEOM3

Table of Bulk Data entry images related to static loads

FRQRMF

FRQRPR table for frequency response

DFFDNF

Table containing the derivatives of forcing frequencies with respect to natural frequencies

CASEFREQ

Case Control table for modal or direct frequency response analysis and based on ANALYSIS=MFREQ or DFREQ

Output Data Blocks: DBUG

Buckling eigenvector matrix in the g-set associated with designed (active) eigenvalues

DPHG

Normal modes eigenvector matrix in the g-set associated with designed (active) eigenvalues

CASEDSF

Case Control table for all load cases and all design variables for the perturbed configuration

LBTAB

Table of eigenvalues and generalized masses for retained buckling eigenvalue responses

BDIAG

Diagonal matrix of buckling divided by buckling generalized differential stiffness matrix

LFTAB

Table of eigenvalues and generalized masses for retained normal mode eigenvalue responses

COGRID

Correlation table between idcid/gid component for displacement responses

COELEM

Correlation table between idcid/eid/component for element responses

DSEDV

Partitioning vector for retained divergence responses

OINTDSF

P-element output control table for the perturbed configuration

PELSDSF

P-element set table for the perturbed configuration

DGEOM2

Table of Bulk Data entry images related to element connectivity and scalar points for the perturbed configuration

DGEOM3

Table of Bulk Data entry images related to static loads for the perturbed configuration

Parameters: APP

Input-character-default=’ ’ Analysis type. Allowable values are:

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STATICS’statics ‘FREQRESP’frequency response ‘TRANRESP’transient respsonse DMRESD

Input-integer-default=0. Design model flag. If set to -1, the design model is limited to the residual structure.

NDVTOT

Input-integer-default=0. Number of unique referenced design variables.

ADJFLG

Output-integer-default=-1. Adjoint sensitivity method flag. 0

No adjoint sensitivity

1

Adjoint sensitivity for static analysis

2

Adjoint sensitivity for frequency response analysis

SEID

Input-integer-default=0. Superelement identification number.

DSNOKD

Input-real-default=0.0. Scale factor on the differential stiffness matrix in buckling design sensitivity analysis. Usually specified as a user parameter.

NNDFRQ

Output-integer-default=0. Number of forcing frequencies which depend upon natural frequencies.

9.91 DSAJ Generates g-set size reduced basis vectors for each design variable Generates the g-set size reduced basis vectors for each design variable and the corresponding design variable correlation table.

Format: DSAJ

EDOM,EQEXIN,BGPDT,CSTM,SIL,BASVEC0,CASECC,GEOM4/ DESVEC,DVIDS,CASEP,DESVECP/ LUSET $

Input Data Blocks: EDOM

Table of Bulk Data entries related to design sensitivity and optimization

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

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SIL

Scalar index list

BASVEC0

Auxiliary displacement matrix. Optional user input.

CASECC

Table of Case Control command images

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

Output Data Blocks: DESVEC

Basis vector matrix which consists of basis vectors generated from DVGRID Bulk Data entries and from columns of BASVEC0 matrix. Its components are defined in the basic coordinate system.

DVIDS

List of shape variable identification numbers to be used for the boundary DVGRID option

CASEP

Case Control table with number of basis vectors in the DESVEC as the number of Case Control records

DESVECP

Basis vector matrix which consists of basis vectors generated from DVGRID bulk data entries and from columns of basvec matrix. Its components are expressed in the global coordinate system.

Parameter: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

9.92 DSAL Generates design sensitivity coefficient matrix Generates the design sensitivity coefficient matrix; for example, the sensitivity coefficients for the retained set of constraints specified in the design model for each design variable.

Format: DSAL

DRSTBL,DELWS,DELVS,DELB1,DELF1, COGRID,COELEM,OUGDSN,OESDSN,OSTRDSN, OEFDSN,OEFITDSN,OESCDSN,OSTRCDSN,R1VALR, OQGDSN,ONRGYDSN,TABDEQ,OL,DSDIV, DELX,DELS,DELFL,DELCE,FRQRPR,DELBSH, DRDUTB,ADELX,R1TABR,DRMSVL/ DSCM/NDVTOT/DELTAB/EIGNFREQ/ADJFLG/SEID $

Input Data Blocks: DRSTBL

Table containing the number of retained responses for each subcase for each of the response types

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DELWS

Matrix of delta weight for all design variables

DELVS

Matrix of delta volume for all design variables

DELB1

Matrix of delta buckling load factor for all design variables

DELF1

Matrix of delta eigenvalue for all design variables

COGRID

Correlation table between idcid/gid component for displacement responses

COELEM

Correlation table between idcid/eid/component for element responses

OUGDSN

Table of displacements in SORT1 format for design responses for the perturbed configuration

OESDSN

Table of element stresses in SORT1 format for the perturbed configuration

OSTRDSN

Table of element strains in SORT1 format for the perturbed configuration

OEFDSN

Table of element forces, excluding non-composite elements, in SORT1 format for the perturbed configuration

OEFITDSN

Table of composite element failure indices for the perturbed configuration

OESCDSN

Table of composite element stresses in SORT1 format for the perturbed configuration

OSTRCDSN

Table of composite element strains in SORT1 format for the perturbed configuration

R1VALR

Matrix of retained type one responses

OQGDSN

Table of single forces-of-constraint in SORT1 format for design responses for the perturbed configuration

ONRGYDSN

Table of element strain energies and energy densities in SORT1 format for design responses for the perturbed configuration

TABDEQ

Table of unique design variable identification numbers

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list

DSDIV

Matrix of delta divergence speed for all design variables

DELX

Matrix of delta trim variable responses for all design variables

DELS

Matrix of delta stability derivative responses for all design variables

DELFL

Matrix of delta flutter responses for all design variables

DELCE

Matrix of delta complex eigenvalue for all design variables

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FRQRPR

Table containing the number of first level retained responses per response type and per frequency or time step

DELBSH

Matrix of finite difference shape step sizes

DRDUTB

Table of adjoint load attributes

ADELX

Matrix of adjoint sensitivities

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attributes

DRMSVL

Table of the RMS response values with respect to the design variables

Output Data Blocks: DSCM

Design sensitivity coefficient matrix

Parameters: NDVTOT

Input-integer-no default. Number of unique referenced design variables.

DELTAB

Input-real-no default. Relative finite difference move parameter as specified on the DOPTPRM Bulk Data entry and stored in the OPTPRM data block.

EIGNFREQ

Input-integer-default=0. Eigenvalue/frequency response type flag.

ADJFLG

SEID

1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

Input-integer-default=0. Adjoint sensitivity method flag. 0

No adjoint sensitivity

1

Adjoint sensitivity for static analysis

2

Adjoint sensitivity for frequency response analysis

Input-integer-default=0. Superelement identification number.

Remarks: DSAL is intended to be executed for each analysis type and superelement. Hence, many of the inputs, outputs, and data blocks are qualified by superelement and/or analysis type. See subDMAP RESPSEN for an example.

9.93 DSAM Creates geometry for backward and forward (or central) perturbation

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Format: DSAM

DTOS4,DGTAB,BGPDT/ BGPDVP,BGPDVB/ S,N,SHAPEOPT/CDIF $

Input Data Blocks: DTOS4

Table relating design variable to grid perturbation. Same as DTOS4K except that the last three words in each entry contain the product of those in DTOS4K and the shape step size.

DGTAB

Table relating DTOS4 records and designed grid data. Correlation table of internal grid sequence for the baseline and perturbed configuration.

Output Data Blocks: BGPDVP

Basic grid point definition table for the forward (or central) perturbed configuration

BGPDVB

Basic grid point definition table for the backward perturbed configuration

Parameters: SHAPEOPT

Output-integer-default=0. Shape optimization flag. Set to 1 if shape design variables are defined.

CDIF

Input-character-no default. Finite difference scheme. ‘YES’

Central

‘NO’

Forward

9.94 DSAN Generates design sensitivity processing table Generates design sensitivity processing table and update element temperature table.

Format: DSAN

TABEV2,ETT/ DSPT1,ETTDV $

Input Data Blocks: TABEV2

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ETT

Element temperature table

Output Data Blocks: DSPT1

Design sensitivity processing table.

ETTDV

Element temperature table where the original element identification numbers have been converted to new design variable identification numbers

Parameters: None.

9.95 DSAP Computes an inertial or pseudo-load matrix Computes an inertial or pseudo-load matrix according to the following summation for frequency response and normal modes:

where:

or for complex eigenvalues:

where:

Format: DSAP

MUX,BUX,KUX,OL,DSPT1/ PX/ APP $

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Input Data Blocks: MUX

Matrix of mass multiplied by displacements or eigenvectors

BUX

Matrix of damping multiplied by displacement or eigenvectors

KUX

Matrix of stiffness multiplied by displacement or eigenvectors

OL

Complex or real eigenvalue summary table, or frequency response frequency output list

DSPT1

Design sensitivity processing table. See Remarks.

Output Data Block: PX

Inertial or pseudo-load matrix

Parameters: APP

Input-character-no default. Analysis type. Allowable values: ‘FREQ’Frequency response ‘CEIG’Complex eigenvalue ‘REIG’Normal modes

Remarks: 1. The number of rows PX is equal to the number of rows in the input matrices. The number of columns in PX is also equal to the number of columns in the input matrices unless DSPT1 is specified, in which case the number of columns is equal to the number of columns in the input matrices times the design variables defined in DSPT1. 2. If the number of columns in the MUX, BUX, and KUX is less than the number of frequencies in OL, PX is truncated accordingly. 3. Any of the inputs can be purged except OL. If DSPT1 is specified, APP can only be equal to ‘FREQ,’the summation is repeated for each design variable, and the result is called pseudo-loads. Also, the result is the negative of the equation above. 4. The input matrices can have any number of rows. For example, the number of rows can relate to a degree-of-freedom set.

9.96 DSAPRT Prints the normalized design sensitivity coefficient matrix Prints the normalized design sensitivity coefficient matrix according to the DSAPRT Case Control command request.

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Format: DSAPRT

CASECC,DESTAB,DSCMCOL,DSCM2,R1VALRG,R2VALRG,R3VALRG, DSIDLBL// DSZERO/EIGNFREQ/XYUNIT/DESCYCLE $

Input Data Blocks: CASECC

Table of Case Control command images

DESTAB

Table of design variable attributes

DSCMCOL

Correlation table for normalized design sensitivity coefficient matrix

DSCM2

Normalized design sensitivity coefficient matrix

R1VALRG

Matrix of initial values of the retained first level (direct) responses

R2VALRG

Matrix of initial values of the retained second level (synthetic) responses

R3VALRG

Matrix of initial values of the retained third level responses

DSIDLBL

Table of design response labels

Output Data Blocks: None.

Parameters: DSZERO

Input-real-default=0.0. Design sensitivity coefficient print threshold. If the absolute value of the coefficient is greater than DSZERO, the coefficient is printed.

EIGNFREQ

Input-integer-default=0. Eigenvalue/frequency response type flag. 1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

XYUNIT

Input-integer-default=0. Fortran unit number to which the DOM12 module writes design optimization x-y plot data.

DESCYCLE

Input-integer-default=0. Design cycle analysis counter.

9.97 DSAR Extracts and truncates data from the transient solution matrix Extracts and truncates the displacement, velocity, acceleration, and dynamic loads from the transient solution matrix into separate matrices.

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Format: DSAR

UXT,TOL,TOL1,PXT/ UDISP,UVELO,UACCE,UXT1,PXT1/ EXTRPL/NDEL $

Input Data Blocks: UXT

Solution matrix from transient response analysis

TOL

Transient response time output list consistent with columns in UXT and PXT

TOL1

Reduced transient response time output list. Subset of time steps in TOL and consistent with columns in outputs

PXT

Transient load matrix in the h-set (modal) or d-set for time steps in TOL

Output Data Blocks: UDISP

Reduced displacement solution matrix from transient response analysis

UVELO

Reduced velocity solution matrix from transient response analysis

UACCE

Reduced acceleration solution matrix from transient response analysis

UXT1

Reduced solution matrix from transient response analysis

PXT1

Reduced transient response load matrix in the h-set (modal) or d-set

Parameters: EXTRPL

NDEL

Input-integer-default=1. Extra solution column flag. An extra column is or is not appended to UDISP, UVELO, and UACCE accordingly: 0

Not appended

1

From the last time step

2

By extrapolation

Input-integer-default=3. If NDEL is -1, an unneeded load vector is deleted for the final time step for each design variable.

Remarks: 1. PXT, UXT1 and PXT1 can be purged. 2. If no truncation is desired, specify TOL for TOL1. For example: DSAR UXT,TOL,TOL,/ UDISP,UVELO,UACCE,,/0 $

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3. UXT and PXT can have any number of rows. For example, the number of rows can relate to a degree-of-freedom set. 4. All outputs have columns which are consistent with time steps in TOL1.

9.98 DSARLP Calculates pseudo-displacements for calculating sensitivities of stability derivatives Calculates the pseudo-displacements used in calculating the sensitivities of stability derivatives and determines the parameters required for all of the static aeroelastic sensitivity analyses.

Format: DSARLP

DRSTBL,R1TABR,AECTRL,CASECC,EDT/ CASEA,UXU,UXR/ S,N,STFLG/S,N,TFLG/S,N,SDFLG/S,N,NSKIP/ S,N,LPFLG/S,N,MACH/S,N,Q/S,N,AEQRATIO $

Input Data Blocks: DRSTBL

Table containing the number of retained responses for each subcase for each of the response types

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attribute.

AECTRL

Table of aerodynamic model‘s control definition

CASECC

Table of Case Control command images

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

Output Data Blocks: CASEA

A single record (subcase) of CASECC for aerodynamic analysis

UXU

Matrix of aerodynamic extra point vectors for use in calculating the sensitivity of unrestrained stability derivatives

UXR

Matrix of aerodynamic extra point vectors for use in calculating the sensitivity of restrained stability derivatives

Parameters: STFLG

Output-integer-no default. Flag to indicate whether the current subcase has active static response (DISP, STRAIN,STRESS, FORCE, CSTRAIN, CSTRESS, or CFORCE on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response.

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TFLG

Output-integer-no default. Flag to indicate whether the current subcase has active trim responses (TRIM on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response.

SDFLG

Output-integer-no default. Flag to indicate whether the current subcase has active stability derivative response (STABDER on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response.

NSKIP

Input/output-integer-no default. Trim subcase counter.

LPFLG

Input/output-integer-default=0. Flag to indicate whether there is another Case Control record to process. Set to -1 for the last subcase and Mach number.

MACH

Output-real-no default. Mach number.

Q

Output-real-no default. Dynamic pressure.

AEQRATIO

Output-real-no default. Aeroelastic feedback dynamic pressure ratio.

Remarks: DSARLP performs a function for static aeroelastic sensitivity analysis that is similar to the AELOOP module for static aeroelastic analysis.

9.99 DSARME Computes RMS values Computes the RMS values for random response analysis in design sensitivity.

Format: DSARME

UPDST,RMSTAB,CFSAB/ RMSVAL $

Input Data Blocks: UPDST

Table of transfer function data needed for RMS calculations

RMSTAB

Table of RMS responses

CFSAB

Matrix of spectral densities–weighting factors for RMS calculations

Output Data Blocks: RMSVAL

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Matrix of initial RMS values

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Parameters: None.

Remarks: None.

9.100 DSARMG Computes gradients of RMS values. Computes the gradients of the RMS values for random response analysis in design sensitivity.

Format: DSARMG

ADELU, DRDUTB, UPSDT, RMSTBR, CFSAB, RMSVLR/ DRMSVL

Input Data Blocks: ADELU

Matrix of basic response sensitivities from adjoint load method.

DRDUTB

Table of adjoint load attributes.

UPSDT

Table of transfer function data needed for RMS calculations.

RMSTBR

Table of retained RMS responses.

CFSAB

Matrix of spectral densities used as weighting factors for RMS.

RMSVLR

Matrix of retained RMS values.

Output Data Blocks: DRMSVL

Sensitivities of the RMS responses.

Remark: DSARMG combines appropriately the sensitivities for the DRESP1 type basic frequency responses, to arrive at the sensitivities for the RMS type responses.

9.101 DSARSN Calculates delta response values for trim variables and stability derivatives

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Format: DSARSN

CASEA,R1TABR,AECTRL,DUX,TR,AERO,DSTABU,DSTABR/ DELX1,DELS1/ TFLG/SDFLG/Q $

Input Data Blocks: CASEA

A single record (subcase) of CASECC for aerodynamic analysis

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attributes

AECTRL

Table of aerodynamic model‘s control definition

DUX

Matrix of aerodynamic extra point displacements for the perturbed configuration

TR

Matrix to transform forces from the support point to the aerodynamic reference point

AERO

Table of control information for aerodynamic analysis

DSTABU

Matrix of unrestrained perturbed dimensional stability derivatives

DSTABR

Matrix of restrained perturbed dimensional stability derivatives

Output Data Blocks: DELX1

Matrix of delta trim variable responses for all design variables for a single trim subcase

DELS1

Matrix of delta stability derivative responses for all design variables for a single trim subcase

Parameters: TFLG

Input-integer-no default. Flag to indicate whether the current subcase has active trim responses (TRIM on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response.

SDFLG

Input-integer-no default. Flag to indicate whether the current subcase has active stability derivative response (STABDER on the DRESP1 Bulk Data entry). 0 indicates no response, 1 indicates an active response.

Q

Input-real-no default. Dynamic pressure.

Remarks: DSARSN is called inside a loop for static aeroelastic sensitivity analysis whenever TFLG or SDFLG is greater than zero. See subDMAP SAERSENS for an example.

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9.102 DSAW Calculates delta-weight and/or delta-volume for each design variable

Format: DSAW

DRSTBL,TABEV2,VELEM,VELEMN,R1TABR/ DELVS,WTCRID,WTDSCP/ CFDFLG $

Input Data Blocks: DRSTBL

Table containing the number of retained responses for each subcase for each of the response types

TABEV2

Merged cross reference table of TABEVP and TABEVS

VELEM

Table of element lengths, areas, and volumes

VELEMN

Table of element lengths, areas, and volumes for the perturbed configuration

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attributes

Output Data Blocks: DELVS

Matrix of delta volume for all design variables

WTCRID

Table of retained weight responses with column and row numbers in rigid mass matrix

WTDSCP

Partitioning vector for weight

Parameter: CFDFLG

Input-integer-default=0. Central finite difference flag. 1 means forward and -1 backward.

9.103 DSDVRG Computes weighting factors to calculate retained divergence response sensitivities

Format: DSDVRG

DSEDV,DIVTAB,PHIDRLR,PHIDLLR,QLLX/ DELDV $

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Input Data Blocks: DSEDV

Partitioning vector for retained divergence responses

DIVTAB

Table of aerostatic divergence data for all subcases

PHIDRL

Retained right divergence eigenvector responses

PHIDLL

Retained left divergence eigenvector responses

QLL

Aerodynamic matrix for divergence analysis

Output Data Blocks: DELDV

Matrix of divergence sensitivity

Parameters: None.

9.104 DSFLTE Calculates right and left eigenvectors for a given eigenvalue Calculates the right and left eigenvectors for a given eigenvalue that has been extracted in a flutter analysis and has been flagged for sensitivity analysis. Selected complex scalar quantities required for flutter sensitivity analysis are also computed.

Format: DSFLTE

KHH,BHH,MHH,QHHL,FLUTAB,R1TABR,CASECC,CPHP,LCPHP/ CPHFL,CPHFR,VTQU/FCSENS $

Input Data Blocks: KHH

Generalized (modal) stiffness matrix

BHH

Generalized (modal) damping matrix

MHH

Generalized (modal) mass matrix

QHHL

Aerodynamic matrix list

FLUTAB

Flutter summary table for all subcases

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attributes

CASECC

Table of Case Control command images

CPHP

Complex eigenvector matrix in the p-set

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LCPHP

Left-handed complex eigenvector matrix in the p-set

Output Data Blocks: CPHFL

Left flutter eigenvector - h-set

CPHFR

Right flutter eigenvector - h-set

VTQU

Table of flutter sensitivity data

Parameters: FCSENS

Input-integer-default=1. Flutter/complex eigenvalue sensitivity flag. 1: Flutter sensitivity 2: Complex eigenvalue sensitivity

Remarks: The calculations in DSFLTE closely follow those used in module FA1 to perform the p-k method of flutter analysis.

9.105 DSFLTF Calculates sensitivity of active flutter responses Format: DSFLTF

VTQU,CDELK,CDELB,CDELM/DELFL/FCSENS $

Input Data Blocks: CDELK

Triple matrix product for flutter stiffness sensitivity

CDELB

Triple matrix product for flutter damping sensitivity

CDELM

Triple matrix product for flutter mass sensitivity

VTQU

Table of flutter sensitivity data

Output Data Block: DELFL

Matrix of delta flutter responses for all design variables

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Parameters: FCSENS

Input-integer-default=1. Flutter/complex eigenvalue sensitivity flag. 1: Flutter sensitivity 2: Complex eigenvalue sensitivity

9.106 DSMA Generates combined design sensitivity/constraint matrix Generates the combined design sensitivity/constraint matrix. Applicable to Old Design Sensitivity Analysis only.

Format: DSMA

DSPT2,OUG1DS,OES1DS,OEF1DS,OES1CDS,OEFITDS/ DSCMR,UNUSED2/ APP $

Format for statics: Format for normal modes: DSMA

DSPT2,DSEGM,,,,/ DSCMR,/ APP $

Input Data Blocks: DSPT2

Old design sensitivity processor table two

DSEGM

Old design sensitivity eigenvalue gradient matrix

OUG1DS

Table of displacements in SORT1 format for design responses

OES1DS

Table of element stresses in SORT1 format for design responses

OEF1DS

Table of element forces in SORT1 format for design responses

OES1CDS

Table of composite element stresses in SORT1 format for design responses

OEFITDS

Table of composite element failure indices for design responses

UNUSED2

Unused and can be purged

Output Data Blocks: DSCMR

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Old combined design sensitivity/constraint matrix

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Parameters: APP

Input-character-default=‘STATICS’ Analysis type. Allowable values are: ‘STATICS’: Statics ‘BUCKL’: Buckling ‘MODES’: Normal modes

Remarks: 1. DSMA is applicable only to old sensitivity analysis. 2. DSPT2 cannot be purged. 3. DSEGM must be present for normal modes or buckling. 4. OUG1DS, OES1DS, and OEF1DS are required only if selected by DSPT2 entries.

9.107 DSPRM Sets design sensitivity parameters Sets design sensitivity parameters based on retained responses for DMAP flow control.

Format: DSPRM

DRSTBL// S,N,WGTVOL/S,N,DOBUCK/S,N,DOMODES/S,N,DOSTAT/ S,N,FAILI/S,N,CSTRES/S,N,CSTRN/S,N,DOFREQ/ S,N,DOCEIG/S,N,DOMTRAN/S,N,DODIVG/S,N,DOSAERO/S,N, DOFLUT/ S,N,DOANALY/S,N,DOSASTAT/ADJFLGG/S,N,DOFSPCF/ S,N,DOTSPCF/S,N,DOWGHT/S,N,DOESE/S,N,DOSSPCF/ S,N,DORMS $

Input Data Block: DRSTBL

Table containing the number of retained responses for each subcase for each of the response types

Output Data Blocks: None.

Parameters: WGTVOL

Output-integer-default=0. Weight/volume retained response flag. Set to >0 if any retained response. 1

Weight only

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2

Volume only

3

Weight and volume

DOBUCK

Output-integer-default=0. Buckling constraint flag. Set to >0 if any constraint.

DOMODES

Output-integer-default=0. Normal modes constraint flag. Set to >0 if any constraint.

DOSTAT

Output-integer-default=0. Statics constraint flag. Set to >0 if any constraint.

FAILI

Output-integer-default=0. Composite failure index constraint flag. Set to >0 if any constraint.

CSTRES

Output-integer-default=0. Composite lamina stress constraint flag. Set to >0 if any constraint.

CSTRN

Output-integer-default=0. Composite lamina strain constraint flag. Set to >0 if any constraint.

DOFREQ

Output-integer-default=0. Frequency response retained response flag. Set to >0 if any retained response.

DOCEIG

Output-integer-default=0. Complex eigenvalue response retained response flag. Set to >0 if any retained response.

DOMTRAN

Output-integer-default=0. Transient response retained response flag. Set to >0 if any retained response.

DODIVG

Output-integer-default=0. Divergence analysis retained response flag. Set to >0 if any retained response.

DOSAERO

Output-integer-default=0. Aerostatic trim or stability derivative retained response flag. Set to >0 if any retained response.

DOFLUT

Output-integer-default=0. Flutter analysis retained response flag. Set to >0 if any retained response.

DOANALY

Output-integer-default=0. Any analysis retained response flag. Set to >0 if any retained response.

DOSASTAT

Output-integer-default=0. Statics or aerostatic retained response flag. Set to >0 if any retained response.

ADJFLG

Input-integer-default=0. Adjoint sensitivity flag.

DOFSPCF

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0

No adjoint sensitivity

1

Adjoint sensitivity for static analysis

2

Adjoint sensitivity for frequency response analysis

Output-integer-default=0. Frequency response retained SPCforce response flag. Set to >0 if any retained response.

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DOTSPCF

Output-integer-default=0. Transient response retained SPCforce response flag. Set to >0 if any retained response.

DOWGHT

Output-integer-default=0. Weight retained response flag. Set to >0 if any retained response.

DOESE

Output-integer-default=0. Static analysis retained element strain energy response flag. Set to >0 if any retained response.

DOSSPCF

Output-integer-default=0. Static analysis retained SPCforce response flag. Set to >0 if any retained response.

DORMS

Output-integer-default=0. RMS response retained response flag. Set to >0 if any retained response.

Remarks: RSP1CT can be specified as input to DSPRM.

9.108 DSTA Creates tables for legacy Design Sensitivity Analysis only. Creates tables related to the design perturbation in legacy Design Sensitivity Analysis only.

Format: DSTA

ECT,EPT,EST,CASECC,EDOM,{UG or LAMA or BLAMA}, CASECCX,ETT,DIT,MPT/ ESTDVP,ESTDCN,CASEDS,ETTDCN,DSPT1,DSPT2, DSROWL,DSCOLL,ETTDV,MPTC,EPTC/ APP/S,N,NOPRT/S,N,NOSAVE/S,N,NOFORT/NEIG $

Input Data Blocks: ECT

Element connectivity table

EPT

Table of Bulk Data entry images related to element properties

EST

Element summary table

CASECC

Table of Case Control command images. of static loads

EDOM

Table of Bulk Data entries related to design sensitivity and optimization

UG

Displacement matrix in g-set from static analysis

LAMA

Normal modes eigenvalue summary table

BLAMA

Buckling eigenvalue summary table

CASECCX

Table of Case Control command images used to generate static loads

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ETT

Element temperature table

DIT

Table of TABLEij Bulk Data entry images

MPT

Table of Bulk Data entry images related to material properties

Output Data Blocks: ESTDVP

EST with element property design variable perturbations

ESTDCN

Element summary table which incorporates combined constraints and design variables

CASEDS

Case control table for the data recovery of design responses

DSESM

Design sensitivity eigenvector selection matrix – Boolean operator to select eigenvectors which are referenced by constraints (buckling and normal modes only).

ETTDCN

Table of design variable and constraint internal identification numbers for the effects of temperature

DSPT1

Design sensitivity processing table

DSPT2

Old Design sensitivity processor table two

DSROWL

Table of design sensitivity row labels for design sensitivity matrix, DSCMR

DSCOLL

Table of design sensitivity column labels for design sensitivity matrix, DSCMR

ETTDV

Element temperature table where the original element identification numbers have been converted to new design variable identification numbers.

MPTC

Copy of MPT except MAT8 records are replaced by equivalent MAT2 records

EPTC

Copy of EPT except PCOMP records are replaced by equivalent PSHELL records

Parameters: APP

Input-character-default=‘STATICS’ Analysis type. Allowable values are: ‘STATICS’: statics ‘BUCKL’: buckling ‘MODES’: normal modes

NOPRT

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Output-integer-default=0. Print flag. Set to 1 if PRINT is requested on the legacy SENSITY Case Control command.

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NOSAVE

Output-integer-default=-1. Data base store flag. Set to 0 if SAVE is requested on the legacy SENSITY Case Control command.

NOFORT

Output-integer-default=-1. OUTPUT4 flag. Set to 0 if FORT is requested on the legacy SENSITY Case Control command.

NEIG

Input-integer-default=0. Number of eigenvalues to keep. 0

Keep all eigenvalues

>0

Keep first NEIG-th eigenvalues

Remarks: 1. ETT, ETTDV, and ETTDC can be purged if no element temperature data exists. 2. DSTA generates the tables necessary to drive other modules that calculate design sensitivity data. These modules include EMG, SSG1, DSVG1, DSVG2, DSVG3, SDR2, DSMAS and LMATPRT.

9.109 DSTAP2 Creates correlation table for normalized design sensitivity coefficient matrix

Format: DSTAP2

R1TABRG,RSP2RG,RSP3RG/ DSCMCOL,DSIDLBL/ UNUSED1/UNUSED2/UNUSED3 $

Input Data Blocks: R1TABRG

Table of attributes of the retained first level (direct) responses

RSP2RG

Table of attributes of the retained second level (synthetic) responses

RSP3RG

Table of attributes of the retained third level responses

Output Data Blocks: DSCMCOL

Correlation table for normalized design sensitivity coefficient matrix

DSIDLBL

Table of design response labels

Parameters: UNUSEDi

Input-integer-default=0. Unused.

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9.110 DSVG1 Creates pseudo loads or scalar terms required in sensitivity analysis

Format: XDICTDS,XELMDS,BGPDT,SIL,CSTM,XDICT,XELM, {UGX or AGX},VG,LAMA,DSPT1,FRQDPV,FRQRPR/ EGX/ NOK4GG/WTMASS/IAPP/DSVGSF/NOPSLG $

DSVG1

Input Data Blocks: XDICTDS

Perturbed element matrix dictionary table. If CDIF=‘YES’, this is the forward or backward perturbed element matrix dictionary.

XELMDS

Table of perturbed element matrices. If CDIF=‘YES’, this is the forward or backward perturbed element matrices.

BGPDT

Basic grid point definition table

SIL

Scalar index list

CSTM

Table of coordinate system transformation matrices

XDICT

Baseline element matrix dictionary table

XELM

Baseline element matrices

UGX

Displacement matrix in g-set. For transient response analysis, UGX can also represent velocity or acceleration.

AGX

Gravity/thermal load matrix due to volumetric changes for the central, forward, or backward perturbed configuration

VG

Left-handed displacement matrix in g-set. Divergence and flutter analysis only.

LAMA

Normal modes or buckling eigenvalue summary table

DSPT1

Design sensitivity processing table

FRQDPV

Table of frequencies matching the perturbed elements summary table (ESTDV) when frequency dependent properties are designed

FRQRPR

Table containing the number of first level retained (DRESP1) responses per response type and per frequency or time step

Output Data Blocks: EGX

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Pseudo-load (equilibrium variation) matrix in the g-set

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Parameters: NOK4GG

Input-integer-default=-1. Structural damping generation flag. -1 Do not generate 0

Generate

WTMASS

Input-real-default=1.0. Specifies scale factor on structural mass matrix.

IAPP

Input-integer-default=1. Analysis type. Allowable values are:

DSVGF

NOPSLG

1

Statics, aerostatic, frequency, or transient response

2

Buckling or normal modes

4

Flutter or divergence

Input-integer-default=0. Specifies scaling of solution vector by eigenvalue. 0

No scaling

1

Scale

Input-integer-default=0. Pseudo-load generation flag. Set to -1 if no load generation is requested for the current superelement based on the SEDV Case Control command.

Remarks: 1. DSVG1 must be executed for mass, stiffness, viscous damping, and structural damping and, if CDIF=‘YES‘, forward and backward perturbed configurations. 2. For transient analysis, DSVG1 must be invoked three times for displacement, velocity, and acceleration which are obtained from the DSAR module. 3. If NOPSLG ≠ 0, a null EGX matrix is generated.

9.111 DSVG1P Creates pseudo loads or scalar terms for p-elements in design sensitivity analysis

Format: DSVG1P

ESTDVM,ESTDV2,BGPDVP,CSTM,MPTX,DIT,DEQATN,DEQIND, UGX,LFTAB,DSPT1,GPSNT,ESTDVB/ EGK,EGM/ COUPMASS/K6ROT/ALTSHAPE/WTMASS/NOPSLG/OPTFLG/ UNUSED7 $

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Input Data Blocks: ESTDVM

EST with updated material property identification numbers

ESTDV2

Merged EST with grid and element property design variable perturbations. If CDIF=‘YES,’this is the forward perturbation.

BGPDVP

Basic grid point definition table for the forward (or central) perturbed configuration

CSTM

Table of coordinate system transformation matrices

MPTX

MPT with design variable perturbations

DIT

Table of TABLEij Bulk Data entry images

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

UGX

Matrix of analysis model displacements in g-set or p-set

DSPT1

Design sensitivity processing table

LFTAB

Table of eigenvalues and generalized masses for retained normal mode eigenvalue responses

GPSNT

Grid point shell normal table

ESTDVB

Element summary table for the backward perturbed configuration. Required only if CDIF=‘YES’

Output Data Blocks: EGK

Pseudo-load (equilibrium variation) matrix in the g-set due to stiffness

EGM

Pseudo-load (equilibrium variation) matrix in the g-set due to mass

Parameters: COUPMASS

Input-integer-default=-1. Coupled mass generation flag. -1 Lumped 0

Coupled

K6ROT

Input-real-default=-1.0. Normal rotational stiffness factor for CQUAD4 and CTRIA3 elements.

ALTSHAPE

Input-integer-default=0. Specifies set of displacement functions in p-element analysis. ALTSHAPE=0 selects the MacNeal set and 1 selects the Full Product Space set.

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WTMASS

Input-real-default=-1.0. Specifies scale factor on structural mass matrix.

NOPSLG

Input-integer-default=0. Pseudo-load generation flag. Set to -1 if no load generation is requested for the current superelement based on the SEDV Case Control command.

OPTFLG

UNUSED7

Input-integer-default=0. DSVG1P application method: 1

Statics

2

Normal modes

3

Acceleration load

Input-integer-default=0. Unused.

Remarks: If NOPSLG ≠ 0, a null EGX matrix is generated.

9.112 DSVG2 Generates pseudo-load matrix for equilibrium changes in thermal load Generates the pseudo-load matrix which reflects equilibrium changes in the thermal load due to variations in the design variables.

Format: DSVG2

BGPDVX,CSTM,SIL,KDICTX,CASDSN,PTELEM, PTELMDSX,{UGX or AGX},DSPT1/ EGTX/ PEXIST/HPFLAG $

Input Data Blocks: BGPDVX

Basic grid point definition table for the central, forward, or backward perturbed configuration

CSTM

Table of coordinate system transformation matrices

SIL

Scalar index list

KDICTX

Baseline element stiffness matrix dictionary table for h-elements or p-elements

CASDSN

Case Control table with unneeded analysis subcase(s) deleted, excluding static aeroelastic subcases

PTELEM

Table of thermal loads in the elemental coordinate system

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PTELMDSX

Table of thermal loads in the elemental coordinate system for the central, forward, or backward perturbed configuration

UGX

Matrix of analysis model displacements in g-set or p-set

AGX

Gravity/thermal load matrix due to volumetric changes for the central, forward, or backward perturbed configuration

DSPT1

Design sensitivity processing table

Output Data Block: EGTX

Pseudo-load matrix (variation in equilibrium) due to changes in the thermal load/design variables for the central, forward, or backward perturbed configuration

Parameters: PEXIST

Input-logical-default=FALSE. Set to TRUE if p-elements are present.

HPFLAG

Input-integer-default=1. Element type processing flag. 1

h-element

2

p-element

Remarks: CSTM and BGPDT can be purged.

9.113 DSVG3 Combines and appends solution matrices for Old Design Sensitivity Analysis only Combines and appends the solution matrices from the analysis and pseudo-loads due to design variable changes in Old Design Sensitivity Analysis only.

Format: DSVG3

UG,UGDS/ UGDS1 $

Input Data Blocks: UG

Displacement matrix in g-set from the analysis

UGDS

Displacement matrix in g-set due to pseudo-loads

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Output Data Block: UGDS1

Displacement matrix in g-set for the total variation

Parameters: None.

9.114 DSVGP4 Generates a perturbed multipoint constraint transformation matrix Generates a perturbed multipoint constraint transformation matrix for rigid element shape sensitivity analysis.

Format: DSVGP4

DGTAB,EQEXIN,GEOM4,RMG,GM,USET,CSTM,BPGDVP/ DELTGM,DVSLIS/ LUSET/NDVTOT/S,N,RGSENS $

Input Data Blocks: DGTAB

Table relating DTOS4 records and designed grid data. Correlation table of internal grid sequence for the baseline and perturbed configuration.

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

RMG

Multipoint constraint equation matrix

GM

Multipoint constraint transformation matrix, m-set by n-set

USET

Degree-of-freedom set membership table for g-set

CSTM

Table of coordinate system transformation matrices

BGPDVP

Basic grid point definition table for the forward (or central) perturbed configuration

Output Data Blocks: DELTGM

Multipoint constraint transformation matrix for the perturbed configuration

DVSLIS

List of design variables affected by shape variations

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Parameters: LUSET

Input-integer-default=0. The number of degrees-of-freedom in the g-set.

NDVTOT

Input-integer-default=0. Number of unique referenced design variables.

RGSENS

Output-logical-default=FALSE. Rigid element sensitivity flag.

Remarks: Assume B is j rows by k columns. Then A must have NSMATS submatrices of size i rows by j columns (if T=0) and C must have i rows by k columns.

9.115 DSVGP5 Performs multiplication of two matrices Performs multiplication of two matrices with one matrix having multiple submatrices and, optionally, the addition of a third matrix to the product. For example, the default (IOPT=0 or T=0) result is: [ A1 * B | A2 * B | A3 * B | . . . An * B ] + [ C1 | C2 | C3 | . . . | Cn ]

Format: DSVGP5

A,B,C,DVSLIS/ D/ NSMATS/T/IOPT $

Input Data Blocks: A

Matrix with NSMATS number of submatrices

B

Submatrix multiplier

C

Additive matrix to be added to product of A and B. Used only if IOPT=0 or 2.

DVSLIS

List of design variables affected by shape variations

Output Data Block: D

Matrix product

Parameters: NSMATS

Input-integer-default=0. Number of submatrices in A.

T

Input-integer-default=0. Ai submatrix transpose flag. Applicable only when IOPT=0.

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IOPT

0

No transpose of Ai (default)

1

Transpose Ai

Input-integer-default=0. DSVGP5 method. T is ignored when IOPT>0. 0

Ai * B + Ci (default)

1

B * Ai

2

Same as 0 except diagonal is extracted from Ai * B + Ci and stored as a column in D.

Remarks: Assume B is j rows by k columns. Then A must have NSMATS submatrices of size i rows by j columns (if T=0) and C must have i rows by k columns.

9.116 DTIIN Input DTI entries to DMAP Input tables referenced on DTI Bulk Data entries.

Format: DTIIN

DTI,DTINDX/DTI1,DTI2,DTI3,DTI4,DTI5,DTI6,DTI7, DTI8,DTI9,DTI10/PARM1/PARM2/PARM3/PARM4/PARM5/ PARM6/PARM7/PARM8/PARM9/PARM10 $

Input Data Blocks: DTI

Collection of tables specified on DTI Bulk Data entries (from IFP)

DTlNDX

Index into DTI (from IFP)

Output Data Blocks: DTIi

Names that appear on field 2 of the DTI entries (that is, the DTI table called DTI1) is output on data block DTI1.

Parameters: PARMi

Output-logical-default = FALSE. If the i-th output data block is generated, PARMi=TRUE.

Remarks: 1. The input data blocks DTI and DTINDX are output from the preface module IFP.

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2. Any output data block can be purged.

Example: Assume the Bulk Data contains three DTI tables named T1, T2, and T3. The following DMAP instruction creates the data blocks T1 and T3. DTIIN

DTI,DTINDX/T1,T3,,,,,,,,/S,N,YEST1/S,N,YEST3 $

9.117 DUMMOD1 Provides dummy module for inclusion of user written subroutines and modules

Format: DUMMOD1

IDB1,IDB2,IDB3,IDB4,IDB5,IDB6,IDB7,IDB8/ ODB1,ODB2,ODB3,ODB4,ODB5,ODB6,ODB7,ODB8/ IPARM1/IPARM2/IPARM3/IPARM4/RPARM1/RPARM2/ CHPARM/RDPARM/CPARM/CDPARM $

Input Data Blocks: IDBi

Table or matrix

Output Data Blocks: ODBi

Table or matrix

Parameters: IPARMi

Input/output-integer-default=-1

RPARMi

Input/output-real-default=-1.0

CHPARM

Input/output-character-default=‘ABCDEFGH’

RDPARM

Input/output-real double precision-default=-1.D0

CPARM

Input/output-complex-default=(-1.0,-1.0)

CDPARM

Input/output-complex double precision-default=(-1.D0, 1.0D0)

9.118 DUMMOD2 Provides dummy module for inclusion of user written subroutines and modules

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Format: DUMMOD2

IDB1,IDB2,IDB3,IDB4,IDB5,IDB6,IDB7,IDB8/ODB1,ODB2, ODB3,ODB4,ODB5,ODB6,ODB7,ODB8/ IPARM1/IPARM2/IPARM3/IPARM4/RPARM1/RPARM2/ CHPARM/RDPARM/CPARM/CDPARM $

Input Data Blocks: IDBi

Table or matrix

Output Data Blocks: ODBi

Table or matrix

Parameters: IPARMi

Input/output-integer-default=-1

RPARMi

Input/output-real-default=-1.0

CHPARM

Input/output-character-default=‘ABCDEFGH’

RDPARM

Input/output-real double precision-default=-1.D0

CPARM

Input/output-complex-default=(-1.0,-1.0)

CDPARM

Input/output-complex double precision-default=(-1.D0, 1.0D0)

9.119 DUMMOD3 Provides dummy module for inclusion of user written subroutines and modules

Format: DUMMOD3

IDB1,IDB2,IDB3,IDB4,IDB5,IDB6,IDB7,IDB8/ ODB1,ODB2,ODB3,ODB4,ODB5,ODB6,ODB7,ODB8/ IPARM1/IPARM2/IPARM3/IPARM4/RPARM1/RPARM2/ CHPARM/RDPARM/CPARM/CDPARM $

Input Data Blocks: IDBi

Table of matrix

Output Data Blocks: ODBi

Table of matrix

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Parameters: IPARMi

Input/output-integer-default=-1

RPARMi

Input/output-real-default=-1.0

CHPARM

Input/output-character-default=‘ABCDEFGH’

RDPARM

Input/output-real double precision-default=-1.D0

CPARM

Input/output-complex-default=(-1.0,-1.0)

CDPARM

Input/output-complex double precision-default=(-1.D0, 1.0D0)

9.120 DUMMOD4 Provides dummy module for inclusion of user written subroutines and modules

Format: DUMMOD4

IDB1,IDB2,IDB3,IDB4,IDB5,IDB6,IDB7,IDB8/ ODB1,ODB2,ODB3,ODB4,ODB5,ODB6,ODB7,ODB8/ IPARM1/IPARM2/IPARM3/IPARM4/RPARM1/RPARM2/ CHPARM/RDPARM/CPARM/CDPARM $

Input Data Blocks: IDBi

Table of matrix

Output Data Blocks: ODBi

Table of matrix

Parameters: IPARMi

Input/output-integer-default=-1

RPARMi

Input/output-real-default=-1.0

CHPARM

Input/output-character-default=‘ABCDEFGH’

RDPARM

Input/output-real double precision-default=-1.D0

CPARM

Input/output-complex-default=(-1.0,-1.0)

CDPARM

Input/output-complex double precision-default=(-1.D0, 1.0D0)

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9.121 DVIEWP Generates view-element and view-grid information for processing p-elements Generates the view-element and view-grid information for processing p-elements in design sensitivity analysis.

Format: DVIEWP

CASECC,OINT,PELSET,ESTDCN,TABECN,BGPDVP,CSTM/ VIEWTBDS/ S,N,VUGNEXT/S,N,VUENEXT/VUGJUMP/VUELJUMP/ VUHEXA/VUPENTA/VUTETRA/VUQUAD4/VUTRIA3/VUBEAM/ S,N,VUEXIST $

Input Data Blocks: CASECC

Table of Case Control command images

OINT

P-element output control table. Contains OUTPUT and OUTRCV Bulk Data entries.

PELSET

P-element set table, contains SETS DEFINITIONS

ESTDCN

Element summary table which incorporates combined constraints and design variables

TABECN

Table of relationship between internal identification numbers of constraints in ESTDCN and elements and responses in R1TABR

BGPDVP

Basic grid point definition table for the forward (or central) perturbed configuration

CSTM

Table of coordinate system transformation matrices

Output Data Blocks: VIEWTBDS

View information table, contains the relationship between each p-element and its view-elements and view-grids for the perturbed model

Parameters: VUGNEXT

Input/output-integer-default=0. Starting identification number for next view-grid.

VUENEXT

Input/output-integer-default=0. Starting identification number for next view-element

VUGJUMP

Input-integer-default=1000. Delta between view-grid identification numbers.

VUELJUMP

Input-integer-default=1000. Delta between view-element identification numbers.

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VUHEXA

Input-character-default=‘VUHEXA’ Name for VUHEXA element.

VUPENTA

Input-character-default=‘VUPENTA’ Name for VUPENTA element.

VUTETRA

Input-character-default=‘VUTETRA’ Name for VUTETRA element.

VUQUAD4

Input-character-default=‘VUQUAD4’ Name for VUQUAD4 element.

VUTRIA3

Input-character-default=‘VUTRIA3’ Name for VUTRIA3 element.

VUBEAM

Input-character-default=‘VUBEAM’ Name for VUBEAM element.

VUEXIST

Output-logical-default=FALSE. View-element flag. Set to TRUE if view-elements exist.

9.122 DYNREDU Computes approximate eigenvectors

Format: DYNREDU

LXX,MXX,CASECC,DYNAMIC/ PHZ,MZZ/ NOZSET/NOYSET/EPSMALC/EPSBIG/S,N,NOBSET0/NORSET $

Input Data Blocks: LXX

Lower triangular factor/diagonal of shifted stiffness matrix

MXX

Mass matrix in any set. Usually v-set.

CASECC

Table of Case Control command images

DYNAMIC

Table of Bulk Data entry images related to dynamics

Output Data Blocks: PHZ

Generalized degree-of-freedom transformation matrix

MZZ

Generalized mass matrix based on PHZ

Parameters: NOZSET

Input-integer-no default. Number of generalized degrees-of-freedom. Also number of columns in PHZ.

NOYSET

Input-integer-no default. Number of generalized degrees-of-freedom with non-null columns in PHZ.

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EPSMALC

Input-real-no default. Small number for tuning.

EPSBIG

Input-real-no default. Large number for tuning.

NOBSET0

Output-integer-default=0. Number of null columns in PHZ in front of non-null columns.

NORSET

Input-integer-default=0. Number of degrees-of-freedom in the r-set.

Remarks: Siemens PLM Software recommends that NOZSET be equal to NOYSET and NOBSET not be specified; that is, DYNREDU LXX,MXX,CASECC,DYNAMIC/ PHY,MYY/ NOYSET/NOYSET/EPSMALC/EPSBIG//NORSET $

9.123 EFFMAS Computes modal effective mass. Compute the modal effective mass based on the normal modes.

Format: EFFMAS

CASECC,MAA,PHA,LAMA,USET,BGPDT,UNUSED,CSTM,VGQ/ TEMF,EMM,DMA,MEMF,MPFEM,MEM,MEW,MDLIST/ SEID/WTMASS/S,N,CARDNO/SETNAM/IUNIT/S,N,IPLOT/EFOPT/S,N,NORBM $

Input Data Blocks: CASECC

Table of Case Control command images

MAA

Mass matrix in a-set or g-set

PHA

Normal modes eigenvector matrix in the a-set or g-set

LAMA

Normal modes eigenvalue summary table

USET

Degree-of-freedom set membership table for g-set

BGPDT

Basic grid point definition table

UNUSED

Unused

CSTM

Table of coordinate system transformation matrices

VGQ

Partitioning vector which is g-set size and contains values of 1.0 at rows corresponding to degrees-of-freedom in the q-set

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Output Data Blocks: TEMF

Total effective mass fraction table

EMM

Effective mass matrix

MA

Rigid body mass matrix for the a-set

MEMF

Modal effective mass fraction table

MPFEM

Modal participation factors for effective mass

MEM

Modal effective mass matrix

MEW

Modal effective weight matrix

MDLIST

List of modes for output selected by effective mass fraction

Parameters: SEID

Input-integer-no default. Superelement identification number.

WTMASS

Input-real-no default. Scale factor on structural mass matrix. See the NX Nastran Quick Reference Guide.

CARDNO

Input/output-integer-default=0. Punch file line counter. CARDNO is incremented by one for each line written to the punch file and is also written into columns 73-80 of each line.

SETNAM

Input-character-default=‘g’. Degree-of-freedom set name.

IUNIT

Input-integer-no default. IUNIT is the Fortran unit number on which the data blocks are to be written if the PLOT option is requested.

IPLOT

Output-integer-default=0. Set to 1 if PLOT option is requested.

EFOPT

Input-integer-default=0. When set to 1, ignores case control parameters and forces output of all results.

NORBM

Output-integer-default=0. Set to 1 if no rigid body mass matrix was produced.

9.124 ELFDR Transforms grid point force balance output from GPFDR module Transforms grid point force balance output (from GPFDR module) from the global coordinate system to the elemental coordinate systems or to the edges of adjacent elements. Applicable to line and shell elements only.

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Format: ELFDR

OGPFB1,GPECT,CSTM,SIL,GPL,BGPDT/ OELOF1,OELOP1/ NOELOF/NOELOP/UNUSED3 $

Input Data Blocks: OGPFB1

Table of grid point forces in SORT1 format

GPECT

Grid point element connection table

CSTM

Table of coordinate system transformation matrices

SIL

Scalar index list

GPL

External grid/scalar point identification number list

BGPDT

Basic grid point definition table

Output Data Blocks: OELOF1

Table of element oriented forces connected to common grid points in SORT1 format

OELOP1

Table of element-oriented forces oriented along adjacent element edge directions and summations of these components on equivalent edges in SORT1 format

Parameters: NOELOF

NOELOP

UNUSED3

Input-integer-default=0. OELOF1 generation flag. =0

9.150 FRRD1 Solves for the steady-state frequency response displacement solution Solves for the steady-state, modal or direct, frequency response, displacement solution using iterative or direct methods.

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Format: CASECC,DIT,KXX,BXX,MXX,K4XX,PXF,FRL,FOL,EDT, SILD,USETD,PARTVEC/ UXF,FOLT/ SOLTYP/NONCUP/ITSEPS/ITSMAX/NSKIP/FRRD1SEL/ S,N,FIRSTBAD/SETNAME/FREQDEP $

FRRD1

Input Data Blocks: CASECC

Table of Case Control command images

DIT

Table of TABLEij Bulk Data entry images

KXX

Stiffness matrix in any set. Usually h- or d-set.

BXX

Viscous damping in any set. Usually h- or d-set.

MXX

Mass matrix in any set. Usually h- or d-set.

K4XX

Structural damping in any set. Usually h- or d-set.

FRL

Frequency response list

FOL

Frequency response frequency output list

PXF

Frequency response load matrix in h-set (modal) or d-set

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

SILD

Scalar index list for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

USETD

Degree-of-freedom set membership table for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

PARTVEC

Partitioning vector with values of 1.0 at the rows corresponding to degrees of freedom which were eliminated in the partition to obtain KXX, and so on. Required for maximum efficiency during symmetric decomposition and if KXX represents a subset of the d-set (SETNAME=‘D‘). PARTVEC is not required if KXX represents the h-set. See SETNAME parameter description below.

Output Data Blocks: UXF

Solution matrix from frequency response analysis in d- or h-set

FOLT

Frequency response frequency output list with first frequency truncated if first frequency is zero. UXF is also similarly truncated.

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Parameters: SOLTYP

Input-character-no default. Solution method. ‘MODAL’: modal, usually for h-set matrices ‘DIRECT’: direct, usually for d-set matrices

NONCUP

Input-integer-no default. Algorithm selection. NONCUP=-1 requests uncoupled algorithm if SOLTYP=‘MODAL’and KXX, BXX, and MXX are diagonal. NONCUP=-2, requests uncoupled algorithm and off-diagonal terms of KXX, BXX, and MXX is ignored.

ITSEPS

Input-integer-default=0. Power of ten for convergence parameter epsilon for iterative solution method.

ITSMAX

Input-integer-default=0. Maximum number of iterations for iterative solution method.

NSKIP

Input-integer-default=1. Record number of current subcase in CASECC. Used only if the SMETHOD command selects the ITER Bulk Data entry which specifies values for the desired iteration parameters. If NSKIP=-1, CASECC is not required and the values are taken from the module specification of the values.

ZFREQ

Input-integer-default=0. Zero frequency truncation selection. If set to 1, the zero frequency, if any, is truncated from UXF and FOL.

FIRSTBAD

Output-logical-default=FALSE. Zero frequency truncation flag. Set to TRUE if first frequency is truncated.

SETNAME

Input-character-default=‘H’ Degree-of-freedom set name represented by KXX, and so on. If KXX represents, or is a subset of, the d-set, for maximum efficiency, the rows and columns KXX and MXX must correspond to or be a partition of the displacement set specified by SETNAME. If KXX and MXX are a partition, PARTVEC must also be specified.

FREQDEP

Input-logical-default=FALSE. Frequency-dependent element flag. Set to TRUE if processing frequency-dependent elements.

Remarks: 1. CASECC, FRL, FOL, and PXF cannot be purged. KXX, BXX, and MXX can be purged. 2. If SOLTYP=‘DIRECT‘, K4XX can be used to simulate viscoelastic materials. (See the NX Nastran User‘s Guide.) Otherwise, it can be purged. If SOLTYP=‘MODAL‘, K4XX is ignored and can be purged. 3. FRRD1 is similar to FRDD2 except that FRRD1 has many more efficiency improvements and viscoelastic material processing. However, FRRD2 performs special operations with the aerodynamic matrix list, QHHL. 4. EDT is required for the iterative solver if NSKIP>0 and the SMETHOD Case Control command selects the ITER Bulk Data entry. Otherwise it can be purged.

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9.151 FRRD2 Solves for the steady-state frequency response displacement solution Solves for the steady-state, modal or direct, frequency response, displacement solution using iterative or direct methods.

Format: KXX,BXX,MXX,QHHL,PXF,FOL,CASECC,EDT,SILD, USETD,PARTVEC/ UXF,FOLT/ BOV/Q/MACH/NONCUP/ITSEPS/ITSMAX/SETNAME/ FRRD2SEL/S,N,FIRSTBAD $

FRRD2

Input Data Blocks: KXX

Stiffness matrix in any set. Usually h- or d-set.

BXX

Viscous damping in any set. Usually h- or d-set.

MXX

Mass matrix in any set. Usually h- or d-set.

QHHL

Aerodynamic matrix list

PXF

Frequency response load matrix in h-set (modal) or d-set

FOL

Frequency response frequency output list

CASECC

Table of Case Control command images

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

SILD

Scalar index list for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

USETD

Degree-of-freedom set membership table for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

PARTVEC

Partitioning vector with values of 1.0 at the rows corresponding to degrees of freedom which were eliminated in the partition to obtain KXX, and so on. Required for maximum efficiency during symmetric decomposition and if KXX represents a subset of the d-set (SETNAME=‘D‘). PARTVEC is not required if KXX represents the h-set. See SETNAME parameter description below.

Output Data Blocks: UXF

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FOLT

Frequency response frequency output list with first frequency truncated if first frequency is zero. UXF is also similarly truncated.

Parameters: BOV

Input-real-no default. Conversion from frequency to reduced frequency.

Q

Output-real-default=0.0. Dynamic pressure.

MACH

Output-real-default=0.0. Mach number.

NONCUP

Input-integer-default=-1. Algorithm selection. NONCUP=-1 requests uncoupled algorithm if KXX, BXX, and MXX are diagonal. NONCUP=-2, requests uncoupled algorithm and off-diagonal terms of KXX, BXX, and MXX is ignored.

ITSEPS

Input-integer-default=0. Power of ten for convergence parameter epsilon for iterative solution method.

ITSMAX

Input-integer-default=0. Maximum number of iterations for iterative solution method.

SETNAME

Input-character-default=‘H’ Degree-of-freedom set name represented by KXX, and so on. If KXX represents, or is a subset of, the d-set, for maximum efficiency, the rows and columns KXX and MXX must correspond to or be a partition of the displacement set specified by SETNAME. If KXX and MXX are a partition, PARTVEC must also be specified.

ZFREQ

Input-integer-default=0. Zero frequency truncation selection. If set to 1, the zero frequency, if any, is truncated from UXF and FOL.

FIRSTBAD

Output-logical-default=FALSE. Zero frequency truncation flag. Set to TRUE if first frequency is truncated.

Remarks: 1. FOL and PXF cannot be purged. KXX, BXX, MXX, and QHHL can be purged. 2. FRRD1 is similar to FRDD2 except that FRRD1 has many more efficiency improvements and viscoelastic material processing. However, FRRD2 performs special operations with the aerodynamic matrix list, QHHL. 3. CASECC and EDT are required if the iterative solver is NSKIP>0 and the SMETHOD Case Control command selects the ITER Bulk Data entry. Otherwise it can be purged.

9.152 FRRDRU Solves for modal frequency response. Modal matrices from GKAMW are needed for displacement solution.

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Format: FRRDRU

CASES,DIT,K2HHF,M2HHF,B2HHF,B2HHCP,PXF,FRL,FOL,UNUSED1, UNUSED2,UNUSED3,VPHFS,KDD1,BDD1,MDD1,PHDSH,KDD2,BDD2,MDD2/ UXF,FOLT/ SOLTYP/NONCUP/ZFREQ/NOERR/FIRSTBAD $

Input Data Blocks: CASES

Table of case control command images

DIT

Table of TABLEij Bulk Data entry images

K2HHF

Modal stiffness matrix of fluid

M2HHF

Modal mass matrix of fluid

B2HHF

Modal damping matrix of fluid

B2HHCP

Modal damping matrix of coupling

PXF

Frequency response load matrix in h-set

FRL

Frequency response list

FOL

Frequency response frequency output list

VPHFS

Partition vector of fluid and structure

KDD1

Modal stiffness matrix generated by GKAMW

BDD1

Modal damping matrix generated by GKAMW

MDD1

Modal mass matrix generated by GKAMW

PHDSH

Projection vectors from D-set to H-set

KDD2

Stiffness matrix of structure

BDD2

Damping matrix of structure

MDD2

Mass matrix of structure

Output Data Blocks: UXF

Solution matrix from frequency response analysis in h-set

FOLT

Frequency response frequency output list with first frequency truncated if first frequency is zero. UXF is also similarly truncated.

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Parameters: SOLTYP

Input-character-no default. Solution method. ‘MODAL’: modal, usually for h-set matrices ‘DIRECT’: direct, usually for d-set matrices

NONCUP

Input-integer-no default. Algorithm selection. NONCUP=-1 requests uncoupled algorithm if SOLTYP=’MODAL’ and KDD1, BDD1 and MDD1 are diagonal. NONCUP=-2, requests uncoupled algorithm and off-diagonal terms of KDD1, BDD1, and MDD1 are ignored.

ZFREQ

Input-integer-default=0. Zero frequency truncation selection. If set to 1, the zero frequency, if any, is truncated from UXF and FOL.

NOERR

Output-integer-default=0. If an error occurred, then NOERR is set to 1.

FIRSTBAD

Output-logical-default=FALSE. Zero frequency truncation flag. Set to TRUE if first frequency is truncated.

9.153 GENTRAN Generates a transformation matrix Generates a transformation matrix that converts the upstream boundary coordinate system to the downstream coordinate system.

Format: GENTRAN

SEMAP,BGPDTS,CSTMS,BGPDTD,CSTMD,SCSTM/ MAPS/ SEID $

Input Data Blocks: SEMAP

Superelement map table

BGPDTS

Basic grid point definition table for the current superelement

CSTMS

Table of coordinate system transformation matrices for the current superelement

BGPDTD

Basic grid point definition table for the downstream superelement

CSTMD

Table of coordinate system transformation matrices for the downstream superelement

SCSTM

Table of global transformation matrices for partitioned superelements

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Output Data Block: MAPS

Superelement upstream to downstream boundary coordinate transformation matrix

Parameter: SEID

Input-integer-default=0. Superelement identification number.

Example: Excerpt from subDMAP PHASE0: DO WHILE ( NOT(RSONLY) AND LPFLG-1 AND SEBULK ) $ SEP2DR SLIST,EMAP//S,N,SEID/S,N,PEID/S,N,SEDWN/ S,N,LPFLG/////////SEP2CNTL//-1/S,N,PARTSE/ S,N,SETYPE/S,N,REID $ IF ( PARTSE ) THEN $ NP=SEDWN $ DBVIEW BGPDTD=BGPDTS WHERE ( PEID=NP ) $ DBVIEW CSTMD =CSTMS WHERE ( PEID=NP ) $ GENTRAN EMAP,BGPDTS,CSTMS,BGPDTD,CSTMD,SCSTM/ MAPS/SEID $ ENDIF $ PARTSE ENDDO $ NOT(RSONLY) AND LPFLG-1 AND SEBULK

9.154 GETCOL Reads the STATSUB and IC(STATSUB) Case Control command subcase identification number.

Format: GETCOL

CASEBUCK,CASESTAT// NSKIP/S,N,BCKCOL/S,N,PRECOL/S,N,ICCOLN $

Input Data Blocks: CASEBUCK

Table of Case Control command images for buckling analysis

CASESTAT

Table of Case Control command images for static analysis

Output Data Blocks: None.

Parameters: NSKIP

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BCKCOL

Output-integer-no default. Subcase record number in CASESTAT referenced by the STATSUB(BUCKLE) subcase identification number. BCKCOL also corresponds to the column number of static solution vector.

PRECOL

Output-integer-default-0. Subcase record number in CASESTAT referenced by the STATSUB(PRELOAD) subcase identification number. PRECOL also corresponds to the column number of static solution vector.

ICCOLN

Output-integer-default=0. Column number of static solution matrix as derived from the IC(STATSUB) Case Control command specification.

Remarks: If the STATSUB subcase identification number is not found in CASEBUCK, BCKCOL is set to 1. If the subcase identification number specified by the STATSUB command is not found in CASESTAT, a fatal message is issued.

9.155 GETMKL Create list of Mach numbers on reduced frequency pairs

Format: GETMKL

EDT/MKLIST/S,N,NMK $

Input Data Blocks: EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

Output Data Blocks: MKLIST

Table of Mach number and reduced frequency pairs

Parameters: NMK

Output-integer-default=0. Number of Mach number and reduced frequency pairs.

9.156 GI Generates aerodynamic spline transformation matrix

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Format: GI

Input Data Blocks: AERO

Table of control information for aerodynamic analysis. Output by APD.

SPLINE

Table of SETi, AELIST, and SPLINEi Bulk Data entry images with external grid identification numbers

AMSPLINE

Table of aerodynamic splines for display

BGPDT

Basic grid point definition table

AEBGPDT

The basic grid point definition table with the aerodynamic degrees of freedom added (ks-set in AEUSET)

AEUSET

Aerodynamic USET table

AECOMP

Aerodynamic component definition table

CSTMA

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points

Output Data Blocks: GPGK

Aerodynamic transformation matrix for loads from the k-set to g-set

GDGK

Aerodynamic transformation matrix for displacements from the k-set to g-set

Parameters: None.

Example: Excerpt from subDMAP AERO0: DBVIEW AEUSET=USET0 WHERE (MODLTYPE=‘AEROSTRC’AND WILDCARD) $ DBVIEW AEBGPDT=BGPDTS WHERE (MODLTYPE=‘AEROSTRC’AND WILDCARD) $ GI AERO,SPLINE,XBGPDT,AEBGPDT,AEUSET,AECOMP,CSTMA/ GPGK0,GDGK0 $

9.157 GKAM Assembles modal mass, damping and stiffness matrices

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Format: GKAM

USETD,PHA,MI,LAMA,DIT,M2DD,B2DD,K2DD,CASECC/ MHH,BHH,KHH,PHDH,ZETA/ NOUE/LMODES/LFREQ/HFREQ/UNUSED5/UNUSED6/UNUSED7/ S,N,NONCUP/S,N,FMODE/KDAMP/FLUID/UNUSED12 $

Input Data Blocks: USETD

Degree-of-freedom set membership table for p-set

PHA

Normal modes eigenvector matrix in the a-set

MI

Modal mass matrix. See Remark 5.

LAMA

Normal modes eigenvalue summary table

DIT

Table of TABLEij Bulk Data entry images

M2DD

Mass matrix contribution from the M2PP Case Control command and reduced to the d-set

B2DD

Total damping matrix from viscous damping elements and the B2PP Case Control command and reduced to the d-set. In transient response analysis, B2DD can also include structural damping effects.

K2DD

Stiffness matrix contribution from the K2PP Case Control command and reduced to the d-set. In frequency response analysis, K2DD can also include structural damping effects.

CASECC

Table of Case Control command images

Output Data Blocks: BHH

Generalized (modal) damping matrix

MHH

Generalized (modal) mass matrix

KHH

Generalized (modal) stiffness matrix.

PHDH

Transformation matrix from d-set to h-set (modal)

ZETA

Diagonal matrix of viscous damping coefficients (modal).

Parameters: NOUE

Input-integer-no default. The number of EXTRA points. Set to -1 if there are no extra points.

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LMODES

Input-integer-no default. The number of lowest modes to use in modal transformation. All outputs have LMODES number of columns.

LFREQ

Input-real-no default. Lower frequency limit of modes to use in modal transformation.

HFREQ

Input-real-no default. Upper frequency limit of modes to use in modal transformation.

UNUSED5

Input-integer-no default. Unused.

UNUSED6

Input-integer-no default. Unused.

UNUSED7

Input-integer-no default. Unused.

NONCUP

Output-integer-no default. If K2DD, B2DD, and M2DD are purged. the model is considered uncoupled and NONCUP is set to -1.

FMODE

Output-integer-default=1. The lowest mode number resulting from LMODES or LFREQ and HFREQ.

KDAMP

Input-integer-default=1. Viscous modal to structural damping flag. If set to -1, viscous modal damping (SDAMPING Case Control command) is included in the stiffness matrix as structural damping.

FLUID

Input-logical-default=FALSE. Fluid damping processing flag. If TRUE, the modal damping set identification number is obtained from the SDAMPING(FLUID) Case Control command.

UNUSED12

Input-logical-default=FALSE. Unused.

Remarks: 1. USETD can be purged if there are no extra points (NOUE0. 8. See the NX Nastran User‘s Guide for further details.

9.158 GKAMW Assembles modal mass, damping and stiffness matrices for FRRDRU.

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Format: GKAMW

USETD,PHA,MI,LAMA,DIT,M2DD,B2DD,K2DD,CASECC/ MHH,BHH,KHH,PHDH,ZETA,BDD1,MDD1/ NOUE/LMODES/LFREQ/HFREQ/UNUSED5/UNUSED6/UNUSED7/ S,N,NONCUP/S,N,FMODE/KDAMP/FLUID/UNUSED12 $

Input Data Blocks: USETD

Degree-of-freedom set membership table for p-set

PHA

Normal modes eigenvector matrix in the a-set

MI

Modal mass matrix. See Remark 6.

LAMA

Normal modes eigenvalue summary table

DIT

Table of TABLEij Bulk Data entry images

M2DD

Mass matrix contribution from the M2PP Case Control command and reduced to the d-set

B2DD

Total damping matrix from viscous damping elements and the B2PP Case Control command and reduced to the d-set. In transient response analysis, B2DD can also include structural damping effects.

K2DD

Stiffness matrix contribution from the K2PP Case Control command and reduced to the d-set. In frequency response analysis, K2DD can also include structural damping effects.

CASECC

Table of Case Control command images

Output Data Blocks: BHH

Generalized (modal) damping matrix

MHH

Generalized (modal) mass matrix

KHH

Generalized (modal) stiffness matrix

PHDH

Transformation matrix from d-set to h-set (modal)

ZETA

Diagonal matrix of viscous damping coefficients (modal).

BDD1

Modal damping matrix

MDD1

Modal mass matrix

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Parameters: NOUE

Input-integer-no default. The number of EXTRA points. Set to -1 if there are no extra points.

LMODES

Input-integer-no default. The number of lowest modes to use in modal transformation. All outputs have LMODES number of columns.

LFREQ

Input-real-no default. Lower frequency limit of modes to use in modal transformation.

HFREQ

Input-real-no default. Upper frequency limit of modes to use in modal transformation.

UNUSED5

Input-integer-no default. Unused.

UNUSED6

Input-integer-no default. Unused.

UNUSED7

Input-integer-no default. Unused.

NONCUP

Output-integer-no default. If K2DD, B2DD, and M2DD are purged. the model is considered uncoupled and NONCUP is set to -1.

FMODE

Output-integer-default=1. The lowest mode number resulting from LMODES or LFREQ and HFREQ.

KDAMP

Input-integer-default=1. Viscous modal to structural damping flag. If set to -1, viscous modal damping (SDAMPING Case Control command) is included in the stiffness matrix as structural damping.

FLUID

Input-logical-default=FALSE. Fluid damping processing flag. If TRUE, the modal damping set identification number is obtained from the SDAMPING(FLUID) Case Control command.

UNUSED12

Input-logical-default=FALSE. Unused.

Remarks: 1. GKAMW is the same as GKAM, except that GKAMW generates special modal matrices for FRRDRU. 2. USETD can be purged if there are no extra points (NOUE0.

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9. See the NX Nastran User‘s Guide for further details.

9.159 GLFONOTR Glue normal and in-plane tractions.

Format: GLFONOTR

GNELM,UGLCURB,ELGNST,CASECC/ OQGGF1,OBG1/NROW/NVEC $

Input Data Blocks: GNELM

Glue element definition table

UGLCURB

Global displacements in basic coordinate system

ELGNST

Table of glue element stiffness

CASECC

Table of Case Control command images

Output Data Blocks: OQGGF1

Glue forces at grid point in basic coordinate system

OBG1

Glue normal and tangential tractions at grid point in basic coordinate system

Parameters: NROW

Input-integer-no default. Number of rows in the glue force vector.

NVEC

Input-integer-no default. Number of solution results to process.

9.160 GMERGE Global mode collection for dmp solution

Format: GMERGE

PHIX1,LAMA,EQMAP,GAPAR,VF01,EQEXINS,COLMAP,BNDMAP/ PHIX/NUMCPU/S,N,ERROR $

Input Data Blocks: PHIX1

Local eigenvector file (required).

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LAMA

Local eigenvalue file (required)

COLMAP

Color map from GPARTN

BNDMAP

Local boundary map from GPARTN

NUMCPU

Number of dmp processors parameter (required)

Output Data Blocks: PHIX

Global eigenvector file

ERROR

Merging error

9.161 GNFM Computes element forces due to large displacements Computes the element forces due to large displacements and optionally computes the elemental stiffness matrices associated with incremental deflections.

Format: GNFM

KELM,KDICT,KDELM,KDDICT,EST,CSTM,UG,BGPDT/ FG,KELM1,KDICT1/ SKPMTX/LUSET/NSKIP $

Input Data Blocks: KELM

Table of element matrices for stiffness

KDICT

KELM dictionary table

KDELM

Table of element matrices for differential stiffness

KDDICT

KDELM dictionary table

EST

Element summary table

CSTM

Table of coordinate system transformation matrices

UG

Displacement matrix in g-set

BGPDT

Basic grid point definition table

Output Data Blocks: FG

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KELM1

Table of element matrices for incremental stiffness

KDICT1

KELM1 dictionary table

Parameters: SKPMTX

Input-integer-default=0. If SKPMTX0, KELM1 and KDICT1 are generated.

LUSET

Input-integer-default=0. The number of degrees-of-freedom in the g-set.

NSKIP

Input-integer-default=0. Loop counter in old geometric nonlinear analysis.

Remarks: 1. FG cannot be purged. 2. KELM1 and KDICT1 can be purged if SKPMTX0.

9.162 GP0 Modifies tables to include p-element information Modifies geometry, connectivity, loads, and constraints tables to include p-element information. Also creates edge, face, and body tables.

Format: GP0

CASECC,GEOM1,GEOM2,GEOM3,GEOM4,EPT, EDT,DEQATN,DEQIND,PELSET,PVAL0/ GEOM1M,GEOM2M,GEOM2A,GEOM3M,GEOM4M, EHT,EHTA,MEDGE,MFACE,GDNTAB,MBODY/ ALTSHAPE/UNIT1/UNIT2/S,N,PVALID/S,N,PEXIST/ GNSTART/S,N,GNMAX/GMTOL/INITAPI/PEDGEP/GNPROC $

Input Data Blocks: CASECC

Table of Case Control command images

GEOM1

Table of Bulk Data entry images related to geometry

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM3

Table of Bulk Data entry images related to static and thermal loads

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

EPT

Table of Bulk Data entry images related to element properties

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EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

PELSET

P-element set table, contains SETS DEFINITIONS. Output by PLTSET.

PVAL0

P-value table generated by the ADAPT module in previous superelement, adaptivity cycle, or run.

Output Data Blocks: GEOM1M

Table of Bulk Data entry images related to geometry and updated for the current p-level

GEOM2M

Table of Bulk Data entry images related to element connectivity and scalar points and updated for the current p-level.

GEOM2A

Table of secondary Bulk Data entry images related to element connectivity and updated for the current p-level

GEOM3M

Table of Bulk Data entry images related to static and thermal loads and updated for the current p-level

GEOM4M

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity and updated for the current p-level

EHT

Element hierarchical table for p-element analysis

EHTA

Secondary element hierarchical table for p-element analysis

MEDGE

Edge table for p-element analysis

MFACE

Face table for p-element analysis

GDNTAB

Table of grid points generated for p-element analysis

MBODY

Body table for p-element analysis

Parameters: ALTSHAPE

Input-integer-default=0. Specifies set of displacement functions in p-element analysis. ALTSHAPE=0 selects the MacNeal set and 1 selects the Full Product Space set.

UNIT1

Input-integer-default=0. Fortran unit number containing edge table information.

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UNIT2

Input-integer-default=0. Fortran unit number containing face table information.

PVALID

Output-integer-default=0. P-value set identification number.

PEXIST

Output-logical-default=TRUE. Set to FALSE if p-elements are not present.

GNSTART

Input-integer-default=0. First grid identification number in GEOM1M.

GNMAX

Output-integer-no default. Maximum grid identification number in GEOM1M.

GMTOL

Input-real-default=1.E-5. Geometric tolerance.

INITAPI

Input-logical-default=TRUE. API flag.

PEDGEP

Input-integer-default=0.

GNPROC

Input-logical-default=TRUE. Grid-n processing flag. If set to TRUE, grid-n information is processed.

9.163 GP1 Performs basic geometry processing

Format: GP1

GEOM1,GEOM2,GEOM3,GDNTAB,MEDGE,SGPDT,DYNAMIC/ GPL,EQEXIN,GPDT,CSTM,BGPDT,SIL,VGF,GEOM3B, DYNAMICB/ S,N,LUSET/S,N,NOCSTM/S,N,NOPOINTS/ UNIT/UPERM/UPRMT/NUFLAG/SEID/NUMLM $

Input Data Blocks: GEOM1

Table of Bulk Data entry images related to geometry

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM3

Table of Bulk Data entry images related to static and thermal loads

GDNTAB

Table of grid points generated for p-element analysis

MEDGE

Edge table for p-element analysis

SGPDT

Superelement basic grid point definition table

DYNAMIC

Table of Bulk Data entry images related to dynamics

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Output Data Blocks: GPL

External grid/scalar point identification number list

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

GPDT

Grid point definition table

CSTM

Table of coordinate system transformation matrices

BGPDT

Basic grid point definition table

SIL

Scalar index list

VGF

Fluid/structure partitioning vector with ones at the rows corresponding to fluid degrees-of-freedom

GEOM3B

Table of Bulk Data entry images related to static and thermal loads with DAREA entry images converted to equivalent FORCE and MOMENT entry images

DYNAMICB

Table of Bulk Data entry images related to dynamics without DAREA entry images

Parameters: LUSET

Output-integer-default=0. The number of degrees-of-freedom in the g-set.

NOCSTM

Output-integer-no default. Number of coordinate systems found in GEOM1. Set to -1 if none are found.

NOPOINTS

Output-integer-no default. Grid point flag. Set to -1 if none are found. Otherwise, set to 1.

UNIT

Input-real-default=1.0. AUNIT record factor for electromagnetic analysis.

UPERM

Input-real-default=1.2566E-06. Permeability for electromagnetic analysis.

UPRMT

Input-real-default=8.8542E-12. Permittivity for electromagnetic analysis.

NUFLAG

Input-integer-default=10. Unit type for electromagnetic analysis.

SEID

Input-integer-default=-1. Superelement identification number.

NUMLM

Input-integer-default=0. Number of Lagrange Multiplies from Lagrange rigid elements.

Remarks: 1. GP1 assembles a list of all grid and scalar points and places them in internal order, computes coordinate system transformation matrices, and transforms all grid points to the basic coordinate system.

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2. No output data block, except VGF, can be purged.

9.164 GP1EX Modify the GEOM3 data block to convert external superelement loads via SELOAD bulk entries into FORCE and MOMENT bulk entries.

Format: GP1EX

GEOM1,GEOM3,BGPDTS,EQEXINS,SELOAD,PG/ GEOM3XSE/SEID/S,N,UPDATE $

Input Data Blocks: GEOM1

Table of bulk entry images related to geometry for the entire model.

GEOM3

Table of bulk entry images related to static and thermal loads for the entire model.

BGPDTS

Basic grid point definition table for the external superelement.

EQEXINS

Table to equivalence external and internal grid/scalar numbers for the external superelement.

SELOAD

DTI table for SELOAD bulk entry images.

PG

External superelement load matrix in the g-set.

Output Data Blocks: GEOM3XSE

Table of bulk data entry images related to static and thermal loads for the entire model that now contains FORCE and MOMENT bulk images to represent the external superelement applied loads.

Parameters: SEID

Input-integer-no default. Superelement ID of the external superelement.

UPDATE

Output-integer-no default. GEOM3 update flag. 0 = GEOM3 not updated and GEOM3XSE not created 1 = GEOM3 updated and GEOM3XSE created

9.165 GP1LM Add Lagrange rigids to geom2 table

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Format: GP1LM

GEOM2,GEOM4/GEOMN/SEID/NUMLM $

Input Data Blocks: GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

Output Data Blocks: GEOM2N

Updated GEOM2 TABLE

Parameters: SEID

Input-integer. Superelement identification number.

NUMLM

Output – integer. Number of Lagrange multipliers.

9.166 GP2 Processes element connectivity

Format: GP2

GEOM2,EQEXIN,EPT,GEOM2A,UNUSED5/ ECT,ECTA/ S,N,ACOUSTIC $

Input Data Blocks: GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

EPT

Element property table

GEOM2A

Table of secondary Bulk Data entry images related to element connectivity and updated for the current p-level

UNUSED5

Unused and can be purged

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Output Data Blocks: ECT

Element connectivity table

ECTA

Secondary element connectivity table

Parameter: ACOUSTIC

Output-integer-default=0. Fluid-structure analysis flag. 0

No fluid elements exist.

1

Penalty or fluid acoustic elements exists.

2

Fluid/structure coupling exists.

Remarks: 1. EQEXIN and ECT cannot be purged. 2. ECTA can be purged if GEOM2A is purged.

9.167 GP3 Processes static and thermal loads

Format: GP3

GEOM3,BGPDT,GEOM2,EDT,UGH,ESTH,BGPDTH,CASEHEAT/ SLT,ETT/ S,N,NOLOAD/S,N,NOGRAV/S,N,NOTEMP $

Input Data Blocks: GEOM3

Table of Bulk Data entry images related to static and thermal loads

BGPDT

Basic grid point definition table

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

UGH

Temperature matrix in g-set from a heat transfer analysis

ESTH

Element summary table from a heat transfer analysis

BGPDTH

Basic grid point definition table from a heat transfer analysis

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Case Control table from a heat transfer analysis

Output Data Blocks: SLT

Table of static loads

ETT

Element temperature table

Parameters: NOLOAD

Output-integer-no default. Static load existence flag. Set to -1 if no static loads and SLT is not created, +1 otherwise.

NOGRAV

Output-integer-no default. Gravity load existence flag. Set to -1 if no GRAV Bulk Data entry images, +1 otherwise.

NOTEMP

Output-integer-no default. Thermal load existence flag. Set to -1 if no TEMP or TEMPD Bulk Data entry images in GEOM3 and ETT is not created, +1 otherwise.

Remarks: 1. BGPDTH cannot be purged. 2. SLT can be purged if there are no static loads. 3. ETT can be purged if there are no thermal loads 4. If UGH is present in structural analysis run, GP3 creates a new temperature set based on UGH with set identification numbers obtained from TSTRUC command in CASEHEAT. BGPDTH is used to correlate UGH to grid points. ESTH is not required for h-elements. For p-elements ESTH is appended to element ETT record for interpolation purposes in element decks. The DBVIEW statements that are used to define these inputs in SOLs 101-200 are listed below: DBVIEW UGH=UG

(WHERE APRCH=‘HEAT ’AND WILDCARD) $

DBVIEW ESTH=EST

(WHERE APRCH=‘HEAT ’) $

DBVIEW BGPDTH=BGPDTS

(WHERE APRCH=‘HEAT ‘) $

CASEHEAT can come from the CASE module or DBLOCATE DATABLK= (CASECCR/CASEHEAT) in the FMS.

9.168 GP4 Generates the degree-of-freedom set table

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Generates the degree-of-freedom set table based on single point constraints, multipoint constraints, rigid elements, and set membership assignment Bulk Data entries (for example, ASET). Also generates the enforced displacement matrix, the multipoint constraint equation matrix, and the enforced motion partitioning vector.

Format: GP4

CASECC,GEOM4,EQEXIN,SIL,GPDT,BGPDT,CSTM, MEDGE,MFACE,MBODY,GEOM2,GDNTAB,GPECTO/ RMG,YS0,USET0,PARTV/ LUSET/S,N,NOMSET/S,N,MPCF2/S,N,NOSSET/S,N,NOOSET/ S,N,NORSET/S,N,NSKIP/S,N,REPEAT/S,N,NOSET/S,N,NOL/ S,N,NOA/SEID/ALTSHAPE/SEBULK/DMAPNO/AUTOMPC $

Input Data Blocks: CASECC

Table of Case Control command images.

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

SIL

Scalar index list

GPDT

Grid point definition table

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

MEDGE

Edge table for p-element analysis

MFACE

Face table for p-element analysis

MBODY

Body table for p-element analysis

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GDNTAB

Table of grid points generated for p-element analysis

GPECT0

Grid point element connection table.

Output Data Blocks: RMG

Multipoint constraint equation matrix

YS0

Matrix of enforced displacements

USET0

Degree-of-freedom set membership table for g-set

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Partitioning vector of enforced motion dof.

Parameters: LUSET

Input-integer-default=0. The number of degrees-of-freedom in the g-set.

NOMSET

Output-integer-no default. Number of degrees-of-freedom in the m-set or multipoint constraint and rigid element flag. Set to -1 if there are none.

MPCF2

Output-integer-no default. Multipoint constraint set identification number change flag. Set to 1 if the current subcase contains a different multipoint constraint set from the previous subcase. Set to -1 otherwise or if there are no multipoint constraints in the current subcase.

NOSSET

Output-integer-no default. Number of degrees-of-freedom in the s-set. or single point constraint flag. Set to -1 if there are none.

NOOSET

Output-integer-no default. Number of degrees-of-freedom in the o-set or omitted degree-of-freedom flag. Set to -1 if there are none.

NORSET

Output-integer-no default. Number of degrees-of-freedom in the r-set. or supported degree-of-freedom flag. Set to -1 if there are none.

NSKIP

Input/output-integer-no default. The record number in CASECC corresponding to the first subcase of the current boundary condition.

REPEAT

Output-integer-no default. Last boundary condition flag. Set to -1 at the last boundary condition; +1 otherwise.

NOSET

Output-integer-no default. Constraint, omit, and support set flag. Set to -1 if NOMSET=-1, NOSSET=-1, NOOSET=-1, NORSET=-1 and no degrees-of-freedom defined in the a-set (for example, ASETi, QSETi Bulk Data entries); +1 otherwise.

NOL

Output-integer-default=1. Dependent set flag. Set to -1 if all degrees-of-freedom belong to m-set, s-set, o-set, and/or r-set; otherwise, the degrees-of-freedom in the l-set.

NOA

Output-integer-default=1. Constraint and omit set flag. Set to -1 if NOMSET=-1, NOSSET=-1, and NOOSET=-1; otherwise the number of degrees-of-freedom in the a-set.

SEID

Input-integer-default=0. Superelement identification number.

ALTSHAPE

Input-integer-default=0. Specifies set of displacement functions in p-element analysis. ALTSHAPE=0 selects the MacNeal set and 1 selects the Full Product Space set.

SEBULK

Input-logical-default=FALSE. Partitioned superelement presence flag. Set to TRUE if partitioned superelements are present or BEGIN SUPER is specified for the first BEGIN BULK Case Control command.

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DMAPNO

Integer-input-default=0. Solution sequence number stored in word 244 of the case control record.

AUTOMPC

Input-character-default=no. Specifies that the software automatically select the m-set dofs rather than use the m-set values as specified on MPC or RIGID element cards. See the AUTOMPC parameter in the Quick Reference Guide for details.

Remarks: 1. YS is purged if SPCD or SPC Bulk Data entries do not specify nonzero values for displacement. 2. GEOM4 can be purged. 3. CSTM can be purged if no coordinate systems are used.

9.169 GP5 Creates table of static loads for panels in coupled fluid/structure analysis.

Format: GP5

ECT,BGPDT,EQEXIN,EDT,SIL,GEOM2/ PANSLT,EQACST,NORTAB/ S,N,MPNFLG/S,N,NUMPAN/S,N,MATCH/NASOUT/GETNUMPN/ S,N,METHOD/S,N,SKINOUT/S,N,NORMAL/S,N,OVLPANG/ S,N,INTOL/S,N,ABSFLG/S,N,NGAUSS $

Input Data Blocks: ECT

Element connectivity table

BGPDT

Basic grid point definition table

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 and SET3 entries

SIL

Scalar index list

GEOM2

Table of bulk data images related to element connectivity

Output Data Blocks: PANSLT

Panel static load table

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EQACST

Equivalence table between internal fluid grid points and internal structural grid points which lie on the fluid/structure boundary. Output by GP5.

NORTAB

Table containing fluid face and the maximum of eight structural grids which lie within the acoustic face

Parameters: MPNFLG

Output-integer-default=0. Set to 1 if multiple panels exist.

NUMPAN

Output-integer-default=1. Number of panels.

MATCH

Output-integer-default=0. Type of fluid/structural mesh matching. 0

Matching mesh

1

Non-meshing mesh

NASOUT

Input-logical-default=TRUE. Print flag for fluid/structural mesh matching summary.

GETNUMPN

Input-logical-default=FALSE. Panel static load computation flag. If TRUE, get number of panels flag only and do not compute panel static loads.

METHOD

Output-character-default=”AS”. Fluid/structural coupling method. When = “AS”, the new accelerated coupling method is used. When = “CP”, the old coupling method is used.

SKINOUT

Input-character-default=”NONE”. Requests coupling debug punch file. When = “PUNCH”, a debug input file and punch file are output. Available only when METHOD = “AS”.

NORMAL

Output-real-default=0.2 when METHOD = “AS”; when = .001 METHOD = “CP”. Determines coupling search distance.

OVLPANG

Output-real-default=30 degrees. Overlapping angular tolerance in degrees. Used only when METHOD = “AS”.

INTOL

Input-real-See the ACMODL bulk data entry in the Quick Reference Guide for defaults. Inward normal search distance to detect fluid-structure interface.

ABSFLG

Input-logical-default=”FALSE”. When “TRUE”, the ABSOLUTE values for search distance are used. Else, use the relative search distance.

NGAUSS

Input-integer-default=0. Number of gauss points.

9.170 GP6 Converts NSML and NSML1 into NSM and NSM1 cards.

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Format: GP6

ECT,IEPT,BGPDT/EPTNSML/S,N,EPTNSML $

Input Data Blocks: ECT

Element connectivity table

IEPT

Table of bulk data entry images related to element properties

BGPDT

Basic grid point definition table

Output Data Blocks: EPTNSML

EPT updated from NSML and NSML1 records

Parameters: EPTNSML

Output-Integer-Default=0. EPTNSML Creation Flag (0: No; -1: Yes)

9.171 GPARTN Graph partitioning used for DMP solutions.

Format: GPARTN

KXX,MXX,USET,SILS,EQEXINS/ KXX1,MXX1,EQMAP,GAPAR,VFO1,USET1,SIL1, EQEXIN1,SPCCOL,MAPFIL,COLMAP,BNDMAP/ NUMCPU/GLOBDOF/LOCDOF/BNDDOF/OPTION $

Input Data Blocks: KXX

Global stiffness matrix file (required)

MXX

Global mass matrix file (required)

USETS

Global set definition data (required only for OPTION=1)

SILS

Global scalar index list (required only for OPTION=1)

EQEXINS

Global external/internal list (required only for OPTION=1)

NUMCPU

Number of dmp processors parameter (required)

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Output Data Blocks: KXX1

Local stiffness matrix partition file (including global boundary)

MXX1

Local mass matrix partition file (including global boundary)

USET1

Local set definition data.

SIL1

Local scalar index list

EQEXIN1

Local external/internal list

EQMAP

Local interior/boundary information data

GAPAR

Local a-set partitioning vector

VF01

Local f-set partitioning vector

SPCCOL

Local spc dof partitioning vector

MAPFILE

Containing 4 distinct components (only for OPTION=2): •

DOFMAP - degrees of freedom vs. nodal data map, see AMLS specification

•

XADJ - points to stiffness matrix adjacency list, see AMLS specification

•

ADJ - stiffness matrix adjacency list, see AMLS specification

•

NODELIST - user requested displacement nodes, see AMLS specification

COLMAP

Color map from GPARTN

BNDMAP

Local boundary map from GPARTN

GLOBDOF

Global degrees of freedom parameter

LOCDOF

Local degrees of freedom parameter

BNDDOF

Boundary degrees of freedom parameter

OPTION

Partitioning (1) or graph information generation (2) parameter

9.172 GPFDR Computes grid point forces and element strain energy

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Format: GPFDR

CASECC,UG,KELM,KDICT,ECT,EQEXIN,GPECT,PG,QG, BGPDT,{LAMA or FOL or TOL or OLF},CSTM,VELEM,PTELEM, QMG,NFDICT,FENL,MELM,MDICT,BELM,BDICT,MDLIST/ ONRGY1,OGPFB1,OEKE1,OEDE1/ APP/TINY/XFLAG/CYCLIC/WTMASS/S,N,NOSORT2 $

Input Data Blocks: CASECC

Table of Case Control command images

UG

Displacement matrix in g-set

KELM

Table of element matrices for stiffness

KDICT

KELM dictionary table

ECT

Element connectivity table

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

GPECT

Grid point element connection table

PG

Static load matrix for the g-set

QG

Single-point constraint forces of constraint matrix in the g-set

BGPDT

Basic grid point definition table

LAMA

Eigenvalue summary table for normal modes. Required for APP=‘REIG’

FOL

Frequency output list. Required for APP=‘FREQRESP’

TOL

Time output list. Required for APP=‘TRANRESP’

OLF

Nonlinear static load factor list. Required for APP=‘NLST’

SIL

Scalar index list

CSTM

Table of coordinate system transformation matrices

VELEM

Table of element lengths, areas, and volumes

PTELEM

Table of thermal loads in the elemental coordinate system

QMG

Multipoint constraint forces of constraint matrix in the g-set

NFDICT

Nonlinear element energy/force index table

FENL

Element energy and forces in nonlinear matrix format

MELM

Elemental matrices for mass

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MDICT

Dictionary table for MELM

BELM

Elemental matrices for damping

BDICT

Dictionary table for BELM

MDLIST

Selected mode list from EFFMAS

Output Data Blocks: ONRGY1

Table of element strain energies and energy densities in SORT1 format.

OGPFB1

Table of grid point forces in SORT1 format.

OEKE1

Elemental kinetic energy in SORT1 format.

OEDE1

Elemental energy loss in SORT1 format.

Parameters: APP

Input-character-no default. Analysis type. Allowable types are: ‘STATICS’

Linear statics

‘REIG’

Normal modes

‘FREQRESP’

Frequency response

‘TRANRESP’

Transient response

‘NLST’

Nonlinear static

TINY

Input-real-default=1.E-03. Small element strain energy value. Element strain energies less than TINY are not printed.

XFLAG

Input-integer-default=0. Strain energy method selection. 0

Elemental force

1

Cross displacement. See Remark 2.

CYCLIC

Input-logical-default=FALSE. Set to TRUE for cyclic symmetry models.

WTMASS

Input-real-default=1.0. Specifies scale factor on elemental mass matrix.

NOSORT2

Output-integer-default=-1. SORT2 format flag for OGPFB1 data block. Set to 1 if SORT2 format is requested; –1 otherwise.

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Remarks: 1. GPFDR creates the grid point force balance table for a user-selected set of points. This table lists the forces acting at each selected point due to element constraints, single-point constraints, and applied loads. Also listed is the sum total of these forces which represents the balance in an opposite direction due to multipoint constraints, general elements, round-off errors, and other nonlisted sources. Subtotals for element sets and element types are also provided. 2. GPFDR creates the element strain energy table for a user-selected set of elements. These selected elements are listed by type with their strain energy, percent of total strain energy with respect to all elements, and strain energy density. The strain energy is computed by one of the following equations: If XFLAG=0 (default):

Equation 9-22. If XFLAG=1:

Equation 9-23. where {u1e} is the displacement for the first subcase or mode, and where {uie} is the displacement for the i-th subcase or mode. 3. The strain energy density is computed by dividing the strain energy by the element volume. The total energy is computed by summing the element strain energies of all elements for which stiffness matrices exist. General elements are not included.

9.173 GPFTOTL Recalculates the totals for grid point force output.

Format: GPFTOTL

OGPFIN/OGPFOU $

Input Data Blocks: OGPFIN

Grid point force balance data block (SORT1 format) for which grid point force balance totals are to be recalculated.

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Output Data Blocks: OGPFOU

Resulting grid point force balance data block (SORT1 format).

Parameters: None

9.174 GPFXPND Expands a grid point force output data block based on a template.

Format: GPFXPND

OGPFTMP,OGPFIN/OGPFOU $

Input Data Blocks: OGPFTMP

Grid point force balance data block to be used as a template (SORT1 format).

OGPFIN

Grid point force balance data block (SORT1 format) to be expanded.

Output Data Blocks: OGPFOU

Resulting grid point force balance data block (SORT1 format).

Parameters: None

9.175 GPJAC Checks element Jacobians

Format: GPJAC

ECT,BGPDT//S,N,JACDET $

Input Data Blocks: ECT

Element connectivity table

BGPDT

Basic grid point definition table

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Output Data Blocks: None.

Parameter: JACDET

Output-integer-default=0. Bad Jacobian detection flag. Set to 1 if a bad Jacobian is detected.

Remarks: By default the run terminates if bad Jacobians are detected. If system cell 213 is equal to 1, the run does not terminate.

9.176 GPSP Performs auto-SPC operation Performs auto-SPC operation; that is, identifies and automatically constrains singularities.

Format: GPSP

Input Data Blocks: KNN

Stiffness matrix in n-set; after multipoint constraint reduction

KGG

Stiffness matrix in g-set

KMM

Stiffness matrix in m-set

RMG

Multipoint constraint equation matrix

USET0

Degree-of-freedom set membership table for g-set

SIL

Scalar index list

GPL

External grid/scalar point identification number list

YS0

Matrix of enforced displacements

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity

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Descriptions of DMAP Modules and Statements

Equivalence table between external and internal grid/scalar identification numbers

Output Data Blocks: USET

Degree-of-freedom set membership table for g-set

YS

Matrix of enforced displacements in the s-set

BD3X3

3x3 diagonal strip for boundary degrees-of-freedom from KGG for parallel domain decomposition

Parameters: NOSSET

Output-integer-default=0. Number of degrees-of-freedom in the s-set. or single point constraint flag. Set to -1 if there are none.

AUTOSPC

Input-character-default=‘YES’ Automatic constraint flag. If set to ‘YES‘, singularities are constrained.

PRGPST

Input-character-default=‘YES’ Singularity summary print flag. If set to ‘YES‘, the summary is printed.

SPCGEN

Input-integer-default=0. SPC Bulk Data entry punch flag. If set to >0, singularities identified by this module are written to the PUNCH file as SPC Bulk Data entries.

EPZERO

Input-real-default=1.E-8. Singularity test parameter. Singularities greater than EPZERO are not constrained.

ACON

Input-integer-default=0. B-set constraint flag. If ACON0, the METHOD command is ignored and the EIGR, EIGB, or EIGRL is selected by this parameter value. All subsequent parameter values (METH, F1, and so on) are ignored. If SID P2, the terms are ignored after P2.

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Example: Generate a vector of 5 unit terms followed by 7 zeros followed by two unit terms. MATGEN

,/UPART/6/14/0/5/7/2 $

Option P1 = 7 Generate a null matrix.

Format: MATGEN

,/MAT/7/P2/P3/P4/P5 $

Input Data Blocks: None.

Output Data Block: MAT

Null matrix

Parameters: P2

Number of rows

P3

Number of columns

P4

Form; if P4 = 0 and P2 = P3, the form is 6 (symmetric). If P4 = 0 and P2 = P3, the form is 2 (rectangular).

P5

Type: if P5 = 0, the type is the machine precision.

Example: Generate a 20 row by 15 column null matrix. MATGEN

,/N20X15/7/20/15 $

Option P1 = 8 Generate a matrix from equations based on its indices. The matrix is in single precision.

Format: MATGEN

,/MAT/8/P2/P3/P4/P5/P6 $

Input Data Blocks: None.

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Output Data Block: MAT

Matrix with element values based on its indices

Parameters: T

DTI table input

P2

= 0 generate all terms ≠ 0 generate only diagonal terms

P3

Number of rows

P4

Number of columns

P5

Number of the record in field 3 of the DTI entry used to define real coefficients P50

Data pairs from record P5 interpreted as above.

Number of the record in field 3 of the DTI entry used to define imaginary coefficients D1 P6 ≤ 0

No coefficients defined.

P6 > 0

Data pairs from record P6 interpreted as above where D(n1) = (n2).

Form of output matrix P7 ≤ 0

Form chosen to be 1 or 2, depending on P3 and P4.

P7 > 0

Form set to P7.

Coefficient print flag P8 = 0

Do not print coefficient lists.

P8 ≠ 0

Print coefficients lists C and D from the DTI input. (Print D list only if P6 > 0.)

The equation used to determine the coefficient of the (l,J)th term of the output matrix is:

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Equation 9-24. The Ci terms are input on two DTI Bulk Data entries. The entry referenced by P5 generates the real part of the term. The entry referenced by P6 generates the imaginary part of the term. The terms referenced by P5 can be input using only the first physical entry of the DTI entry (P5 < 0). The coefficients are defined by adjacent pairs of numbers on the DTI entry. The first number of the pair is an integer that names the coefficient being defined. For example, a value of 9 means the C9 value is to follow. The second number of a pair is a real number that defines the value of the coefficient. Zero coefficients need not be defined.

Bulk Data Entry: 1

2

3

4

5

AB

0

7

1

2

3.5

1

-5.2

DTI

AB

1

3

DTI

AB

2

DTI

AB

3

DTI

6

7

8

4

0.01

4

7.9

12

-21.8

13

6.6

9

1.0

8

9

10

For F1(I,J = 4J; I = 1, 100, J = 1200: MATGEN AB/Ml/8//100/200/-1 $

For M2(I,J = 3.5J − 5.21 = 1100J = 1200 : MATGEN AB/M2/8//100/200/0 $

For ; I = 100 and J = 1200: MATGEN AB/M3/8//100/200/2/1 $

For HILBERT(I,J) = 1.0/(I + J − 1); I,J = 1, 10: MATGEN AB/HILBERT/8//10/10/3 $ 3RD RECORD

Option P1 = 9 Generate a transformation between external and internal sequence matrices for g-set size matrices.

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Format: MATGEN

EQEXIN/TRANS/9/P2/P3 $

Input Data Block: EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

Output Data Block: TRANS

Transformation matrix

Parameters: T

EQEXIN table output by module GP1

P2

0

Output nontransposed factor where [UINT]=[MAT][UEXT]

1

Output transposed factor where [UEXT]=[MAT][UINT]

P3

Number of terms in g-set. The parameter LUSET, which is output by the GP1 module, contains this number in most solution sequences.

Examples: Transform a g-set size vector UGV to external sequence. MATGEN EQEXIN/INTEXT/9//LUSET $ MPYAD INTEXT,UGV,/UGVEXT/1 $

Transform an a-set size matrix to external sequence. VEC USET/VATOG/’G’/’A’/’COMP’ $ MERGE KAA,,,,VATOG,/KAGG/ $0 EXPAND TO $ GSIZE, INTERNAL SORT MATGEN EQEXIN/INTEXT/9/0/LUSET $ SMPYAD INTEXT,KAGG,INTEXT,,/KAAGEXT/3////1////6 $ $ (KAAGEXT) = TRANSPOSE(INTEXT)*(KAAG)* $ (INTEXT) ITS FORM IS 6 (SYMMETRIC)

By default in SOLs 100 through 200, PARAM, OLDSEQ is -1, which means this operation is not required.

Option P1 = 10 Not used.

Option P1 = 11 Generate a rectangular matrix, driven by USET table

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Format: MATGEN

USET/MAT/11/P2/P3/////////SET1/SET2 $

Input Data Block: USET

Degree-of-freedom set membership table for g-set

Output Data Block: MAT

Rectangular matrix based on the USET table

Parameters:. T

USET table output by module GP4

P2

Input-integer-default=0. Null matrix generation option flag. =1

Generate a null matrix P3 columns and a-set size rows.

≠0

Generate a null matrix with an identity sub-matrix based on SET1 and SET2 degree-of-freedom sets.

P3

Input-integer-default=0. Number of columns in MAT. Applies only to P2=1.

SET1

Input-character-default=‘A’ Degree-of-freedom set name which corresponds to the number of rows in MAT. Applies only when P2≠1.

SET2

Input-character-default=‘L’ Degree-of-freedom set name which corresponds to the number of columns in MAT. Applies only when P2≠1.

Remarks: If P2≠1, and one or both of the sets requested in SET1 and SET2 does not exist, MAT is returned purged, and P5 is returned with the value of -1. If MAT does exist, P5 is returned with the value of 0.

Option P1 = 12 Generate a rectangular matrix of prescribed properties.

Format: MATGEN

,/MAT/12/P2/P3/P4/P5/P6/P7/P8/P9 $

Input Data Blocks: None.

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Output Data Block: MAT

Rectangular matrix

Parameters: P2

Number of columns

P3

Number of rows

P4

Type of elements in the matrix: 1

Real single precision

2

Real double precision

3

Complex single precision

4

Complex double precision

P5

Density of the matrix times 10000

P6

Average string length

P7

Total number of strings in the matrix

P8

Number of null columns

P9

Average bandwidth

Remarks: 1. The default value for parameters P2, P3, P4, P5, and P7 is zero. Therefore, in order to successfully create the matrix, nonzero values for these parameters must be input. 2. The average string length is internally computed based on the other properties of the matrix. P6 is used only as a check. If the value computed is not the same as P6, a user warning message to that effect is issued. 3. In order to verify the properties of the output matrix, set DIAG 8 and check the matrix trailer information.

9.211 MATGPR Degree-of-freedom matrix printer Prints nonzero terms of matrices along with the external grid point and component identification numbers corresponding to the row and column position of each term.

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Formats: 1. For matrices with degrees of freedom that relate to grid or scalar points (g-set): MATGPR

BGPDT,USET,,MATRIX//COLNAM/ROWNAM/PRNTOPT/TINY/F1$

MATGPR

GPL,USET,SIL,MATRIX//COLNAM/ROWNAM/PRNTOPT/TINY/F1 $

2. For matrices with degrees of freedom that relate to grid, scalar or extra points (p-set): MATGPR

GPLD,USETD,SILD,MATRIX//COLNAM/ROWNAM/PRNTOPT/ TINY/F1 $

3. For matrices with degrees of freedom that relate to aerodynamic elements (ks-set): MATGPR

BGPDT,USET,,MATRIX//COLNAM/ROWNAM/PRNTOPT/ TINY/F1 $

4. Print a matrix in the format similar to DISPLACEMENT output with a user-defined column label and page header. MATGPR

BGPDT,USET,,MATRIX// ‘OFP‘/ROWNAM/PRNTOPT/TINY//// LCOLLBL1/LCOLLB2/LCOLLBL3/LCOLLBL4/ RCOLLBL1/RCOLLB2/RCOLLBL3/RCOLLBL4/ HDRLBL1/HDRLBL2/HDRLBL3/HDRLBL4/ HDRLBL5/HDRLBL6/HDRLBL7/HDRLBL8/ PUNCH/S,N,CARDNO $

Input Data Blocks: GPL

External grid/scalar point identification number list

GPLD

External grid/scalar/extra point identification number list. (GPL appended with extra point data.)

USET

Degree-of-freedom set membership table for g-set

USETD

Degree-of-freedom set membership table for p-set

SIL

Scalar index list

SILD

Scalar index list for the p-set

MATRIX

Any matrix related to degrees-of-freedom

BGPDT

Basic grid point definition table

BGPDT*

Family of basic grid point definition tables for all superelements

USET*

Family of USET tables

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Parameters: COLNAM

Input-character-no default. Set name for columns in MATRIX.

ROWNAM

Input-character-default = ’ ’ Set name for rows in MATRIX. If ROWNAM is blank, it defaults to COLNAM.

PRNTOPT

Input-character-default = ’ALL’. Must be one of the following values: Option

Action

NULL

Only null columns are identified.

ALL

Print all nonzero terms in matrix.

ALLP

Print numbers converted to magnitude/phase.

TINY

Real-default = 0.0. If F1 = 0 and TINY ≥ 0, printed output is provided only for those matrix terms, aij, that satisfy the relation |aij| ≥ TINY. If F1 = 0 and TINY ≤ 0, printed output is provided only for those matrix terms, aij, that satisfy the relation |aij| ≤ TINY. If TINY = 1.E37, MATGPR returns. If F1 is nonzero, see the following description of F1.

F1

Real-default = 0.0. If F1 is not zero, printed output is provided for only those matrix terms that satisfy aij > TINY or aij 0, the 6 x 6 single-precision matrix is the transformation matrix from the coordinate system with the coordinate ID = P3 to the basic system. If P3 points to a cylindrical or spherical coordinate system, the transformation location is at the origin of the P3 system. Scalar and extra points contain 1.0. If P3 = -1, the 6 x 6 single-precision matrix is the global-to-basic transformation for each grid point. Scalar and extra points contain 1.0. 2. If SIL is purged, the MATMOD uses LUSET for the size of the g-set. The assumption is made that only grids exist in the g-set. LUSET must not be zero if SIL is purged.

Examples: Transform KGG to another coordinate system. 1. Assume TRANS to be a 6 x 6 transformation matrix and KGG was formed using only one coordinate system (global coordinate system is the same at each grid point). Transform KGG using TRANS. MATMOD TRNSP SMPYAD

TRANS,SIL,,,,,,,,,,,,,/TRANSG,/5 $ TRANS/TRANSGT $ TRANSG,KGG,TRANSGT,,,/KGGPRIME/3 $

2. Assume KGG was formed using coordinate system 10 as the global coordinate system for all grid points. Transform KGG to the basic coordinate system. MATMOD TRNSP SMPYAD

CSTM,SIL,,,,,,,,,,,,,/TRANSG,/5//10 $ TRANSG/TRANSGT $ TRANSG,KGG,TRANSGT,,,/KGGBASIC/3 $

3. Assume KGG was formed using arbitrary coordinate systems as the global coordinate system for each grid point. Transform KGG to the basic coordinate system. MATMOD TRNSP SMPYAD

CSTM,SIL,BGPDT,,,,,,,,,,,,/TRANSG,/5//-1 $ TRANSG/TRANSGT $ TRANSG,KGG,TRANSGT,,,/KGGBASIC/3 $

Transform KGGBASIC coordinate system 10. MATMOD

CSTM,SIL,,,,,,,,,,,,,/TRANS10,/5//10 $

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TRNSP TRANS10/TRANST10T $ SMPYAD TRANS10T,KGGBASIC,TRANS10,,,/KGG10/3 $

Option P1 = 6 Find the maximum absolute value for each row over all columns of a matrix.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/6 $

Input Data Block: I1

Any matrix (real only)

Output Data Block: O1

Column vector with terms that represent the absolute maximum over all columns of I1 for each row

Example: Find the maximum displacements over all loading conditions. MATMOD

UG,,,,,,,,,,,,,,/UGMAX,/6 $

Option P1 = 7 Find the maximum absolute value for each column over all the rows of a matrix.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/7 $

Input Data Block: I1

Any matrix (real only)

Output Data Block: O1

Column vector with a term that represents the absolute maximum over all rows of I1 for each column

Example: Find the maximum displacement for each loading condition. MATMOD

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UG,,,,,,,,,,,,,,/MAXDISP,/7 $

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Option P1 = 8 Normalize matrix.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/8////S,N,NORMREAL/ S,N,NORMIMAG $

Input Data Block: I1

Any matrix (real or complex)

Output Data Block: O1

Matrix shaped like I1 with every term divided by the term in I1 with the largest absolute value

Parameters: NORMREAL

Output-real single precision. Set to the real part of the normalizing factor.

NORMIMAG

Output-real single precision. Set to the imaginary part of the normalizing factor if I1 is complex.

Option P1 = 9 Find the maximum (absolute magnitude) value of each of the three columns of the UHT-transient response solution matrix. (The columns of UHT represent displacement, velocity, and acceleration for each output time step.)

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/9 $

Input Data Block: I1

Transient response solution matrix consisting of H rows by three column matrices (which represent displacement, velocity, and acceleration for each output time step) appended to form a matrix H rows by three times the number of output time steps columns. (Real only). [[{u1} {n1} {a1}] [{u2} {n2} {a2}]...[{ui} {#i} {ai}]]

Output Data Block: O1

H-row by three column matrix of peak displacements, velocities, and accelerations

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Example: Find and output maximum transient response. MATMOD UHT,,,,,,,,,,,,,,/UHTMAX,/9 $ DDRMM CASEXX,UHTMAX,PHIP1,,,,/OUPMAX,,,,/ $ OFP OUPMAX,,,,// $

Option P1 = 10 Convert matrix I1 into its complex conjugate.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/10 $

Input Data Block: I1

Any matrix (real or complex)

Output Data Block: O1

Matrix shaped like I1 with every term converted to its complex conjugate

Example: Find the magnitude of terms of a complex vector. MATMOD CMPLX,,,,,,,,,,,,,,/CMPLXC,/10 $ ADD CMPLX,CMPLXC/CMPLXSQ///1 $ DIAGONAL CMPLXSQ/CMLPXMAG/’WHOLE’/0.5 $

Option P1 = 11 Form a new Basic Grid Point Definition Table (BGPDT) with grid locations that are given by I1.

Format: MATMOD

LOCVEC,BGPDT,,,,,,,,,,,,,/BGPDTN,/11 $

Input Data Blocks: LOCVEC

G-size vector with values that represent grid locations in the basic coordinate system

BGPDT

Basic grid point definition table

Output Data Block: BGPDTN

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New BGPDT table with grid point locations that are displaced by LOCVEC

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Example: Build new BGPDT table based on the deformed state. $ Convert displacement vector to basic $ coordinate system PARAML CSTM//’PRESENCE’////S,N,NOCSTM IF (NOCSTM > -1) THEN $ MATMOD CSTM,SIL,BGPDT,,,,,,,,,,,,/TRANS,/5//-1 $ MPYAD TRANS,UG/UGBASIC $ ELSE $ EQUIVX UG/UGBASIC/ALWAYS $ ENDIF $ $ Form vector containing new grid locations in $ basic coordinate system VECPLOT UGBASIC,BGPDT,SCSTM,CSTM,,,,/ LOCVEC/0/0/3 $ $ Generate new BGPDT MATMOD LOCVEC,BGPDT,,,,,,,,,,,,,/BGPDTNEW,/11 $

Option P1 = 12 Perform simultaneous null column search on up to three matrices.

Format: MATMOD

I1,I2,I3,,,,,,,,,,,,/O1,O2/12/S,N,NONULL/ NMATRIX $

Input Data Blocks: I1, I2, I3

Matrices to search for simultaneous null columns (real or complex)

Output Data Blocks: O1

Column vector which has 1.0 at those rows where all matrices selected for searching have null columns

O2

Square symmetric matrix which has 1.0 on the diagonal of those columns where all matrices selected for searching have null columns

Parameters: NONULL

Output-integer. Set to -1 if no simultaneous null columns found; otherwise, it is set to the number of simultaneous null columns.

NMATRIX

Input-integer-default=0. Number of matrices to be included in null column search.

Remarks: 1. I2 and I3 can be purged. 2. O2 can be purged.

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Example: Search for simultaneous null columns in the g-size mass, damping, and stiffness matrices and remove rows and columns corresponding to these columns. MATMOD MGG,BGG,KGG,,,,,,,,,,,,/PARTNULL,/12/S,N,NONULL/3 $ IF (NONULL > 0) THEN $ PARTN MGG,PARTNULL,/MGGNEW,,,/-1 $ EQUIVX MGGNEW/MGG/ALWAYS $ PARTN BGG,PARTNULL,/BGGNEW,,,/-1 $ EQUIVX BGGNEW/BGG/ALWAYS $ PARTN KGG,PARTNULL,/KGGNEW,,,/-1 $ EQUIVX KGGNEW/KGG/ALWAYS $ ENDIF $

Option P1 = 13 Copies any data block.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/13 $

Input Data Block: I1

Any data block (table or matrix)

Output Data Block: O1

Copy of I1

Remarks: COPY module is preferred over this option.

Option P1 = 14 Filter small magnitude terms from a matrix; more capabilities than option 2.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/14/PURGE/UPLOW/STRTR/ FILTER/RELFLT/TRUNC $

Input Data Block: I1

Matrix to be filtered (real or complex)

Output Data Block: O1

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Parameters: PURGE

Input-integer-default=0. If PURGE = 0, and the input matrix has no nonzero terms, the output matrix is purged. If PURGE≠ 0, and the input matrix has no nonzero terms, the output matrix is null.

UPLOW

Input-integer-default=0. If UPLOW < 0, all lower triangular terms are set to zero. If UPLOW > 0, all upper triangular terms are set to zero. If UPLOW = 0, the action of this parameter is ignored.

STRTR

Input-integer-default=0. If STRTR=0, string trailer is written.

FILTER

Input-real single precision-default=0.0. Terms in I1 with an absolute magnitude less than the absolute value of FILTER are set to zero.

RELFLT

Input-real single precision-default=0.0. If RELFLT≠ 0.0, terms of I1 are set to zero when

Equation 9-25. I1 must be square for this option TRUNC

Input-integer-default=0. If TRUNC ≠ 0, truncate terms of I1 accordingly

Equation 9-26.

Remarks: 1. If FILTER = 0.0, O1 is a copy of I1. 2. If relative filtering is desired, FILTER must be zero (default). 3. If FILTER ≠ 0 or RELFLT < 0, the absolute filter technique is used. 4. If I1 is not square and the relative filtering option is selected, FILTER is set to RELFLT and the absolute filtering technique is used. A user warning message is also issued.

Option P1 = 15 Not implemented.

Option P1 = 16 Put matrix into MATPOOL format, optional DMIG punched output.

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Format: MATMOD

I1,I2,,,,,,,,,,,,,/O1,/16/PNDMIG/USENAM/ TYPOUT////////CCHAR/MATNAM $

Input Data Blocks: I1

Any matrix of g-rows arranged in external (ascending by GRID ID) sequence. (Real or complex).

I2

EQEXIN table from module GP1

Output Data Block: O1

Table data block in MATPOOL format containing I1

Parameters PNDMIG

Input-integer-default=0. If PNDMIG≠0, I1 is printed in DMIG format to the punch output file (.pch).

USENAM

Input-integer-default=0. If USENAM≠0 and PNDMIG≠0, I1 is printed using the name defined in MATNAM.

TYPOUT

Input-integer-default=0. Default is to set DMIG precision to machine precision. The default can be overridden by specifying: 1

Real single-precision output

2

Real double-precision output

3

Complex single-precision output

4

Complex double-precision output

CCHAR

Input-character-default=blank. Continuation characters to be used for DMIG output. If nonblank continuation characters are specified, a maximum of 9999 DMIG entries can be printed for any single matrix. Only the first two characters of the nonblank mnemonic are used for the continuation string.

MATNAM

Input-character-default=blank. Matrix name to use for I1. Only valid when USENAM≠0 and PNDMIG≠0.

Remarks: 1. I1 must be a g-row size matrix arranged in external sequence (see PARAM, OLDSEQ, and MATGEN Option 9). The rows are always labeled with the external sequence (grid or scalar IDs and component numbers). If the input matrix form is 1 (square) or 6 (symmetric) the columns are also labeled with the external sequence, and the IFO entry on the generated DMIG entry is set to 1 or 6. If the form is 6, only the terms in one triangle are output. If the

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input matrix form is 2 (rectangular form), the columns are labeled sequentially, starting with unity. The IFO is set to 9. If the form is not 1, 2, or 6, the module returns with no output. 2. EQEXIN table must not be purged.

Example: Output KGG and PG matrices in MATPOOL formatted table and punch to DMIG Bulk Data entries (MATGEN Option 9 is being used to resequence them from internal to external sort). MATGEN MPYAD MPYAD MATMOD MPYAD MATMOD MATMOD

EQEXIN/INTEXT/9/0/LUSET $ INTEXT,KGG,/KGGE/1 $ KGGE,INTEXT,/KGGEXT $ KGGEXT,EQEXIN,,,,,,,,,,,,,/MATPOOL1,/16/1 $ INTEXT,PG,/PGEXT/1 $ PGEXT,EQEXIN,,,,,,,,,,,,,/MATPOOL2,/16/1 $ KGGEXT,EQEXIN,,,,,,,,,,,,,/MATPOOL1,/16/1/1//////////KNAME $

Option P1 = 17 Generate a g-size partitioning vector from a user-defined set of grid and/or scalar points or from a user-supplied bit position that designates one of the USET sets.

Format: MATMOD

EQEXIN,USET,SIL,CASECC,GRDLST,,,,,,,,,,/CP,/17/UBIT/SETFLG/ S,N,NOCP////////SETSTR1/SETSTR2/SETSTR3/SETSTR4 $

Input Data Blocks: EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

USET

Degree-of-freedom set membership table for g-set

SIL

Scalar index list

CASECC

Table of Case Control command images

GRDLST

Optional line of allowable grid and scalar points. (Real single-precision vector.) If purged, all are allowed. Only applies to SETFLG≠0 and UBIT=0.

Output Data Block: CP

Column partitioning vector

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Parameters: UBIT

Input-integer-default=0. Obsolete method for set selection. For a more user-friendly method, use SETSTRi. In order to select specific sets for UBIT, add the corresponding decimal equivalent numbers from the table below. For example, sets R, O, and M, UBIT=8+4+1=13. For supersets, add the decimal equivalent numbers of the mutually exclusive sets which are contained in the superset. For example, set S combines the SB and SG set and therefore UBIT=1024+512=1536. The presence of any grid point degree of freedom in the associated sets causes all degrees of freedom associated with that grid point to be given a value of 1.0 in the output vector.

SETFLG

SetName

DecimalEquivalentNumber

Q

4194304

BE

2097152

C

1048576

K

262144

SA

131072

E

2048

SB

1024

SG

512

R

8

O

4

BF

2

M

1 Input-integer-default=0. If SETFLG ≠ 0, SETFLG selects a set of grid point identification numbers of which all degrees of freedom associated with each point are assigned a value of 1.0 in the corresponding row of CP. If no SET command is found, the UBIT parameter is used. If SETFLG>0, the PARTN=SID Case Control command selects the SET command. If SETFLG -1) THEN $ A,CPARTN,RPARTN/ANEW/SYM $ ANEW/A/ALWAYS $

Option P1 = 26 Used internally for development testing.

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Option P1 = 27 Convert a diagonal matrix (form 3) to a symmetric matrix (form 6).

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,/27 $

Input Data Block: I1

Diagonal matrix of form 3 (real or complex)

Output Data Block: O1

Symmetric matrix of form 6 containing diagonal terms of I1

Remarks: 1. Form 3 matrices are not output by any module. They are only allowed as input by the INPUTT2, INPUTT4, and DMIIN modules. 2. The SMPYAD, MPYAD, and ADD modules do not accept form 3 matrices. The matrices should now be converted to form 6 before use in these modules.

Example: DMIIN MATMOD

DMI,DMINDX/A3,,,,,,,,, $ A3,,,,,,,,,,,,,,/A6,/27 $

where A3 is the DMI matrix defined by the Bulk Data entries DMI,A3,0,3,1,1,,4,1 DMI,A3,1,2,2.0,3.0,4.0

and A6 is the matrix

Option P1 = 28 Convert the first column of a matrix to a symmetric matrix (form 6) with the terms of the first column along the diagonal and off-diagonal terms set to zero.

Format: MATMOD

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I1,,,,,,,,,,,,,,/O1,/28 $

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Input Data Block: I1

Any matrix of form 1, 2, or 6 (real or complex)

Output Data Block: O1

Symmetric matrix (form 6) with terms of the first column of I1 along the diagonal and off-diagonal terms set to zero.

Example: MATMOD

B,,,,,,,,,,,,,,/BDIAG,/28 $

If B is the matrix

Figure 9-2. BDIAG is

Figure 9-3.

Option P1 = 29 Make output requests consistent for superelement combined output.

Format: MATMOD

CASECC,,,,,,,,,,,,,,/XCASECC,/29 $

Input Data Blocks: CASECC

Table of Case Control command images

Output Data Blocks: XCASECC

Modified table of Case Control command images

Remarks: This only makes sense with PARAM,SECOMB,YES.

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Option P1 = 30 Print data blocks or a portion of data blocks as a table of hexadecimal values.

Format: MATMOD

I1,I2,I3,I4,I5,I6,,,,,,,,,/,/30/BBLK/EBLK $

Input Data Blocks: Ii

Any data block (matrix or table)

Parameters: BBLK

Input-integer-default=1. Beginning GINO block number.

EBLK

Input-integer-default=-1. Ending GINO block number. Default value implies the total number of blocks.

Option P1=31 Writes the bit map of a matrix to the punch file.

Format: MATMOD

MAT,,,,,,,,,,,,,,/,/31/MAXSIZ $

Input Data Block: MAT

Any matrix

Output Data Block: None.

Parameter: MAXSIZ

Input-integer-default=0. Maximum size of the bit map matrix (row and/or column)

Option P1=32 Convert tables created by DRMH1 into DTI Bulk Data entry format and write to the punch file. Also converts DRMH1 directory tables in DTI Bulk Data entry format into DRMH1 output table format.

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Format: MATMOD

TXY,,,,,,,,,,,,,,/TOUT,/32/CONVERT $

Input Data Block: TXY

DRMH1 directory table in DTI or table data block format

Output Data Block: TOUT

DRMH1 directory table in table data block format or DTI format

Parameter: CONVERT

Input-integer-default=0. Convert option. 0

Table data block format to DTI format

1

DDTI to table data block format

Remarks: Table record 3 is all character and reading DTI entries produces all numbers. Therefore, CONVERT=1 converts the DTI numbers to character values.

Option P1=33 Create a single column matrix from the frequency response output list table, FOL. The frequencies are also converted to radian units.

Format: MATMOD

FOL,,,,,,,,,,,,,,/FOLMAT,/33 $

Input Data Block: FOL

Frequency response frequency output list

Output Data Block: FOLMAT

Matrix of frequencies in radian units

Parameters: None.

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Option P1=34 Extract the real and imaginary parts of complex matrix into two real matrices.

Format: MATMOD

CMAT,,,,,,,,,,,,,,/RMAT,IMAT/34//PREC $

Input Data Block: CMAT

Complex matrix

Output Data Blocks: RMAT

Matrix containing real part of CMAT

IMAT

Matrix containing imaginary part of CMAT

Parameter: PREC

Input-integer-default=0. Precision of output matrices. 0

Machine-precision (default)

1

Single

2

Double

Option P1=35 Sorts row term values in a selected column of the input matrix and produces a list vector and/or a Boolean matrix that contains the indices of the sorted terms.

Format: MATMOD

IM,,,,,,,,,,,,,,/ SORTLIST,SORTBOOL/S,N,P1/COLNUM/S,N,PRESORT/ SORTOPT/// NKEYS $

Input Data Block: IM

Any matrix

Output Data Blocks: SORTLIST

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Vector consisting of the row numbers of the original positions of the sorted terms

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SORTBOOL

Square matrix containing unity at a row position in the column associated with the sorted row terms

Parameters: P1

Input/output-integer-no default. On output, P1=-1 if the input matrix is purged or both output data blocks are purged.

COLNUM

Input-integer-default=0. Selects the column number of the input matrix that is sorted to produce SORTLIST and SORTBOOL. Default selects the first column.

PRESORT

Output-integer-default=0 Pre-sort flag. Set to -1 if column is already sorted.

SORTOPT

Input-integer-default=0. Sort option specification.

NKEYS

-2

Absolute value in descending order

-1

Algebraic value in descending order

0

Implies SORTOPT=1 if IM is real, and SORTOPT=2 if IM is complex.

1

Algebraic value in ascending order

2

Absolute value in ascending order

Input-integer-default=1. Duplicate value sort option specification. 1

Single key sort

2

Double key sort to maintain original order of terms in case of duplicate terms

Remarks: For complex matrices, only SORTOPT=2 or -2 is allowed.

Example: Given the input matrix, IM, generate an algebraic ascending order sort. The input matrix and its sorted order (algebraically ascending) are:

IM =

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The MATMOD call looks like this: P1=35 $ MATMOD

IM,,,,,,,,,,,,,,/LIST,BOOL/S,N,P1//S,N,SORTED////2

$

and the output matrix LIST for NKEYS=2 contains LIST =

For NKEYS=1, it is equally likely that the indices for equal values are in a different order. For example, if the MATMOD call statement were P1=35 $ MATMOD

IM,,,,,,,,,,,,,,/LIST,BOOL/S,N,P1//S,N,SORTED////1

$

the output matrix LIST for NKEYS=1 contain either LIST =

or LIST =

since there are duplicate terms (0.0‘s) in the input matrix column and a single key sort was used. The Boolean square matrix contains unit values in the appropriate positions so that it can be used to create the sorted input matrix by means of a simple matrix multiply as in: MPYAD

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producing the sorted IM matrix, IMS, as IMS =

Remarks: 1. If the matrix input into this option contains more than one column and SORTBOOL is used subsequently to operate on this matrix, all columns have their rows re-ordered according to the sort obtained from the column processed by the MATMOD operation. In this case, the column that was selected during the MATMOD operation to produce the sorted ordering is guaranteed in sort. Other columns may or may not have their rows in sorted order. 2. The output data blocks are in machine precision, regardless of the precision of the input matrix. 3. NKEYS=2 provides a more repeatable sort in the presence of equal values in the input, at the cost of longer run times. A test on a typical vector showed a difference of a factor of approximately ten. If repeatability is not essential, NKEYS=1 is the preferred choice.

Option P1=36 Reduce the GRID record in the GEOM1 table to the entries corresponding to grid identification numbers specified in a Case Control set.

Format: MATMOD

GEOM1,CASECC,,,,,,,,,,,,,/GEOM1R,/36/GRIDSET/S,N,NOGEOM1 $

Input Data Blocks: GEOM1

Table of Bulk Data entry images related to geometry

CASECC

Table of Case Control command selections

Output Data Block: GEOM1R

GEOM1 table with reduced GRID record

Parameters: GRIDSET

Input-integer. SET Case Control command identification number which contains a list grid point identification numbers.

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Output-integer. Processing status flag. +1 No grid data found matching gridset. 0

GRIDSET found and contents match some GRIDs in GEOM1.

-1 GRIDSET found and contents matches all GRIDs in GEOM1.

Remarks: Only the GRID record is processed and all other GEOM1 records are copied as is to GEOM1R.

Option P1=37 Reduce the element and SPOINT records in the GEOM2 table to the entries corresponding to element or SPOINT identification numbers specified in a Case Control set.

Format: MATMOD

GEOM2,CASECC,,,,,,,,,,,,,/GEOM2R,/37/ ELEMSET/GRIDSET/S,N,NOGEOM2 $

Input Data Blocks: GEOM2

Table of Bulk Data entry images related to geometry

CASECC

Table of Case Control command selections

Output Data Block: GEOM2R

GEOM2 table with reduced element record

Parameters: ELEMSET

Input-integer. SET Case Control command identification number which contains a list element point identification numbers.

GRIDSET

Input-integer. SET Case Control command identification number which contains a list SPOINT identification numbers.

NOGEOM2

Output-integer. Processing status flag. +1 No element and SPOINTs found matching ELEMSET and GRIDSET. 0

ELEMSET and GRIDSET found and contents match some elements and SPOINTs in GEOM2.

-1 ELEMSET and GRIDSET found and contents match all elements and SPOINTs in GEOM2.

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Option P1=38 Reduce the records in the EST table to the entries corresponding to element numbers specified in a Case Control set.

Format: MATMOD

EST,CASECC,,,,,,,,,,,,,/ESTR,/38/ ELEMSET/GRIDSET/S,N,NOEST $

Input Data Blocks: EST

Table of Bulk Data entry images related to geometry

CASECC

Table of Case Control command selections.

Output Data Block: ESTR

EST table with reduced records

Parameters: ELEMSET

Input-integer. SET Case Control command identification number that contains a list element point identification numbers.

GRIDSET

Input-integer. SET Case Control command identification number which contains a list grid point identification numbers.

NOEST

Output-integer. Processing status flag. +1 No element found matching contents of ELEMSET 0

ELEMSET found and contents match some elements in EST

-1 ELEMSET and contents match all elements and SPOINTs in EST

Option P1=39 Remove and identify explicit zero terms in a matrix.

Format: MATMOD

I1,,,,,,,,,,,,,,/O1,O2/39/S,N,NOXPLZER $

Input Data Block: I1

Any matrix

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Output Data Blocks: O1

Matrix I1 with explicit zero terms removed

O2

Matrix containing a 1.0 at the row and column, where an explicit zero was found in I1

Parameter: NOXPLZER

Output-integer. Explicit zero existence flag. Set to -1 if no explicit zeros are found.

Option P1=40 Remove unused q-set degrees-of-freedom from USET.

Format: MATMOD

USET,VAXW,,,,,,,,,,,,,/USETN,VAXWN/40 $

Input Data Block: USET

Degree-of-freedom set membership table for g-set.

VAXW

Column vector for a-set degrees of freedom which has a 1.0 at those locations where a-set structural matrices are null.

Output Data Blocks: USETN

New degree-of-freedom set membership table for g-set (with unused q-set degrees of freedom removed).

VAXWN

Modified VAXW corresponding to USETN.

Option P1=41 Generate a partitioning vector from a set of grid points defined in the Bulk Data Section on a ROTORG card.

Format: MATMOD

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EQEXIN,USET,SIL,CASECC,DYNAMICS,,,,,,,,,,/PARTV,/41/PFLAG/ROTGID/NOVEC $

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Input Data Block: EQEXIN

Equivalence table between external and internal grid/scalar identification numbers.

USET

Degree-of-freedom set membership table for g-set.

SIL

Scalar index list.

CASECC

Table of Case Control command images.

DYNAMICS

Table of Bulk Data entry images related to dynamics.

Output Data Blocks: PARTV

Column partitioning vector.

Parameters: PFLAG

Input-integer-default=0. Processing flag. If 0, process ROTORG bulk data entries. If 1, process ROTORB bulk data entries.

ROTGID

Input-integer. ROTGID must be less than zero. The absolute value of ROTGID selects the ROTORG or ROTORB Bulk Data card containing a set of grid point identification numbers. Six degrees of freedom will be associated to each point by assigning six values of 1.0 in the corresponding row of PARTV.

NOVEC

Output-integer-no default. Set to 0 if PARTV created; set to -1 if PARTV is not created (i.e. ROTORG or ROTORB bulk data entry doesn’t exist).

Remarks: 1. None of the data blocks may be purged.

Example: MATMOD EQEXIN,USET,SIL,CASECC,DYNAMICS,,,,,,,,,,/PARTG,/41/0/-11/NOVEC $ The Bulk Data Section contains: ROTORG 11 1 3 THRU 5 7 The resulting partitioning vector PARTG: 1 0 1 1 1 0 1

Option P1=42 Generate a partitioning vector from a set of data defined in the Bulk Data Section on SOL 200.

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Format: MATMOD

BGPDT,EQEXIN,SIL,CASECC,EDOM,EPT,EPTABF,GEOM2,XYCDB,PARTV,,,,,/ RGPV,/42/NEPT/NOSE $

Input Data Block: BGPDT

Basic grid point definition table.

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers.

SIL

Scalar index list.

CASECC

Table of Case Control command images.

EDOM

Table of Bulk Data entries related to design sensitivity and optimization.

EPT

Table of Bulk Data entry related to element properties.

EPTABF

Family of tables of designed property attributes.

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar point.

XYCDB

Table of X-Y plotting commands.

PARTV

Partitioning vector output by MATMOD with option P1=44.

Output Data Blocks: RGPV

Row partitioning vector.

Parameters: NEPT

Input-integer-default=0. The number of EPOINT used in FE model.

NOSE

Input-integer default=0. NOSE should be set to 1 if superelement is used.

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Remarks: 1. The partitioning vector RGPV is generated from the following data defined in the Bulk Data: - grids and elements defined in set - properties defined in DESVAR - grids, elements, properties defined in DRESP. 2. Option 42 does not support shape optimization. 3. Option 42 does not support material optimization. 4. Option 42 does not support XYPLOT, PLOT, POST output request.

Example: The partitioning vector RGPV includes 0 or 1: 1011101

Option P1=43 Generate a partitioning vector from a set of modal indices defined in the Case Control Section on a SET card referenced to by a MODSEL card.

Format: MATMOD

EQEXIN,USET,SIL,CASECC,DYNAMICS,,,,,,,,,,/PARTMS1,/43/NEIGV/MODSEL/NOVEC $

Input Data Block: EQEXIN

Equivalence table between external and internal grid/scalar identification numbers.

USET

Degree-of-freedom set membership table for g-set.

SIL

Scalar index list.

CASECC

Table of Case Control command images.

DYNAMICS

Table of Bulk Data entry images related to dynamics.

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Output Data Blocks: PARTMS1

Column partitioning vector.

Parameters: Parameter 2 not used at this time. NEIGV

Input-integer. When the Case Control MODSEL card references a Case Control "SET = ALL" card the value of NEIGV will be used to determine the set of grid point identification numbers. Thus the set will contain grids 1 to n where n equals the value of NEIGV.

MODSEL

Input-integer. MODSEL must be less than zero. The absolute value of MODSEL selects a Case Control MODSEL card which points to a Case Control SET card containing a set of grid point identification numbers. Each point in the set will be assigned a value of 1.0 in the corresponding row of PARTMS1.

NOVEC

Output-integer. NOVEC will be set to -1 if the partitioning vector is null or cannot be generated. Otherwise, it will be set to zero.

Remarks: 1. None of the data blocks may be purged. 2. MODSEL parameter must be a negative integer value less than zero.

Example: MATMOD EQEXIN,USET,SIL,CASECC,DYNAMICS,,,,,,,,,,/PARTMS1,/43/0/-10/NOVEC $ The Case Control Section contains: SET 10 = 1, 3 THRU 5, 7 MODSEL = 10 The resulting partitioning vector PARTMS1: 1 0 1 1 1 0 1

Option P1=44 Create a g-set partitioning vector for sparse data recovery based on the output requests in the case control section. This option is only valid for frequency and transient response output requests.

Format: MATMOD

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BGPDTS,SILS,CASES,USETS,EPTS,GEOM2S,EQEXINS, XYCDB,GMTG,GOATG,GPECT,PCDB,POSTCDB,SETMC,EDT/PARTV, /44/NOEPT/NOSE/IWHO///NUMPAN $

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Input Data Blocks: BGPDTS

Basic grid point definition table.

SILS

Scalar index list.

CASES

Table of Case Control command images.

USETS

Table of degree-of-freedom sets.

EPTS

Element property table.

GEOM2S

Table of bulk data entries related to element connectivity.

EQEXINS

Table of external and internal grid/scalar numbers.

XYCDB

Table of XY plotting commands.

GMTG

Transpose of GM (multipoint constraint transformation matrix; m-set by n-set) where the n-set dimension has been expanded to g-set size.

GOATG

Transpost of GOA (o-set to a-set transformation) which has been expanded to the g-set.

GPECT

Grid point element connection table.

PCDB

Table of model plotting commands.

POSTCDB

Table of OUTPUT(POST) commands.

SETMC

Modal contribution set definitions

EDT

Element deformation table. Contains PANEL, SET1, and SET3 bulk entries.

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Output Data Block: PARTV

Sparse data recovery partitioning vector (length is g-set). Values of 1 indicate retained dof; values of 0 indicate ignored dof.

Parameters: NOEPT

Input-integer default=0. Number of EPOINTs to process.

NOSE

Input-integer default=0. NOSE should be set to 1 if superelement is used.

IWHO

Input-integer default=0. IWHO should be set to 0 for enforced motion; set to 1 for SOL 111 or SOL 112 with superelements.

NUMPAN

Input-integer default=0. Number of acoustic panels.

Remarks: 1. All data blocks must exist except for GMTG, GOATG, PCDB, and POSTCDB. If any of the required data blocks are purged, the module will not produce PARTV. 2. GMTG must exist in order to process m-set degrees-of-freedom. GOATG must exist to process o-set degrees-of-freedom. PCDB and POSTCDB must exist to process model plotting commands and OUTPUT(POST) commands, respectively. 3. If the user requests ‘ALL’ for any of the supported case control output requests, PARTV will contain all values of 1 and the SPARSEDR system cell (421) will be reset to 0, indicating that sparse data recovery is OFF. 4. The supported case control output requests are: a. b. c. d. e. f. g. h. I. j. k. l. m. n.

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DISPLACEMENT VELOCITY ACCELERATION OLOAD STRESS/ELSTRESS STRAIN/ELSTRAIN FORCE/ELFORCE EDE EKE ESE XYPEAK XYPRINT XYPLOT XYPUNCH

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o. p. q. r. s. t. u.

MPCFORCE SPCFORCE GPFORCE GPSTRESS GPSTRAIN MODCON PANCON

Option P1=45 Construct XCASECC by selecting the desired records of CASECC.

Format: MATMOD

CASECC,,,,,,,,,,,,,,/XCASECC,/45/P2/P3/P4 $

Input Data Blocks: CASECC

Table of Case Control command images.

Output Data Block: XCASECC

Table of Case Control command images for each processor in DMP environment

Parameters: P2

Input-integer default=0. Skip P2 records from the beginning of CASECC.

P3

Input-integer default=0. Copy the subsequent P3 records to XCASECC after P2 records.

P4

Input-integer default=0. The remaining number of records after P3 records is copied to XCASECC.

Remarks: Example: Extract 2, 3, and 4th record from CASECC that has 6 records. MATMOD CASECC,,,,,,,,,,,,,,/XCASECC,/45/1/3/2 $

Option P1=46 Used internally for development.

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Option P1=47 Used internally for development.

Option P1=48 Used internally for development.

Option P1=49 Modify Case Control to create data type-specific set and reference.

Format: MATMOD

CASECC,,,,,,,,,,,,,,/CASEX,/49/IDTYPE/IELEM $

Input Data Blocks: CASECC

Case Control data block

Output Data Block: CASEX

Modified Case Control data block

Parameters: IDTYPE

Integer-input-default=0. Data type code: 0=stress, 1=strain, 2=element force.

IELEM

Integer-input-default=0. Element ID.

Option P1=50 Extract item-code specific data from a modal contributions output data block and create a column vector.

Format: MATMOD

ORES,,,,,,,,,,,,,,/VECT,/50/ITMCOD $

Input Data Blocks: ORES

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Descriptions of DMAP Modules and Statements

Output Data Block: VECT

Vector of modal contributions results

Parameters: ITMCOD

Integer-input-default=0. Element item code.

Option P1=51 Generate a surface spline to connect two point fields in close proximity, but not necessarily coincident.

Format: MATMOD

IM1,IM2,,,,,,,,,,,,,/OM1,/51/P2/P3/P4/P5 $

Input Data Blocks: IM1

Matrix of independent points. 3 rows by NI columns. NI = number of independent points.

IM2

Matrix of dependent points. 3 rows by ND columns. ND = number of dependent points.

Output Data Block: OM1

Transformation matrix describing the surface spline connection. NI rows by ND columns. NI = number of independent points. ND = number of dependent points.

Parameters: P2,P3

P4

Input-integer default=0,0. Used to define boundary condition of the surface spline. 0,0

Surface spline is unconstrained at the edges.

-1,0

A zero moment X-directional end condition is imposed on the surface spline.

0,-1

A zero moment Y-directional end condition is imposed on the surface spline.

Input-integer default=1. Coordinate pair selection.

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1

XY point pairs are used for the surface spline fit.

2

XZ point pairs are used for the surface spline fit.

3

YZ point pairs are used for the surface spline fit.

Input-real default=1.0. Used to stiffen springs applied during the surface spline generation.

Option P1=52 Used internally for development.

Option P1=53 Generate a g-size partitioning vector and a list of grid IDs that correspond to the structural grids that are a part of an acoustic coupling matrix.

Format: MATMOD

EQEXIN,USET,SIL,AG0MAX,,,,,,,,,,,/PARTV,ACGRIDS/53/// S,N,NOPARTV $

Input Data Blocks: EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

USET

Degree-of-freedom set membership table for g-set

SIL

Scalar index list

AG0MAX

Column matrix of maximum values in each row of the AG0 matrix (usually derived using MATMOD option 6)

Output Data Block: PARTV

Column partitioning vector for all 6 degrees-of-freedom of grids which are a part of the acoustic coupling

ACGRIDS

Column vector containing the grid IDs of the grids which are a part of the acoustic coupling; the grid IDs are represented as real values

Parameters: NOPARTV

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Output-integer. NOPARTV is set to -1 if the output data blocks are null or cannot be generated. Otherwise, it is set to zero.

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Remarks: 1. None of the data blocks can be purged.

Option P1=54 Used internally for development.

Option P1=55 Compute modal damping coefficients, as in the GKAM module.

Format: MATMOD

LAMA,CASECC,DIT,,,,,,,,,,,,/ZETA,/55 $

Input Data Block: LAMA

Normal modes eigenvalue summary table.

CASECC

Table of Case Control command images.

DIT

Table of TABLEij Bulk Data entry images.

Output Data Block: ZETA

Diagonal matrix of modal damping coefficients as produced by the GKAM module.

Option P1=56 Replace the value of, or add a value to, a single term in a matrix.

Format: MATMOD

I1,,,,,,,,,,,,,,/ O1,/ 56/ICOL/IROW/TYPE/REAL//NCOL/NROW/////////REALD/CMPLX/CMPLXD $

Input Data Block: I1

A matrix. May be purged. See NCOL.

Output Data Block: O1

Modified I1 matrix.

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Parameters: ICOL

Column number.

IROW

Row number.

TYPE

Type of value to be replaced or added. 1 Replace current value with REAL. 2 Replace current value with REALD. 3 Replace current value with CMPLX. 4 Replace current value with CMPLXD. -1 Add REAL to current value. -2 Add REALD to current value. -3 Add CMPLX to current value. -4 Add CMPLXD to current value.

REAL

Real single-precision value.

NCOL

Number of columns in O1 if I1 is purged. Default=ICOL.

NROW

Number of rows in O1 if I1 is purged. Default=IROW.

REALD

Real double-precision value.

CMPLX

Complex single-precision value.

CMPLXD

Complex double-precision value.

Example: In matrix A, add 10.5 to the value of a32 (the element of the matrix at column 2 and row 3): MATMOD A,,,,,,,,,,,,,,/A1,/56/2/3/—1/10.5 $

Option P1=57 Modify frequency list table TOL.

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Format: MATMOD

TOL,,,,,,,,,,,,,,/ TOL1,/ 57/P2/P3 $

Input Data Block: TOL

Table of frequencies in transient response.

Output Data Block: TOL1

Truncated table of frequencies containing values ranging between P2 and P3.

Parameters: P2

Input-integer-default = 0. First frequency table entry to copy from TOL to TOL1.

P3

Input-integer-default = 0. Last frequency table entry to copy from TOL to TOL1.

9.214 MATPCH Punches contents of Matrix Data Blocks Punches the contents of matrix data blocks onto DMI Bulk Data entries.

Format: MATPCH

I1,I2,I3,14,I5//IVNIT/N1/N2/N3/N4/N5 $

Input Data Blocks: Ii

Any real matrix data block

Output Data Blocks: None.

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Parameters: IVNIT

Input-integer-default=0. Fortran unit number. If this parameter is negative, an echo of the DMI Bulk Data entries generated is printed on the FORTRAN unit given by the absolute value of PRINTOPT.

Ni

Input-character-default=blank. Continuation entry prefix. Used to form a unique continuation string for the DMI Bulk Data entries. For example, if Ni=’xx’, this produces continuations of the form (xx 1), (xx 2), and so on. The default value causes the blank continuation option to be used. See Remark 4 if explicit continuations are desired.

Remarks: 1. The nonzero elements of each matrix are punched on double-field DMI entries as shown in the example below. The name of the matrix is obtained from the header record of the data block. Field 10 contains the three-character parameter value in columns 74 through 76 and an incremented integer record count in columns 77 through 80 if nondefault values are used for the Ni parameters. 2. Double precision matrices are converted to single precision. Only the real part of complex matrices are used. 3. All matrices are output on double-field entries in single precision. 4. If Ni is specified, Ni must be different for each corresponding input matrix. Also, the maximum number of records that can be punched is 99999. If full square matrices are considered, a maximum order of 629 is allowed. If matrices larger than this are desired, use the OUTPUT2 or OUTPUT4 modules to produce a FORTRAN readable file. 5. Only sufficiently small nonpurged data blocks are punched onto DMI Bulk Data entries.

Example: Let the data block MAT contain the matrix

Figure 9-4. The DMAP statement MATPCH MAT// $

produces the following DMI entries:

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1

2

DMI

MAT

DMI

MAT

*

3 0

4 2

5 1

6

7

8

9

2

5

1

1

1.000000E 00

3

2.000000E 00

5

3.000000E 00

DMI*

MAT

2

3

4.000000E 00

*

5.000000E 00

DMI*

MAT

3

1

6.000000E 00

*

7.000000E 00

5

8.000000E 00

DMI*

MAT

6

4

10

6

9.000000E 00

9.215 MATPRN General matrix printer Prints general matrix data blocks.

Format: MATPRN

M1,M2,M3,M4,M5/ $

Input Data Blocks: Mi

Matrix data blocks, any of which can be purged (real or complex)

Remarks: 1. Any or all input data blocks can be purged. 2. If any data block is not a matrix, it is printed as if it were a table. 3. MATPRN prints the row index for the term that begins each line of printout. 4. MATPRN does not print out two or more consecutive lines of zeroes, but instead issues a message of the form: ROW POSITIONS xxxx THRU yyyy NOT PRINTED – ALL = 0.0. 5. If DIAG 30 is set by the DIAGON function before MATPRN (see Example 3), and turned off after MATPRN, most of the digits of the internal representations are printed. Normally, the output is truncated to five or six digits. 6. For large, sparse matrices with scattered terms, Siemens PLM Software recommends using either the MATPRT or MATGPR modules.

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Examples: 1. MATPRN

KGG/$

MATPRN

KGG,PL,PG,BGG,UPV//$

2.

3. DIAGON(30) $ PRINT EXTENDED PRECISION MATPRN KGG/$ DIAGOFF(30) $

9.216 MATPRT Matrix printer

Format: MATPRT

MATRIX//PRNTLABL/PRNTFLAG $

Input Data Block: MATRIX

Matrix data block to be printed. If [X] is purged, nothing is done.

Parameters: PRNTLABL

Integer-input-default=0. Print label. If PRNTFLG=1, the matrix is labeled with “ROW n”; otherwise it is labeled with “COLUMN n.”

PRNTFLAG

Integer-input-default=0. Print flag. If PRNTFLAG < 0, do not print [X]; Y ≥ 0, print [X].

Remarks: Each column (or row) of the matrix is broken into groups of six terms (3 terms if complex) per printed line. If all the terms in a group are 0, the line is not printed. If the entire column (or row) is 0, it is not printed. If the entire matrix is null, it is not printed.

Example: Print the mass matrix. MATPRT

MGG// $

9.217 MATREDU Reduces square matrix from g-set to a-set or p-set to d-set

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Reduces a square matrix from the g-set to the a-set, or p-set to the d-set. Optionally produces the s-set by f-set partition following multipoint constraint elimination and reduction.

Format: MATREDU

{XGG or XPP},{USET or USETD},{GM or GMD},{GOA or GOD}/ {XAA or XDD},XSF,XSS/ S,N,{NOXGG OR NOXPP} $

Input Data Blocks: XGG

Square matrix in g-set

XPP

Square matrix in p-set

USET

Degree-of-freedom set membership table for g-set

USETD

Degree-of-freedom set membership table for p-set

GM

Multipoint constraint transformation matrix, m-set by n-set

GMD

Multipoint constraint transformation matrix with extra points, m-set by ne-set

GOA

Omitted degree-of-freedom transformation matrix, o-set by a-set

GOD

Omitted degree-of-freedom transformation matrix with extra points, o-set by d-set

Output Data Blocks: XAA

Reduced square matrix in a-set

XDD

Reduced square matrix in d-set

XSF

S-set by f-set matrix partition of XGG or XPP after multipoint constraint elimination and reduction

XSS

S-set by s-set matrix partition of XGG or XPP after multipoint constraint elimination and reduction

Parameters: NOXGG

Output-integer-default=1. XGG existence flag. Set to -1 if XGG does not exist.

NOXPP

Output-integer-default=1. XPP existence flag. Set to -1 if XPP does not exist.

Remarks: 1. If XGG or XPP is not symmetric, the unsymmetric formulation of reduction is used.

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2. XGG or XPP can be purged, in which case MATREDU returns with NOXAA=-1 or NOXDD=-1. 3. GM (or GMD) and GOA (or GOD) cannot be purged unless their m-set and o-set degrees-of-freedom do not exist. 4. XSF can be purged. 5. The method of reduction is equivalent to a combination of the DMAP modules UPARTN, UMERGE1, SMPYAD, and MCE2.

9.218 MCE1 Creates multipoint constraint transformation matrix

Format: MCE1

USET,RMG/ GM $

Input Data Blocks: USET

Degree-of-freedom set membership table for g-set

RMG

Multipoint constraint equation matrix

Output Data Block: GM

Multipoint constraint transformation matrix, m-set by n-set

Parameters: None.

9.219 MCE2 Performs multipoint constraint elimination and reduction Performs multipoint constraint elimination and reduction on up to four g-set size square matrices.

Format: MCE2

USET,GM,XGG1,XGG2,XGG3,XGG4/ XNN1,XNN2,XNN3,XNN4 $

Input Data Blocks: USET

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Degree-of-freedom set membership table for g-set

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GM

Multipoint constraint transformation matrix, m-set by n-set

XGGi

Square matrices in g-set

Output Data Blocks: XNNi

Square matrices in n-set

Parameters: None.

Remarks: Any or all of XGGi and XNNi can be purged. However, if any of XGGi is specified, the corresponding XNNi must also be specified.

Example: Reduce Kgg to Knn. MCE2

USET,GM,KGG,,,/KNN,,, $

9.220 MDATA Computes pressures for selected elements associated with virtual fluid mass

Format: MDATA

CASECC,XYCDB,MAR,MEA,UAX,OL/ OEP/ APP/S,N,NOSORT2/FREQINDX $

Input Data Blocks: CASECC

Table of Case Control command images for the primary model

XYCDB

Table of x-y plotting commands

MAR

Table of virtual mass element areas

MEA

Matrix of element forces per unit motion of the a-set

UA

Displacement or eigenvector matrix in the a-set

Output Data Block: OEP

Table of element pressures due to virtual mass in SORT1 or SORT2 format

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Parameters: APP

Input-character-no default. Type of analysis. Allowable values are: ‘REIG’: Normal modes ‘CEIG’: Complex eigenvalues ‘FREQ’: Frequency response ‘TRAN’: Transient response

NOSORT2

Input-integer-default=-1. Set to 1 if SORT2 format is requested.

FREQINDX

Input-integer-default=0. Frequency or time step index. Selects frequency associated with UA.

Remarks: 1. XYCDB can be purged. 2. MDATA is available only for normal modes, complex modes, frequency response, and transient response using direct methods only.

9.221 MDCASE Partitions the Case Control table Partitions the Case Control table into separate Case Control tables based on the ANALYSIS Case Control command.

Format: MDCASE

CASECC,EDOM/ CASESTAT,CASEMODE,CASEBUCK,CASEFREQ,CASECEIG, CASEMTRN,CASESAER,CASEDVRG,CASEFLUT,CASESMST, CASESMEM,CASEHEAT,CASEUPSE,CASESADV,CASESNMB, CASEXX/ S,N,STATCC/S,N,MODECC/S,N,BUCKCC/S,N,DFRQCC/ S,N,MFRQCC/S,N,DCEIGCC/S,N,MCEIGCC/S,N,MTRNCC/ S,N,SAERCC/S,N,DVRGCC/S,N,FLUTCC/S,N,SMSTCC/ S,N,SMEMCC/S,N,HEATCC/S,N,UPSECC/S,N,DESOBJ/ S,N,DESGLB/S,N,OBJSID/SEPRTN /S,N,WVFLG $

Input Data Blocks: CASECC

Table of Case Control command images

EDOM

Table of Bulk Data entries related to design sensitivity and optimization

Output Data Blocks: CASESTAT

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Case Control table for static analysis and based on ANALYSIS=STATICS

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CASEMODE

Case Control table for normal modes analysis and based on ANALYSIS=MODES

CASEBUCK

Case Control table for buckling analysis and based on ANALYSIS=BUCK

CASEFREQ

Case Control table for modal or direct frequency response analysis and based on ANALYSIS=MFREQ or DFREQ

CASECEIG

Case Control table for modal or direct complex eigenvalue analysis and based on ANALYSIS=MCEIG or DCEIG

CASEMTRN

Case Control table for modal transient analysis and based on ANALYSIS=MTRAN

CASESAER

Case Control table for aerostatic analysis and based on ANALYSIS=SAERO

CASEDVRG

Case Control table for aerostatic divergence analysis and based on ANALYSIS=DIVERG

CASEFLUT

Case Control table for flutter and based on ANALYSIS=FLUTTER

CASESMST

Case Control table for structural analysis and based on ANALYSIS=STRU

CASESMEM

Case Control table for electromagnetic analysis and based on ANALYSIS=ELEC

CASEHEAT

Case Control table for heat transfer analysis and based on ANALYSIS=HEAT

CASEUPSE

Case Control table for upstream superelements only

CASESADV

Combined Case Control table which includes CASESAER or CASEDVRG

CASESNMB

Combined Case Control table which includes CASESTAT, CASEMODE, CASEBUCK, CASESAER, CASEDVRG, and CASEFLUT

CASEXX

Case Control table intended for Phase 1 matrix generation, assembly and reduction

Parameters: STATCC

Output-logical-default=FALSE. Static analysis subcase flag. Set to TRUE if at least one ANALYSIS=STATICS command is found in CASECC, and CASESTAT is specified in the output list.

MODECC

Output-logical-default=FALSE. Normal modes analysis subcase flag. Set to TRUE if at least one ANALYSIS=MODES command is found in CASECC, and CASEMODE is specified in the output list.

BUCKCC

Output-logical-default=FALSE. Buckling analysis subcase flag. Set to TRUE if at least one ANALYSIS=BUCK command is found in CASECC, and CASEBUCK is specified in the output list.

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DFRQCC

Output-logical-default=FALSE. Direct frequency response analysis subcase flag. Set to TRUE if at least one ANALYSIS=DFREQ command is found in CASECC, and CASEFREQ is specified in the output list.

MFRQCC

Output-logical-default=FALSE. Modal frequency response analysis subcase flag. Set to TRUE if at least one ANALYSIS=MFREQ command is found in CASECC, and CASEFREQ is specified in the output list.

DCEIGCC

Output-logical-default=FALSE. Direct complex eigenvalue analysis subcase flag. Set to TRUE if at least one ANALYSIS=DCEIG command is found in CASECC, and CASECEIG is specified in the output list.

MCEIGCC

Output-logical-default=FALSE. Modal complex eigenvalue analysis subcase flag. Set to TRUE if at least one ANALYSIS=MCEIG command is found in CASECC, and CASECEIG is specified in the output list.

MTRNCC

Output-logical-default=FALSE. Modal transient response analysis subcase flag. Set to TRUE if at least one ANALYSIS=MTRAN command is found in CASECC, and CASEMTRN is specified in the output list.

SAERCC

Output-logical-default=FALSE. Aerostatic analysis subcase flag. Set to TRUE if at least one ANALYSIS=SAERO command is found in CASECC, and CASESAER is specified in the output list.

DVRGCC

Output-logical-default=FALSE. Aerostatic divergence analysis subcase flag. Set to TRUE if at least one ANALYSIS=DIVERG command is found in CASECC, and CASEDVRG is specified in the output list.

FLUTCC

Output-logical-default=FALSE. Flutter analysis subcase flag. Set to TRUE if at least one ANALYSIS=FLUTTER command is found in CASECC, and CASEFLUT is specified in the output list.

SMSTCC

Output-logical-default=FALSE. Structural analysis subcase flag. Set to TRUE if at least one ANALYSIS=STRUCT command is found in CASECC, and CASESMST is specified in the output list.

SMEMCC

Output-logical-default=FALSE. Electromagnetic analysis subcase flag. Set to TRUE if at least one ANALYSIS=ELECT command is found in CASECC, and CASESAER is specified in the output list.

HEATCC

Output-logical-default=FALSE. Heat transfer analysis subcase flag. Set to TRUE if at least one ANALYSIS=HEAT command is found in CASECC, and CASEHEAT is specified in the output list.

UPSECC

Output-logical-default=FALSE. Superelement analysis subcase flag. Set to TRUE if SUPER=ALL or SUPER>0 in CASECC, and CASEUPSE is specified in the output list.

DESOBJ

Output-integer-default=0. DESOBJ Case Control command set identification number.

DESGLB

Output-integer-default=0. DESGLB Case Control command set identification number.

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OBJSID

Output-integer-default=-1. Superelement identification number associated with DESOBJ. Set to -1 for all cases unless you specify the DESOBJ command in a particular superelement subcase.

SEPRTN

Input-logical-default=FALSE. SUPER command processing flag. Set to TRUE to ignore SUPER command.

WVFLG

Output-integer-default=0. Weight/volume response flag. If CASECC does not contain any subcases for statics, normal modes, or buckling subcase, set to 1 if there is a weight or volume response specified on the DRESP1 Bulk Data entry image in EDOM.

Remarks: 1. Any output data block can be purged. 2. EDOM can be purged if WVFLG is not required. 3. CASEXX is a copy of one of the following in the order that they appear and if they exist: CASESTAT CASESAER CASEDVRG CASEMODE CASEFREQ CASEMTRN CASEFLUT

9.222 MERGE Matrix merge Forms a matrix from its partitions.

Format: MERGE

A11,A21,A12,A22,CP,RP/A/SYM/TYPE/FORM $

Input Data Blocks: Aij

Matrix partitions (real or complex)

CP

Column partitioning vector

RP

Row partitioning vector

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Output Data Block: A

Merged matrix from Aij

Parameters: SYM

Input-integer-default=-1. SYM < 0, {CP} is used for {RP}. SYM ≥ 0, {CP} and {RP} are distinct.

TYPE

Input-integer-default=0. Type of [A]. If TYPE is 0, the type of the output matrix is the maximum type of [A11], [A21], [A12], and [A22].

FORM

Input-integer-default=0. Form of [A]. (See Remark 3.)

Remarks: 1. MERGE is the inverse of PARTN in the sense that if [A11], [A12], [A21], [A22] are produced by PARTN using {RP}, {CP}, FORM, SYM and TYPE from [A], MERGE produces [A]. The operation of MERGE is dependent upon the partitioning vectors, {CP} and {RP}, and the symmetry flag, SYM.

Figure 9-5. Let [A] be an m by n matrix, {CP} be an nx1 vector containing q zero elements; and {RP} be a mx1 vector containing p zero elements. Partition [A11] consists of all elements Aij of [A] for which CPj = RPi = 0.0 in the same order as they appear in [A]. Partition [A12] consists of all elements Aij of [A] for which CPj≠ 0.0 and RPi = 0.0 in the same order as they appear in [A]. Partition [A21] consists of all elements Aij of [A] for which CPj = 0.0 and RPi ≠ 0.0 in the same order as they appear in [A]. The following describes the operations: Let

NC = number of nonzero terms in {CP} NR = number of nonzero terms in {RP} NROWA = number of rows in [A] NCOLA = number of columns in [A]

Case 1:

{CP} is purged and SYM ≥ 0: MERGE A11,A21,,,,RP/A/1 $

[A11] is a (NROWA-NR) by NCOLA matrix. [A21] is a NR by NCOLA matrix. [A12] is not written. [A22] is not written.

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Case 2:

(RP) is purged and SYM ≥ 0: MERGE A11,,A12,,CP,/A/1 $

[A11] is a NROWA by (NCOLA - NC) matrix. [A21] is not written. [A12] is a NROWA by NC matrix. [A22] is not written. Case 3:

{RP} is purged and SYM < 0: MERGE A11,A21,A12,A22,CP,/A $

[A11] is a (NROWA-NC) by (NCOLA-NC) matrix. [A21] is a NC by (NCOLA – NC) matrix. [A12] is a (NROWA – NR) by NC matrix. [A22] is a NC by NC matrix. Case 4:

Neither {CP} nor {RP} are purged and SYM ≥ 0: MERGE A11,A21,A12,A22,CP,RP/A/1 $ [A11] is a (NROWA – NR) by (NCOLA – NC) matrix.[A21] is a NR by (NCOLA – NC) matrix.[A12] is a (NROWA – NR) by NC matrix[A22] is a NR by NC matrix.

2. [A11], [A12], [A21], and [A22] must be unique matrices. 3. When FORM = 0, a compatible matrix [A] results as shown in the following table: Form of [A22]

Form of [A11]

Square

Rectangular

Symmetric

Square

Square

Rectangular

Rectangular

Rectangular

Rectangular

Rectangular

Rectangular

Symmetric

Rectangular

Rectangular

Symmetric

4. Any or all of [A11], [A12], [A21], [A22] can be purged. When all are purged, this implies [A] = 0. 5. Both {RP} and {CP} cannot be purged.

Examples: 1. Let A11, A12, A21, A22, {CP} and {RP} be defined as follows:

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The DMAP instruction MERGE

A11,A21,A12,A22,CP,RP/A/1 $

creates the real matrix:

2. If, in Example 1, the DMAP instruction was written as MERGE

A11,A12,,,CP,/A/1 $ RP,CP distinct

the input matrices would be

3. If, in Example 1, the DMAP instruction was written as MERGE

A11,A21,,,,RP/A/1 $

the input matrices would be

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4. If the DMAP instruction is written as MERGE

A11,A21,A12,A22,,RP/A/-1 $

and the input matrices are:

the resulting matrix would be

9.223 MERGEOFP Merges linear and nonlinear stress output Merges OESL (linear element stresses from SDR2) with OESNL (nonlinear element stresses from SDRNL).

Format: MERGEOFP

OES1,OESN1/OES1X $

Input Data Blocks: OES1

Table of element stresses in SORT1

OESNL1

Table of nonlinear element stresses in SORT1 format

Output Data Block: OES1X

Table of linear and nonlinear element stresses in the SORT1 and linear element format

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Remarks: The linear and nonlinear element stress files are read concurrently. The output file is produced with the same order of files as the input files, but where the same element name and ID appear on each input file, the linear element stress data block for the element immediately precedes the nonlinear element stress data block on the output file.

9.224 MESSAGE Prints messages Prints messages to the standard NX Nastran output file.

Format: MESSAGE

//P1/P2/.../Pn $

Parameter: Pi

Input-default is blank. Cannot exceed 80 characters in length.

Remarks: 1. Parameter inputs can be parameter names, actual values, or character strings. 2. Variable parameters must have been typed prior to this statement. 3. The number of parameters is limited only by the size of VPS. 4. The MESSAGE module normally prints to the .f06 standard NX Nastran output file (FORTRAN Unit 6). To have the print also appear in the Performance Summary Table (FORTRAN Unit 4 or dayfile), DIAG 53 must be turned on by the DIAG Executive Control Statement.

Example: MESSAGE

//’USER DMAP MSG’/10/’ERROR IN ITER. NO.’/COUNT $

9.225 MGEN Creates virtual fluid mass matrices

Format: MGEN

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CASECC,MATPOOL,EST,CSTM,BGPDT/ MCHI,MLAM,GEG,MAR,MCHI2,MLAM2/ LUSET/S,N,NOMGEN/UNUSED3/WTMASS/UNUSED5 $

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Input Data Blocks: CASECC

Table of Case Control command images

MATPOOL

Table of Bulk Data entry images related to hydroelastic boundary, heat transfer radiation, virtual mass, DMIG, and DMIAX entries

EST

Element summary table

CSTM

Table of coordinate system transformation matrices

BGPDT

Basic grid point definition table

Output Data Blocks: MCHI

Matrix relating displacements to source strengths

MLAM

Matrix relating element forces to source strengths

GEG

Element displacement interpolation matrix

MAR

Table of virtual mass element areas

MCHI2

Secondary matrix relating displacements to source strengths

MLAM2

Secondary matrix relating element forces to source strengths

Parameters LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

NOMGEN

Output-integer-default=-1. Fluid mass existence flag. Set to the MFLUID set identification number if MFLUID is specified in CASECC.

unused3

Input-real-default=0.0. Unused.

WTMASS

Input-real-default=1.0. Specifies scale factor on structural mass matrix.

unused5

Input-integer-default=-1. Unused.

9.226 MKCNTRL Assembles a description of aerodynamic controllers sets

Format: MKCNTRL

EDT,CSTMA,AEBGPDT/ AECTRL,TRX,AECSTMHG/ SYMXZ/AUNITS $

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Input Data Blocks: EDT

Element deformation table

CSTMA

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points

AEBGPDT

Basic grid point definition table for the aerodynamic degrees-of-freedom

Output Data Blocks: AECTRL

Table of aeroelastic model controls

TRX

Boolean matrix to select accelerations from the list of aerodynamic extra points

AECSTMHG

Table of aerodynamic coordinate system transformation matrices that contains only the hinge moment referenced coordinates systems, if not null.

Parameters: SYMXZ

Input-real-no default. x-z symmetry flag.

AUNITS

Input-real-no default. Used to convert accelerations expressed in gravity units to units of length per time squared.

Remarks: None.

9.227 MKCSTMA Merge coordinate system tables; usually tables from structural and aerodynamic models.

Format:. MKCSTMA

CSTM1,CSTM2/CSTMM $

Input Data Block: CSTMi

Tables of coordinate system transformation matrices

Output Data Block: CSTMM

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Parameters: None.

9.228 MKSPLINE Generates splines to interpolated results from structural to aero model

Format: MKSPLINE

EDT,CSTMA,AEGRID,AECOMP/ SPLINE $

Input Data Blocks: EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

CSTMA

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points

AEGRID

Basic grid point definition tables for the aerodynamic model

AECOMP

Aerodynamic component definition table

Output Data Block: SPLINE

Table of SETi, AELIST, and SPLINEi Bulk Data entry images with external grid identification numbers

Parameters: None.

Example: Excerpt from subDMAP PHASE0: DBVIEW AEGRID=BGPDTS WHERE (MODLTYPE=‘AEROMESH’AND WILDCARD) $ MKSPLINE EDT,CSTMA,AEGRID,AECOMP/SPLINE $

9.229 MODACC OFREQ, OTIME, and OMODES command processor. Removes columns in solution and load matrices based on the OTIME, OFREQ, and OMODES case control commands.

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Format: MODACC

CASECC,OL,U,P1,P2,P3/ OL1,U1,P11,P21,P31/APP/IOPT $

Input Data Blocks: CASECC

Table of Case Control command images.

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list.

U

Solution matrix from normal modes, complex modes, transient response, or frequency response.

Pi

Any matrix with the same number of columns as there are eigenvalues, frequencies, or time steps in OL.

Output Data Blocks: OL1

OL truncated by the OFREQ or OTIME or OMODES command.

U1

U truncated by the OFREQ or OTIME or OMODES command.

Pi1

Pi truncated by the OFREQ or OTIME or OMODES command.

Parameters: APP

Input-character-default=‘TRAN’. Analysis type.

IOPT

‘REIGEN’

Normal modes

‘FREQRESP’

Frequency response

‘TRANRESP’

Transient response

‘CEIGEN’

Complex eigenvalues

Input-integer-default=0. Processing options: 0=process OFREQ or OTIME or OMODES. 1=process SETMC for MODCON. 2=process SETMC for PANCON.

Remarks: 1. MODACC selects vectors based on OTIME or OFREQ or OMODES commands in CASECC. If APP = ’CEIG’, the selection is based on the imaginary part of the complex eigenvalue. If APP = ’REIG’, the selection is based on the frequency (f = w/2π)

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2. Here are typical data block names and the appropriate value of APP: LAMA

APP = ‘REIG’

CLAMA

APP = ‘CEIG’

FOL

APP = ‘FREQ’

TOL

APP = ‘TRAN’

3. If APP=’CEIGEN,’ P11 must not be purged.

9.230 MODEPF Computes mode participation factors for fluid-structure models in frequency response analysis.

Format: MODEPF

BGPDT,USET,CASECC,EDT,ABESF*, PHASH2,UHFS,PHDFH,MFHH,BFHH, KFHH,FOL,ABEH*,PHDFH1,PHDFH2, UHFF,AH,PFHF,UNUSED,PNLLST, VGA,GEOM2/ GPMPF,FMPF,SMPF,PMPF,LMPF, MPFMAP/ NOFREQ/NOLOADF/GRIDFMP/NUMPAN/PNQALNAM/ SYMFLG/MPNFLG/FLUIDMP/STRUCTMP/PANELMP/ GRIDMP/NOSASET/FILTERF/FILTERS $

Input Data Blocks: BGPDT

Basic grid point definition table

USET

Degree-of-freedom set membership table for g-set

CASECC

Table of Case Control command images

EDT

Table of Bulk Data entry images containing SET1 entries

ABESF*

Family of a-set size panel area matrices

PHASH2

Structural partition (row-wise) of eigenvector matrix PHDH. Also partitioned column-wise according to parameter STRUCTMP

UHFS

Structural partition (row-wise) of solution matrix UHF. Also partitioned column-wise according to parameter STRUCTMP

PHDFH

Fluid partition (row-wise) of eigenvector matrix PHDH

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MFHH

Fluid partition of modal mass matrix MHH

BFHH

Fluid partition of modal damping matrix BHH

KFHH

Fluid partition of modal stiffness matrix KHH

FOL

Table of forcing frequencies

ABEH*

Family of signed modally reduced area matrices

PHDFH1

Fluid partition (row-wise) of eigenvector matrix PHDH reduced to a-set size

PHDFH2

PHDFH1 partitioned by parameter FLUIDMP

UHFF

Fluid partition (row-wise) of solution matrix UHF. Also partitioned column-wise according to parameter FLUIDMP

AH

Signed global modally reduced area matrix

PFHF

Fluid partition of frequency response modally reduced load matrix

UNUSED

Unused

PNLLST

Table of triplets defining panel names and their associated IPANEL qualifier values

VGA

G-set size partitioning vector with values of 1.0 at the rows corresponding to the a-set

GEOM2

Table of bulk data images related to element connectivity

Output Data Blocks: GPMPF

Matrix of grid panel mode participation factors

FMPF

Matrix of fluid mode participation factors

SMPF

Matrix of contribution of structure to fluid mode participation factors

PMPF

Matrix of contribution of structural panels to fluid mode participation factors

LMPF

Matrix of fluid force to fluid mode participation factors

MPFMAP

Table describing content of mode participation factor matrices

Parameters: NOFREQ

Input-integer-no default. Number of excitation frequencies.

NOLOADF

Input-integer-no default. Number of load cases per frequency.

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GRIDFMP

Input-integer-no default. Case Control set identification number of fluid grids that are output: 0

Case Control set that contains grid list to be output

NUMPAN

Input-integer-no default. Number of panels.

PNQALNAM

Input-character-default=” Name of qualifier for panels.

SYMFLG

Input-complex-default=(1.,0.). Scale factor.

MPNFLG

Input-integer-no default. Panel existence flag.

FLUIDMP

Input-integer-default=-1. Number of fluid modes to use in computing factors. If FLUIDMP>0, compute factors for the first FLUIDMP modes.

STRUCTMP

Input-integer-default=-1. Number of structure modes to use computing factors.

PANELMP

Input-integer-default=-1. Flag to compute panel participation factors. See Remark 2.

GRIDMP

Input-integer-default=-1. Case Control set identification number for a set of fluid grids.

NOSASET

Input-integer-default=-1. Number of degrees-of-freedom in the a-set of the structure.

FILTERF

Input-real-default=0.95. Filter for fluid factor matrices.

FILTERS

Input-real-default=0.95. Filter for structure factor matrices.

Remarks: 1. VGA can be purged if no diagnostic printouts are desired. 2. If STRUCTMP>0, these are the output options: •

Compute structural mode participation factors.

•

If MPNFLG>0 and PANELMP>-1, compute panel mode participation factors, PMPF.

•

Compute load mode participation factors, LMPF.

•

If MPNFLG>0 and GRIDMP>-1, compute fluid grid mode participation factors, GMPF.

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9.231 MODEPOUT Filter, sort, and printout mode participation factor matrices. Also create table data blocks suitable for XY plots and power spectral density calculations.

Format: MODEPOUT

LAMAF,LAMAS,CASECC,FMPF,SMPF, PMPF,LMPF,GMPF,MPFMAP/ OFMPF2E,OFMPF2M,OSMPF2E,OSMPF2M,OPMPF2E, OPMPF2M,OLMPF2E,OLMPF2M,OGMPF2E,OGMPF2M, UNUSED1,UNUSED2,UNUSED3,UNUSED4,UNUSED5/ OUTFMP/OUTSMP/FMPFEPS/SMPFEPS/MPFSORT/ NOMPF2E $

Input Data Blocks: LAMAF

Normal modes eigenvalue summary table for the fluid portion of the model

LAMAS

Normal modes eigenvalue summary table for the structural portion of the model

CASECC

Table of Case Control command images

FMPF

Matrix of fluid mode participation factors

SMPF

Matrix of contribution of structure to fluid mode participation factors

PMPF

Matrix of contribution of structural panels to fluid mode participation factors

LMPF

Matrix of fluid force to fluid mode participation factors

GPMPF

Matrix of grid panel mode participation factors

MPFMAP

Table describing content of mode participation factor matrices

Output Data Blocks: OFMPF2E

Table of fluid mode participation factors by excitation frequencies

OFMPF2M

Table of fluid mode participation factors by normal mode

OSMPF2E

Table of structure mode participation factors by excitation frequencies

OSMPF2M

Table of structure mode participation factors by normal mode

OPMPF2E

Table of panel mode participation factors by excitation frequencies

OPMPF2M

Table of panel mode participation factors by normal mode

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OLMPF2E

Table of load mode participation factors by excitation frequencies

OLMPF2M

Table of load mode participation factors by normal mode

OGMPF2E

Table of grid mode participation factors by excitation frequencies

OGMPF2M

Table of grid mode participation factors by normal mode

UNUSEDi

Unused

Parameters: OUTFMP

Input-integer-default=0. Number of fluid modes to output.

OUTSMP

Input-integer-default=0. Number of structure modes to output.

FMPFEPS

Input-real-default=0.0. Threshold for filtering out small fluid factor magnitudes.

SMPFEPS

Input-real-default=0.0. Threshold for filtering out small structure factor magnitudes.

MPFSORT

Input-integer-default=11. Sort flag.

NOMPF2E

10

Sort on absolute value (magnitude)

20

Sort on real portion

30

Sort on complex portion

40

Sort on phase angle (must convert)

1

Descending sort

2

Ascending sort

Input-integer-default=-1. 0

Generate

-1

Do not generate

Remarks: 1. The O*MPF2E data blocks are suitable for input to the XYTRAN module. 2. The O*MPF2M data blocks are suitable for input to the RANDOM module.

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9.232 MODEPT Updates PACABS and PACABR Bulk Data entry records based upon data on TABLEDi Bulk Data entry records.

Format: MODEPT

EPT,DIT/EPTX/S,N,NOGOMEPT $

Input Data Blocks: EPT

Table of Bulk Data entry images related to element properties; in particular, PACABS and PACABR entries

DIT

Table of TABLEij Bulk Data entry images

Output Data Blocks: EPTX

Copy of EPT except that PACABS and PACABR entries are updated with TABLEij references

Parameter: NOGOMEPT

Logical-output-default=FALSE. Set to TRUE if an error is detected in the Bulk Data entries.

Remarks: 1. MODEPT does not terminate the run if an error is detected in the Bulk Data entries. NOGOMEPT should be checked before proceeding to the GP1 module. 2. MODEPT must appear after the IFP.

Example: See the example in the IFP module description.

9.233 MODGDN Updates geometry table for existence of p-elements and superelements

Format: MODGDN

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GEOM1,SEMAP,MFACE,MEDGE,MBODY/ GEOM1P/ S,N,NOSEMAP $

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Descriptions of DMAP Modules and Statements

Input Data Blocks: GEOM1

Table of Bulk Data entry images related to geometry

SEMAP

Superelement map table

MFACE

Face table for p-element analysis

MEDGE

Edge table for p-element analysis

MBODY

Body table for p-element analysis

Output Data Block: GEOM1P

Table of Bulk Data entry images related to geometry updated for p-elements and superelements

Parameter: NOEMAP

Output-integer-default=0. Superelement map table flag. Set to -1 if SEMAP does not exist.

9.234 MODGM2 Create table entries for PLPLANE and PLSOLID Bulk Data Creates internal records in the element connectivity table based on the presence of PLPLANE and PLSOLID Bulk Data entry records. Internal records are also created from fluid elements defined on the PSOLID Bulk Data entry.

Format: MODGM2

EPT,GEOM2,GEOM1/ GEOM2X,GEOM1X/ S,N,ACFLAG/OSWPPT/OSWELM/S,N,NSWPPT/ S,N,NSWELM/S,N,SWEXIST/S,N,NOGOMGM2 $

Input Data Blocks: EPT

Table containing element properties Bulk Data entry records

GEOM2

Table containing element connectivity Bulk Data entry records

GEOM1

Table of Bulk Data entry images related to geometry

Output Data Block: EPTX

Copy of EPT except for the records shown in Remark 2

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GEOM1 table related to axisymmetric conical shell, hydroelastic, acoustic cavity, and spot weld element analysis

Parameter: ACFLAG

Integer-output-default=0. ACFLAG>0 indicates fluid elements: 0 No fluid elements 1 Fluid elements 2 Fluid/structure coupling

OSWPPT

Input-integer-default=0. Offset for spot weld projection point IDs.

OSWELM

Input-integer-default=0. Offset for spot weld element IDs.

NSWPPT

Output-integer-default=0. Current spot weld projection point ID.

NSWELM

Output-integer-default=0. Current spot weld element ID.

SWEXIST

Output-logical-no default. Spot weld element existence flag. Set to TRUE if spot weld elements exist.

NOGOMGM2

Output-logical-no default. MODGM2 module error return flag. Set to TRUE if an error is found.

Remarks: 1. MODGM2 must appear after the IFP. 2. The following GEOM2 Bulk Data entry records are replaced by the internal records in GEOM2X: GEOM2 Record -----CQUAD4 CQUAD8 CTRIA3 CTRIA6 CQUAD CTRIAX CQUADX CHEXA CPENTA CTETRA

GEOM2X record Fluid Hyperelastic -------------------n/a QUAD4FD n/a QUAD8FD n/a TRIA3FD n/a TRIA3FD n/a QUADFD n/a TRIAXFD n/a QUADXFD HEXPR HEXAFD PENPR PENTAFD TETPR TETRAFD

Example: See the example in the IFP module description.

9.235 MODGM4 Reads SPCs and SPCDs and generates unique SPC and SPCD records

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Reads the SPCs and SPCDs that were defined by GMBC, GMSPC, SPC, SPC1, or SPCD Bulk Data entries and generates the unique SPC and SPCD records.

Format: MODGM4

CASECC,GEOM2M,GEOM4M,DEQATN,DEQIND,DIT,BGPDTM,EPT/ GEOM4P/ GNSTART/S,N,MODGM4/ALTSHAPE/S,N,NSWELM $

Input Data Blocks: CASECC

Table of Case Control command images

GEOM2M

Table of Bulk Data entry images related to element connectivity and scalar points and updated for the current p-level

GEOM4M

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity and updated for the current p-level

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

DIT

Table of TABLEij Bulk Data entry images

BGPDTM

Basic grid point definition table and updated for the current p-level

EPT

Table containing element properties Bulk Data entry records

Output Data Blocks: GEOM4P

Table of Bulk Data entry images related to constraints, updated for the constraints applied by GMBC, GMSPC, SPC, SPC1, or SPCD Bulk Data entries

Parameters: GNSTART

Input-integer-default=0. First grid identification number in GEOM1M.

MODGM4

Output-logical-default=FALSE. GEOM4P update flag. Set to TRUE if GEOM4M is updated.

ALTSHAPE

Input-integer-no default. Specifies set of displacement functions in p-element analysis. ALTSHAPE=0 selects the MacNeal set and 1 selects the Full Product Space set.

NSWELM

Output-integer-default=0. Current spot weld element ID.

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9.236 MODTRK Reorders eigenvalues and eigenvectors to be consistent with previous design cycle Compares the mode set of the current design cycle with those of the previous design cycle, identifies or tracks these modes, and reorders the eigenvalues and eigenvectors to be consistent with the previous design cycle.

Format: MODTRK

CASECC,EDOM,R1TABR,LAMA,MGG,MAA,PHG,PHA,PHGREF, PHAREF/MTRAK,LAMA1,PHG1,PHA1,PHGREF1,PHAREF1/ DESCYCLE/S,N,NOTRACK $

Input Data Blocks: CASECC

Table of Case Control command images

EDOM

Table of Bulk Data entries related to design sensitivity and optimization

R1TABR

Table of retained first level (direct) (DRESP1 Bulk Data entry) attributes

LAMA

Normal modes eigenvalue summary table

MGG

Mass matrix in g-size

MAA

Mass matrix in a-set

PHG

Normal modes eigenvector matrix in the g-set

PHA

Normal modes eigenvector matrix in the a-set

PHGREF

Designed normal modes eigenvector matrix in the g-set from the prior design cycle output of MODTRK

PHAREF

Designed normal modes eigenvector matrix in the a-set from the prior design cycle output of MODTRK

Output Data Blocks: MTRAK

Table of updated DRESP1 Bulk Data entry images corresponding to the new mode numbering

LAMA1

Normal modes eigenvalue summary table updated for mode tracking

PHG1

Normal modes eigenvector matrix in the g-set updated for mode tracking

PHA1

Normal modes eigenvector matrix in the a-set updated for mode tracking

PHGREF1

Designed normal modes eigenvector matrix in the g-set updated for mode tracking

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PHAREF1

Designed normal modes eigenvector matrix in the a-set updated for mode tracking

Parameters: DESCYCLE

Input-integer-no default. Design cycle analysis counter.

NOTRACK

Output-logical-default=FALSE. Mode tracking success flag. Set to TRUE if mode tracking was successful.

Remarks: MODTRK prints a report on mode switching activity for the current design cycle and punches out updated DRESP1 Bulk Data entries that correspond to the new mode positions.

Example: Excerpt from subDMAP FEA: DESITERP=DESITER-1 $ DBVIEW PHAREF0=PHAREF WHERE (DESITER=DESITERP) $ DBVIEW PHGREF0=PHGREF WHERE (DESITER=DESITERP) $ MODTRK CASEM,EDOM,LAMAS,MGG,MAA,PHG,PHSA,PHGREF0,PHAREF0/ MTRAKS,NEWLAMA,NEWPHG,NEWPHA,PHGREF,PHAREF/ DESCYCLE/S,N,NOTRACK $

9.237 MODTRL Modify trailer Modify data block trailer data.

Format: MODTRL

DB//P1/P2/P3/P4/P5/P6 $

Input Data Block: DB

Data block with trailer that is to be modified

Parameters: Pi

Input-integer-default=-1. New value for i-th trailer word.

Remarks: 1. Negative parameters are ignored. Nonnegative parameters cause the corresponding word of the data block trailer to be replaced by the value of the parameter.

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2. MODTRL should be scheduled immediately after the functional module that generates the data block. For example: ADD MODTRL EQUIVX

I1,I2/O1 $ O1////6 $ Ol/O2/ALWAYS $

3. If MODTRL is used to increase the number of columns in a matrix, the resulting matrix is unusable in most modules, including MATPRN and ADD. 4. The correspondence between the parameters and the content of a matrix trailer is as follows: Parameter

Matrix trailer

P1

Number of columns

P2

Number of rows

P3

Form

P5

Number of nonzero words

For matrices, P4 and P6 must be -1 or unspecified. See Examples 2 and 3. 5. For table trailer contents, see the data block descriptions.

Examples: 1. Make KAA symmetric (form=6) (MPYAD labels it square (form=1)). MPYAD MODTRL

GO,KOA,KAAB/KAA/1 $ KAA////6/ $

2. Use ADD5 to change the precision of a matrix. If the new precision does not match the machine precision, specify PUTSYS (newprecision,55) before ADD5. For example, on a double-word machine: •

Single to double ADD5

•

SINGLE,,,,/DOUBLE $

Double to single PUTSYS(1,55) $ ADD5 DOUBLE,,,,/SINGLE $ PUTSYS(2,55) $

3. In order to change the type (complex or real) of a matrix, use ADD to convert real to complex and MATMOD(34) for complex to real. For example, •

Real to complex ADD

•

Complex to real MATMOD

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REAL,/CMPLX//(0.,1.) $

CMPLX,,,,,/REAL,/34 $

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9.238 MODUSET Modifies the degree-of-freedom set membership table (USET)

Format: MODUSET

UNUSED1,USET/ USETM/ USETOP/MAJOR/SET0/SET1/USETADD/UNUSED6/UNUSED7 $

Input Data Blocks: EDITVEC

Vector with zeros in rows to be removed under USETOP=‘FILTER’ See Remark 2.

USET

Degree-of-freedom set membership table for g-set

Output Data Block: USETM

Modified degree-of-freedom set membership table for g-set

Parameters: USETOP

Input-character-default=‘UNION’ Name of desired operation. See Remark 1.

MAJOR

Input-character-default=‘U3’ Name of the major set. The major set must be larger than the subsets defined by SET0 and SET1.

SET0

Input-character-default=‘U2’ Name of the "zeros" subset of MAJOR.

SET1

Input-character-default=‘U1’ Name of the "ones" subset of MAJOR.

USETADD

Input-integer-default=1. USET length extension. If USETOP=‘EXPAND‘, extend the size of the USET by this amount.

UNUSED6

Input-integer-default=0. Unused.

UNUSED7

Input-integer-default=0. Unused.

Remarks: 1. The values and actions for USETOP are: UNION

Combine SET0 and SET1 into MAJOR

COMP0

Form SET0 from complement of MAJOR and SET1

COMP1

Form SET1 from complement of MAJOR and SET0

DELETE

Remove degrees-of-freedom from MAJOR

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TURNON

Add degrees-of-freedom from MAJOR

COPY

Copy degrees-of-freedom from SET0 to MAJOR

EXPAND

Extend USET length by USETADD.

MOVE

Move SET0 degrees-of-freedom to MAJOR

FILTER

Remove degrees-of-freedom from USET that correspond to zero rows in EDITVEC

2. EDITVEC can be purged if USETOP≠‘FILTER’

Examples: 1. Scalar degrees-of-freedom 1 through 5 are defined in the u1-set and u3-set and scalar degrees-of-freedom 6 through 10 in the u2-set and u3-set. SOL ... COMPILE ... ALTER ... MODUSET ,,USET/USET1 $ CEND BEGIN BULK SPOINT,1,THRU,10 USET1,U1,0,1,THRU,5 USET1,U3,0,6,THRU,10

2. The u1-set is empty. The u2-set contains the a-set and the u3-set contains the f-set. MODUSET MODUSET MODUSET

,,USET/VSET/‘COMP0‘/‘F’/‘U1‘/‘A’ $ ,,VSET/WSET/‘COMP1‘/‘F’/ /‘U2’$ ,,WSET/XSET/‘UNION‘/‘U3‘/‘U1‘/‘U2’$

3. The following alter puts all degrees-of-freedom automatically constrained by GPSP into the sg-set. COMPILE SEKR0 ALTER ‘GPSP‘(,-1) $ BEFORE GPSP $ MOVE DOF IN SET SB INTO SET U3 MODUSET, ,USET0/VSET/‘MOVE‘/‘U3‘/‘SB‘/ $ EQUIVX VSET/USET0/ALWAYS $ MESSAGE //‘SB SET SHOULD NOW BE EMPTY - CHECK BELOW‘/ $ TABPRT USET0,EQEXINS//‘USET‘/11 ALTER ‘GPSP’$ AFTER GPSP MESSAGE //‘SB SET SHOULD NOW BE ONLY AUTOSPC DOF - CHECK BELOW‘/ $ TABPRT USET,EQEXINS//‘USET‘/11 $ MOVE CURRENT SB (ALL FROM AUTOSPC) INTO SG MODUSET, ,USET/VSET1/‘MOVE‘/‘SG‘/‘SB‘/ $ MESSAGE //‘SB SET SHOULD NOW BE EMPTY,SG SHOULD BE PS + AUTOSPC‘/ $ TABPRT VSET1,EQEXINS//‘USET‘/11 $ NOW MOVE SET U3 BACK INTO SB MODUSET, ,VSET1/VSET2/‘MOVE‘/‘SB‘/‘U3‘/ $ EQUIVX VSET2/USET/ALWAYS $ MESSAGE //‘SB SET SHOULD NOW BE ONLY SPC DOF‘/ ’SG SHOULD BE PS + AUTOSPC‘/ $ TABPRT USET,EQEXINS//‘USET‘/11 $

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9.239 MONVEC Forms monitor point rigid body vectors

Format: MONVEC

Input Data Blocks: AEMONPT

Table of aerodynamic monitor points

MONITOR

Table of structural monitor points

AEROCOMP

Table of aerodynamic components when MESH=‘AERO’

STRUCOMP

Table of structural components when MESH=‘STRU’

AEBGPDT

Basic grid point definition table for the aerodynamic degrees-of-freedom

CSTMA

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points

Output Data Blocks: SRKS

Matrix of monitor point rigid body vectors

Parameters: None.

9.240 MPP Prints monitor point results Prints monitor point results for either trim subcase or for any one UXDAT instance or for any one UXDAT instance by interpolation of the UXV.

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Format: MPP

Input Data Blocks: AECTRL

Table of aeroelastic model controls.

UXDAT

Table of aerodynamic extra point identification numbers, displacements, labels, type, status, position and hinge moments

MONITOR

Monitor point table

AEMONPT

Aerodynamic monitor point table

MPSR

Rigid aerodynamic loads on structural monitor points at trim (excluding inertial loads and static applied loads)

MPAR

Rigid aerodynamic loads on aerodynamic monitor points at trim

MPSER

Elastic restrained loads on structural monitor points at trim (excluding inertial loads and static applied loads)

MPAER

Elastic restrained loads on aerodynamic monitor points at trim

MPEU

Elastic unrestrained loads on monitor points either at trim or across ADB/AEDB

MPSIR

Inertial loads on structural monitor points at trim

MPSRP

Rigid loads on structural monitor points due to static applied loads

MPSERP

Elastic restrained loads on structural monitor points due to static applied loads

UXV

Control state matrix for ADB or AEDB

ADBINDX

Index of ADB or AEDB

Output Data Blocks: None.

Parameters: MACH

Input-real-no default. Mach number.

Q

Input-real-no default. Dynamic pressure.

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AECONFIG

Input-character-no default. Aerodynamic configuration.

SYMXY

Input-integer-no default. Aerodynamic x-y symmetry flag.

SYMXZ

Input-integer-no default. Aerodynamic x-z symmetry flag.

MESH

Input-character-no default. Mesh type

Examples: 1. Print structural monitor point loads at trim. MPP

AECTRL,UXDAT,MONITOR,MPSR,MPSER,,MPSIR,MPSRP,MPSERP,,// MACH/Q/AECONFIG/SYMXY/SYMXZ/‘STRUCT’$

2. Print aerodynamic monitor point loads at trim. MPP

AECTRL,UXDAT,AEMONPT,MPAR,MPAER,,,,,,// MACH/Q/AECONFIG/SYMXY/SYMXZ/‘AERO’$

9.241 MPYAD Matrix multiply and add Perform the multiplication of two matrices and optionally, the addition of a third matrix to the product.

Format: MPYAD

A,B,C/X/T/SIGNAB/SIGNC/PREC/FORM $

Input Data Blocks: A

Left-hand matrix in the matrix product

B

Right-hand matrix in the matrix product

C

Matrix to be added to the product

Output Data Block: X

Matrix product

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Parameters: T

Integer-input-default = 0. Transpose flag. T = 1, perform [A]T [B] T = 0, perform [A][B]

SIGNAB

Integer-input-default = 1. Sign of product flag. SIGNAB = +1, perform [A] [B] SIGNAB = -1, perform −[A][B]

SIGNC

Integer-input-default = 1. Sign of [C] flag. SIGNC = +1, add [C] SIGNC = -1, subtract [C]

PREC

Integer-input-default = 0. Precision. PREC = 1, element of [X] are output in single precision PREC = 2, elements of [X] are output in double precision PREC = 0, elements of [X] are output in the precision of the computer

FORM

Integer-input-default = 0. Form of [X]. FORM = 0, form of [X] is 1 (square) or 2 (rectangular)

Remarks: 1. If no matrix is to be added, [C] must be purged. [A] can be Form 3. 2. [A] and [B] can be the same data block, but both must be different from [C]. 3. If [A] or [B] is purged, and [C] is purged, [X] is purged. [C] cannot be Form 3. 4. If [A] and/or [B] is purged, but [C] exists, the purged matrices are equivalent to null matrices, and [X] are output. 5. [X] cannot be purged. 6. if the precision of the computer is double precision and B is single precision, and Methods 1, 2, 3 are deselected, PREC must be set equal to 1. 7. The MPYAD keyword (or SYSTEM(66)) and the SPARSE keyword (or SYSTEM(126)) on the NASTRAN statement is used for MPYAD method deselection. (The SPARSE keyword is described in Remark 11.) The Deselection Values in the table below are used to deselect or disable a single method or several methods. If MPYAD=0 and SPARSE=1, which are the defaults, the method that results in the lowest CPU and I/O time is selected. If all transpose methods are deselected, T must be equal to zero (default). If all nontranspose methods are deselected, T must be equal to 1.

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Method

Storage technique

MPYAD keyword deselection value

1 Nontranspose

1

1

1 Transpose

1

2

2 Nontranspose

—

4

2 Transpose

—

8

3 Nontranspose

—

16

3 Transpose

—

32

4 Nontranspose

—

64

4 Transpose

—

128

1 Nontranspose

A

256

1 Nontranspose

B

512

1 Nontranspose

C

1024

1 Nontranspose

D

2048

1 Nontranspose

E

4096

1 Nontranspose

F

8192

1 Transpose

A

16384

1 Transpose

B

32768

1 Transpose

C

65536

1 Transpose

D

131072

1 Nontranspose

2

8388608

1 Transpose

2

16777216

1 Nontranspose

3

67108864

1 Transpose

3

134217728

•

For methods 2, 3, and 4, a combination of methods is selected by subtracting the sum of their Deselection Values from 255. For example, NASTRAN MPYAD = 243 (which is obtained from 255-(4+8)) selects only Methods 2 Transpose and Nontranspose.

•

For Method 1 Submethods (storage techniques), a combination of methods is selected accordingly. First, sum their Deselection Values then add 1 (if Nontranspose) and/or 2 (if Transpose). This total is then subtracted from 262143. See examples below.

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Example 1:

If only Method l Nontranspose with storage techniques D, E, and F are desired, NASTRAN MPYAD=247806 (which is obtained from 262143-(2048 + 4096 + 8192 + 1)).

Example 2:

If Method 2 is also desired in Example 1, NASTRAN MPYAD=247794 (which is obtained from 262143-(2048 + 4096 + 8192 + 8 + 4 + 1)).

8. As an alternative to the deselection procedure described above, the MPYAD keyword value can be set to select a single method while deselecting all other methods and submethods. To select a single method, add 1048576 to the selection value of the desired method shown in the table below. For example, if Method 1 Nontranspose Storage Submethod C is desired, MPYAD = 1048586; computed from 1048576 + 10. Method

9-424

Storage submethod

Selection value

Method

StorageSubmethod

SelectionValue

1 Nontranspose

1

0

1 Transpose

1

1

2 Nontranspose

—

2

2 Transpose

—

3

3 Nontranspose

—

4

3 Transpose

—

5

4 Nontranspose

—

6

4 Transpose

—

7

1 Nontranspose

A

8

1 Nontranspose

B

9

1 Nontranspose

C

10

1 Nontranspose

D

11

1 Nontranspose

E

12

1 Nontranspose

F

13

1 Transpose

A

14

1 Transpose

B

15

1 Transpose

C

16

1 Transpose

D

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Method

Storage submethod

Selection value

1 Nontranspose

2

23

1 Transpose

2

24

1 Nontranspose

3

26

1 Transpose

3

27

If a Storage Submethod under Method 1 is selected in this manner, a printout of timing estimates for the other submethods can be requested by adding 3145728 to the selection value above. Using the previous example, MPYAD = 3145738, computed from 3145728 + 10. 9. Sparse methods are deselected or selected by the SPARSE keyword (or SYSTEM(126)) on the NASTRAN statement. The default SPARSE = 1 causes the automatic selection of sparse methods if their CPU and I/O estimates are lower than those estimated for the methods in Remark 7. If the sparse method is not desired, specify SPARSE = 0 or 6. •

In order to select or force one or both methods below, add l to its value(s) below. Sparse method

SPARSE keyword value

Nontranspose

2

Transpose

4

Example 1:

To force the sparse nontranspose method, specify SPARSE = 3, computed from 1 + 2.

Example 2:

To force the sparse methods, specify SPARSE = 7, computed from 1 + 2 + 4.

Note that if SPARSE = 2, 3, 4, 5, or 7, all methods in Remark 2 are turned off or deselected, and the MPYAD keyword must be equal to zero. •

The SPARSE keyword is also used for sparse method selection within all modules which perform matrix decomposition and forward-backward substitution; for example, DCMP, DECOMP, FBS, and SOLVE.

10. The diagonal matrix format (FORM = 3) for input matrices is not supported for the transpose option (T = 1), and causes an “ILLEGAL INPUT” fatal message. [A] can be transposed with the TRNSP module. 11. Parallel processing in this module (Methods 1 Nontranspose Storage E and Transpose Storage C only) is selected with the NASTRAN statement keyword PARALLEL (or SYSTEM(107)) which is set to the number of parallel processors (default = 0). To force parallel processing, the MPYAD keyword must be set to one of the following values:

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MPYAD keyword

Storage technique

1048592

Transpose C

1048588

Nontranspose E

192512

Both

Examples: 1. [X] = [A][B] + [C] MPYAD A,B,C/X/ $

2. [X]=[A]T [B] - [C] MPYAD A,B,C/X/1//-1/ $

3. [X] = -[A] [B] MPYAD A,B,/X//-1 $

9.242 MRGCOMP Merges two existing aerodynamic or structural component tables

Format: MRGCOMP

COMP1,COMP2/ COMP/ COMPRPLC $

Input Data Blocks: COMPi

Table of aerodynamic or structural components

Output Data Block: COMP

Merged table of components

Parameter: COMPRPLC

Input-logical-default=FALSE. If TRUE, components with duplicate names are copied from COMP1 into COMP.

Remarks: Duplicate component names causes a fatal message to be issued unless COMPRPLC is true.

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9.243 MRGMON Merges two monitor point tables Merges two monitor point tables and optionally output their associated matrices.

Format: MRGMON

MON1,MON2,SZR1,SZR2/ MON,SZR/ MONRPLC $

Input Data Blocks: MONi

Monitor tables

SZRi

Associated monitor matrices

Output Data Blocks: MON

Merged monitor table

SZR

Merged monitor matrices

Parameter: MONRPLC

Input-logical-default=FALSE. If TRUE, components with duplicate names are copied from MON1 into MON.

Remarks: 1. Duplicate monitor points causes a fatal message to be issued unless MONRPLC is true. 2. SZR1, SZR2, and SZR can be purged. 3. SZR is created only if both SZR1 and SZR2 exist.

9.244 MSGHAN Passes message number for processing by MSGPOP API

Format: MSGHAN

//MSGNUM/MSGINP1/MSGINP2/S,N,MSGOUT $

Input Data Blocks: None.

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Output Data Blocks: None.

Parameters: MSGNUM

Input-integer-default=0. Message number.

MSGINP1

Input-integer-default=0. Optional integer input.

MSGINP2

Input-integer-default=0. Optional integer input.

MSGOUT

Output-integer-default=0. Optional integer output.

9.245 MSGSTRES Computes data based on fields generated by MSGMESH Computes grid point stresses, maximum and minimum stresses, and stress contour plots based on fields generated by MSGMESH.

Format: MSGSTRES

FORCE,OES1X// S,N,PLTNUM/NOMSGSTR $

Input Data Blocks: FORCE

Table of MSGSTRESS plotting commands defined under the OUTPUT(CARDS) section in CASE CONTROL and MSGMESH field information

OES1

Table of element stresses or strains in SORT1 format

Output Data Blocks: None.

Parameters: PLTNUM

Input/output-integer-default=0. Plot frame counter.

NOMSGSTR

Input-integer-default=0. MSGSTRES execution flag. Set to -1 if MSGSTRES execution is not desired.

9.246 MTRXIN Converts matrices input on DMIG Bulk Data entries to matrix data blocks.

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Format: Form 1 – Simplified (CASECC is purged) MTRXIN

Form 2 – Case Control Command Selection of stiffness, mass, and damping (or square) matrices (IOPT=1 for K2GG, and so on, and IOPT=0 for K2PP, and so on, and TF) MTRXIN

Form 3 – Case Control Command selection of load (or rectangular) matrix (IOPT=2) MTRXIN

Form 4 – Selection of DMIK, DMIJ and DMIJI by data block names MATKi, MATJi, and MATJIi. MTRXIN

Form 5 – Selection of stiffness, mass, damping, and loads (or square) matrices by K2PNAM, and so on, input parameter values (IOPT=10 through 12).

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MTRXIN

Form 6 - Selection of DMIK, DMIJ, and DMIJI matrices by the MATNAMi input parameter values (IOPT=13 through 15) MTRXIN

Input Data Blocks: CASECC

Table of Case Control command images

MATPOOL

Table of Bulk Data entry images related to hydroelastic boundary, heat transfer radiation, virtual mass, DMIG, and DMIAX entries

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

EQDYN

Equivalence table between external and internal grid/scalar/extra point identification numbers. (EQEXIN appended with extra point data)

TFPOOL

Table of TF Bulk Data entry images

AEBGPDTK

Basic grid point definition table for the aerodynamic ks-set degrees of freedom

AEBGPDTJ

Basic grid point definition table for the aerodynamic js-set degrees of freedom

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AEBGPDTI

Basic grid point definition table for the aerodynamic js-set interference degrees of freedom

Output Data Blocks: NAMEi

Matrices defined on DMIG Bulk Data entries

K2GG, etc.

Matrices defined on DMIG Bulk Data entries and referenced by the K2GG, M2GG, B2GG, K42GG, A2GG, K2PP, M2PP, B2PP, or P2G Case Control commands

MATPi

Matrices defined on DMIG Bulk Data entries and intended for the p-set

MATGi

Matrices defined on DMIG Bulk Data entries and intended for the g-set

RMATG

Rectangular matrix defined on DMIG Bulk Data entries and can have an arbitrary number of columns but g-set rows, similar to P2G

MATKi

Matrices defined on DMIK Bulk Data entries

MATJi

Matrices defined on DMIJ Bulk Data entries

MATIi

Matrices defined on DMIJI Bulk Data entries

Parameters: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

LUSETD

Input-integer-no default. The number of degrees-of-freedom in the p-set.

NONAMEi

Output-integer-default=-1. NAMEi generation flag. Set to +1 if NAMEi is generated; -1 otherwise.

NOK2, etc.

Output-integer-default=-1. K2GG, and so on, generation flag. Set to +1 if K2GG, and so on is generated; -1 otherwise.

IOPT

Input-integer-default=0. Case Control command selection flag. 0

No Case Control command selection (see Form 1) or K2GG, and so on, and TFL Case Control command selection (see Form 2)

1

K2GG, and so on, Case Control command selection (see Form 2)

2

P2G Case Control command selection (see Form 3)

3

DMIK selection by output data block name (see Form 4)

4

DMIJ selection by output data block name (see Form 4)

5

DMIJI selection by output data block name (see Form 4)

10

K2PP, M2PP, and B2PP selection by input parameter value (see Form 5)

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11

K2GG, M2GG, B2GG, K42GG, and A2GG selection by input parameter value (see Form 5)

12

P2G selection by input parameter value (see Form 5)

13

DMIK selection by input parameter value (see Form 6)

14

DMIJ selection by input parameter value (see Form 6)

15

DMIJI selection by input parameter value (see Form 6)

LKSET LJSET, LISET

Output-integer-default=0. Size of ks-set, js-set, and inteference js-set extracted from the AEBGPTK, AEBGPDTJ and AEBGPDTI tables.

NOMATi

Output-integer-default=1. Generation flag. Set to +1 if MAT* is generated; 1 otherwise.

MATNAMi

Input-character-default=’ ’ Matrix name found on DMIG, DMIJ, DMIK, and DMIJI Bulk Data entries.

TFLID

Input-integer-default=0. Transfer function set identification number. TFLID is ignored if IOPT=3, 4, 5, 13, 14, or 15.

NFEXIT

Input-logical-default=TRUE. Termination flag. If FALSE, do not issue User Fatal Message 2070 and do not terminate the module if the matrix is not found.

Remarks: 1. Any output data block can be purged. 2. Form 1 is used to input matrices from DMIG entries named in the DMAP statement output section. No Case Control commands are required. 3. Forms 2 and 3 are used to select the matrices with Case Control commands: K2GG, M2GG, B2GG, K42GG, A2GG, K2PP, M2PP, B2PP, or P2G. “-2GG” matrices are of dimension g by g. “-2PP” matrices are of dimension p by p. The P2G matrix has g-rows, with the number of columns determined by the several methods used to input rectangular matrices described on the DMIG entry. 4. if the output data blocks are specified on a CALL statement and the DMIIN module is specified in the subDMAP referenced by the CALL statement, the data block name specified on the CALL statement must be the same as the name specified on the DMIIN module.

Examples: 1. Assume the Bulk Data contains two DMIG matrices, named M1 and M2, which reference grid and/or scalar points only. The following set of DMAP instructions generate these two matrices in matrix format, multiply them, and print the result. MTRXIN ,,MATPOOL,EQEXIN,,/Ml,M2,,,/LUSET/S,N,NOMl/S,N,NOM2$ IF (NOM1 > -1 AND NOM2 > -1) THEN $ MPYAD M1,M2,/PRODUCT $ MATPRN PRODUCT//$

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ENDIF $

2. Assume the Bulk Data contains two DMIG matrices, MASS and STIFF, which reference grid and/or scalar points only. The following Case Control and DMAP instructions generate these two matrices in matrix format and add them to the structural mass and stiffness. Case Control: M2GG = MASS K2GG = STIFF

DMAP instructions: MTRXIN

CASECC,MATPOOL,EQEXIN,,/STIFF,MASS,,,/ LUSET/S,N,NOSTIFF/S,N,NOMASS///1 $ IF (NOSTIFF > -1) THEN $ ADD KGG,STIFF/KGGNEW $ EQUIVX KGGNEW/KGG/ALWAYS $ ENDIF $ IF (NOMASS > -1) THEN $ ADD MGG,MASS/MGGNEW $ EQUIVX MGGNEW/MGG/ALWAYS $ ENDIF

9.247 NASSETS Combines all element sets for MSGMESH, and sets defined on SET1 Combines all element sets defined in Case Control, including OUTPUT(PLOT) sections, for MSGMESH, and sets defined on SET1 Bulk Data entries.

Format: NASSETS

CASECC,ELSET,EDT/ SET/ MESHSET $

Input Data Blocks: CASECC

Table of Case Control command images

ELSET

Table of element sets defined in OUTPUT(POST) or SETS DEFINITION section of Case Control

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

Output Data Blocks: SET

Table of combined sets

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Parameter: MESHSET

Input-integer-default=0. MSGMESH set processing flag. If nonzero, combine mesh sets defined in the MSGMESH punch file.

9.248 NLCOMB Consolidates tables related to nonlinear elements and applied loads Consolidates tables related to nonlinear elements and applied loads for the current nonlinear analysis iteration.

Format: NLCOMB

CASECC,ESTNL,KDICTNL,BKDICT,ETT,PTELEM0, UNUSED8,MPT,EQEXIN,SLT,DLT,BGPDT/ ELDATA,{SLT1 or DLT1}/ NSKIP/LSTEP/LINC/STATIC/LGDISP/OSTEP $

Input Data Blocks: CASECC

Table of Case Control command images

EST

Element summary table containing geometric and/or material nonlinear elements

KDICTNL

KELMNL dictionary table

BKDICT

BKELM dictionary table

ETT

Element temperature table

PTELEM0

Table of thermal loads in the elemental coordinate system from prior subcase

PTELEM

Table of thermal loads in the elemental coordinate system for the current subcase

UNUSED8

Not used and can be purged

MPT

Table of Bulk Data entry images related to material properties

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

SLT

Table of static loads

DLT

Table of dynamic loads

BGPDT

Basic grid point definition table

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Output Data Blocks: ELDATA

Table of combined nonlinear information data

SLT1

Table of static loads updated for nonlinear analysis

DLT1

Table of dynamic loads updated for nonlinear analysis

Parameters: NSKIP

Input-integer-no default. Subcase record number to read in CASECC.

LSTEP

Input-integer-no default. Load step. The current iteration step at the subcase level for static solutions.

LINC

Input-integer-no default. Number of load increments for this subcase.

STATIC

Input-integer-default=0. Static analysis flag. Set to zero for static analysis and one for dynamic analysis.

LGDISP

Input-integer-default=0. Large displacement flag. Set to 1 for large displacement analysis.

OSTEP

Input-integer-default=0. Restart step number.

9.249 NLITER Computes nonlinear analysis solution matrices and tables Computes nonlinear analysis solution matrices and tables. Applicable to static structural or steady state heat transfer analysis.

Format: NLITER

CASECC,CNVTST,PLMAT,YSMAT,KAAL, ELDATA,KELMNL,LLLT,GM,MPT, DIT,MGG,SLT1,CSTM,BGPDT, SIL,USET,RDEST,RECM,KGGNL, ULLT,GPSNT,EDT,DITID,DEQIND, DEQATN,FENL,EPT,PCOMPT/ UGNI,FGNL,ESTNLH,CIDATA,QNV, FFGH,MUGNI,MESTNL,DUGNI,BTOPCNV, BTOPSTF,FENL1/ S,N,LOADFAC/S,N,CONV/S,N,RSTEP/S,N,NEWP/ S,N,NEWK/S,N,POUTF/S,N,NSKIP/LGDISP/ S,N,NLFLAG/S,N,ITERID/S,N,KMATUP/S,N,LSTEP/ S,N,KTIME/S,N,SOLCUR/TABS/ S,N,KFLAG/S,N,NBIS/NORADMAT/S,N,LASTCNMU/ SIGMA/S,N,ARCLG/S,N,ARCSIGN/S,N,TWODIV/ LANGLE/S,N,ITOPT/S,N,ITSEPS/ITSMAX/ S,N,PLSIZE/IPAD/IEXT/ S,N,ADPCON/PBCONT/S,N,NBCONT/GPFORCE $

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Input Data Blocks: CASECC

Table of Case Control command images

CNVTST

Convergence test matrix

PLMAT

Initial and final load matrices for subcase

YSMAT

Initial and final enforced displacement matrices

KAAL

Element stiffness matrix for linear elements only reduced to a-set

ELDATA

Table of combined nonlinear information data

KELMNL

Table of element matrices for stiffness for nonlinear elements

LLLT

Lower triangular factor for nonlinear elements including material, slideline, and differential stiffness effects

GM

Multipoint constraint transformation matrix, m-set by n-set

MPT

Table of Bulk Data entry images related to material properties

DIT

Table of TABLEij Bulk Data entry images

MGG

Radiation matrix in g-size

SLT1

Table of static loads updated for nonlinear analysis

CSTM

Table of coordinate system transformation matrices

BGPDT

Basic grid point definition table

SIL

Scalar index list

USET

Degree-of-freedom set membership table for g-set

RDEST

Radiation element summary table

RECM

Radiation exchange coefficient matrix

KGGNL

Stiffness matrix in g-set for material nonlinear elements only

ULLT

Upper triangular factor for nonlinear elements including material, slideline, and differential stiffness effects

GPSNT

Grid point shell normal table

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

DITID

Table of identification numbers in DIT

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DEQIND

Index table to DEQATN data block

DEQATN

Table of DEQATN Bulk Data entry images

FENL

Strain energy and grid point force at every element from the previous load step in nonlinear matrix format

EPT

Table of Bulk Data entry images related to element properties

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry

Output Data Blocks: UGNI

Displacement matrix at converged step in the g-set

FGNL

Nonlinear element force matrix from the last iteration

ESTNLH

Nonlinear element summary table at converged step

CIDATA

Miscellaneous data for controlled increment method

QNV

Quasi-Newton sweeping vectors

FFGH

Follower force for OLOAD output

MUGNI

Displacement matrix for stiffness update

MESTNL

Nonlinear element summary table at current step

DUGNI

Incremental displacement matrix between the last two converged steps

BTOPOCNV

Updated contact regions input information table

BTOPOSTF

Updated contact regions topological information table

FENL1

Strain energy and grid point force at every element at the current load step in nonlinear matrix format

Parameters: LOADFAC

Input/output-complex-no default. Load factor. The real part is the load factor for the current iteration, having a fractional value between 0 and 1.

CONV

Input/output-integer-default=0. Nonlinear analysis convergence flag. On input: 0

Initialization

On output:

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-1

Convergence has not been achieved.

1

Convergence has been achieved.

RSTEP

Input/output-integer-default=0. Controlled increments counter.

NEWP

Input/output-integer-default=1. New subcase flag.

NEWK

-1

Current subcase has not been completed.

1

Current subcase has been completed.

Output-integer-default=1. Stiffness update flag. -1

Do not update stiffness.

1

Update stiffness.

2

Update stiffness, the solution is diverging and MAXBIS has been reached.

POUTF

Output-integer-default=1. Intermediate output flag. Set to -1 if intermediate output is not requested.

NSKIP

Input/output-integer-no default. On input: Subcase record number to read in CASECC. On output: Set to -2 if run is to be fatally terminated.

LGDISP

Input-integer-no default. Large displacement and follower force flag. -1

No large displacement and follower force effects are considered.

1

Large displacement and follower force effects are considered.

2

Only large displacement effects are considered.

NLFLAG

Output-integer-default=0

ITERID

Input/output-integer-no default. Nonlinear analysis iteration count.

KMATUP

Input/output-integer-default=1. Stiffness matrix update count within the increment.

LSTEP

Input/output-integer-default=0. Load step. The current iteration step at the subcase level for static solutions.

KTIME

Input/output-real-no default. CPU time remaining. If KTIME is positive, KTIME is the time remaining at the start of the stiffness update. If negative, no stiffness update was done since the last exit from NLITER. KTIME still holds the negative of the stiffness update time from the last stiffness update.

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SOLCUR

Input/output-integer-default=0. Nonlinear loop identification number.

TABS

Input-real-default=0.0. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius or 459.69 in Fahrenheit.

KFLAG

Input/output-integer-default=1. Stiffness update flag. Set to -1 to update stiffness before starting bisection. It reflects the NEWK and CONV status at the last converged solution or stiffness update. See Remark 6.

NBIS

Input/output-integer-default=0. Current bisection counter.

NORADMAT

Input-integer-default=0. Radiation flag. -2

No radiation

-1

Initial radiation

1

Single band radiation with constant emissivity

2

Radiation with temperature dependent emissivity

3

Multiple band radiation with constant emissivity

LASTCNMU

Input/output-real-default=0.0. Last converged value of the arc-length load factor.

SIGMA

Input-real-default=1.0. The Stefan-Boltzmann constant. Used to compute radiant heat flux.

ARCLG

Input/output-real-default=1.0. The arc length at the last converged step.

ARCSGN

Input/output-integer-default=1. The sign of PDDP at the beginning of the subcase. This is used in restarts in the post-buckling region.

TWODIV

Input/output-integer-default=0. Nonlinear analysis divergence flag.

LANGLE

0

No previous divergence on this load step

1

One previous divergence on this load step

Input-integer-default=1. Large rotation calculation method: 1

Gimbal angle

2

Rotation vector

ITOPT

Input-integer-default=0. Preconditioner method for iterative solver. See the “SOLVIT” module description.

ITSEPS

Input/output-integer-default=0. Power of ten for convergence parameter epsilon for iterative solution method. On output, set to 0 for convergence and 1 for no convergence.

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ITSMAX

Input-integer-default=0. Maximum number of iterations for iterative solution method.

PLSIZE

Input/output-integer-default=0. Size of the load matrix. Compared to the size of load matrix in the previous subcase in order to detect boundary condition changes in the current subcase. Boundary condition changes are not allowed in the arc-length method.

IPAD

Input-integer-default=0. Padding level for reduced incomplete Cholesky factorization. See the “SOLVIT” module description.

IEXT

Input-integer-default=0. Extraction level for reduced incomplete Coolest factorization. See the “SOLVIT” module description.

ADPCON

Input-real-default=0.0. Contact penalty value. Scale factor for adjusting penalty values on restart. Update penalty values if positive.

PBCONT

Input-integer-default=0. Slideline contact flag.

NBCONT

Output-integer-default=0. Number of bisections due to slideline contact.

GPFORCE

Input-integer-default=-1. The number of columns in FENL. If GPFORCE is less than or equal to zero, no GPFORCE or ESE command is present.

Remarks: 1. NLITER updates the displacement vector for as many iterations as are necessary to attain an equilibrium between the applied loads and the forces. NLITER calculates nonlinear forces and follower forces which are used to obtain new displacements until a converged solution is found, or a new stiffness matrix is necessary, or a bisection of the load step is necessary. 2. KGGNL is needed for the reduced incomplete Cholesky factorization in the iterative solver only. Otherwise it can be purged. 3. MGG, RDEST, RECM are required only for heat transfer analysis. Otherwise, they can be purged. 4. ULLT is required only for unsymmetric stiffness. Otherwise, it can be purged. 5. TABS is required for creep analysis. 6. KFLAG is explained iln more detail below:

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-1

Solution had converged, but no stiffness update had been made or solution had not converged, and a stiffness matrix update had been made. A new stiffness matrix is required before starting bisection.

1

Solution had converged and a stiffness update had been made. No new stiffness matrix is required before starting bisection.

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9.250 NLTRD Computes transient nonlinear analysis solution matrices and tables Computes transient nonlinear analysis solution matrices and tables. Applicable to dynamic structural analysis only.

Format: NLTRD

CASECC,MESTNL,PDT,YS,KRDD, ELDATA,KELMNL,LAM1DD,GM,MPT, DIT,UAM1DD,DLT1,CSTM,BGPDT, SIL,USETD,AM2,AM3,NLFT, KSGG,DITID/ ULNT,IFG,ESTNLH,IFD,OESNL1, PNL,TEL/ BETA/S,N,CONV/S,N,STIME/S,N,NEWP/S,N,NEWK/ S,N,OLDDT/S,N,NSTEP/LGDISP/S,N,CONSEC/S,N,ITERID/ S,N,MU/S,N,KTIME/S,N,LASTUPD/S,N,NOGONL/ S,N,NOTIME/MAXLP/UNUSED17/UNUSE18/UNUSE19/ TABS/LANGLE $

Input Data Blocks: CASECC

Table of Case Control command images

MESTNL

Nonlinear element summary table at current step

PDT

Dynamic load vectors for transient analysis in the d-set

YS

Matrix of enforced displacements or temperatures

KRDD

Combined linear and material nonlinear stiffness matrix in the d-set

ELDATA

Table of combined nonlinear information data

KELMNL

Table of element matrices for stiffness for nonlinear elements

LAM1DD

Lower triangular factor of the dynamic tangential matrix in the d-set

GM

Multipoint constraint transformation matrix, m-set by n-set

MPT

Table of Bulk Data entry images related to material properties

DIT

Table of TABLEij Bulk Data entry images

UAM1DD

Upper triangular factor of the dynamic tangential matrix in the d-set

DLT1

Table of dynamic loads updated for nonlinear analysis

CSTM

Table of coordinate system transformation matrices

BGPDT

Basic grid point definition table

SIL

Scalar index list

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USETD

Degree-of-freedom set membership table for the p-set

AM2

Damping matrix in the d-set for linear elements multiplied by the negative of the time step delta

AM3

Combined mass and damping matrix multiplied the square of the reciprocal of the time step delta and the reciprocal of twice the time step delta, respectively

NLFT

Nonlinear Forcing function table

KSGG

S-set by f-set matrix and s-set by s-set partitions of the material nonlinear stiffness matrix and expanded to g-set size

DITID

Table of identification numbers in DIT

Output Data Blocks: ULNT

Solution matrix from nonlinear transient response analysis in the d-set

IFG

Matrix of nonlinear element forces for the g-set at the output time steps

ESTNLH

Nonlinear element summary table at converged step

IFD

Matrix of nonlinear element forces at constrained points at the output time steps

OESNL1

Table of nonlinear element stresses in SORT1 format

PNL

Nonlinear load matrix appended from each output time step

TEL

Transient response time output list appended from each subcase

Parameters: BETA

Input-complex-default=(.33333,0.0). Integration parameter.

CONV

Input/output-integer-default=1. Nonlinear analysis convergence flag. On input: 0

Initialization

On output:

STIME NEWP

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Convergence has not been achieved.

1

Convergence has been achieved.

Input/output-real-default=0.0. On initial input, starting time step and on output, accumulated time used for restarts. Output-integer-default=1. New subcase flag.

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NEWK

-1

Current subcase has not been completed.

1

Current subcase has been completed.

Input/output-integer-default=1. Stiffness update flag. -1

Do not update stiffness.

>0

Update stiffness. Represents the number of consecutive time steps which have shown divergence. If this number reaches 5, the solution process is terminated.

OLDDT

Input/output-real-default=0.0. Time step increment used in the previous iteration or time step to be used after the matrix update or subcase switch.

NSTEP

Input/output-integer-default=0. Current time step position for subcase, set to 0 at the beginning of the subcase.

LGDISP

Input-integer-no default. Large displacement and follower force flag. -1

No large displacement and follower force effects aree considered.

1

Large displacement and follower force effects are considered.

2

Only large displacement effects are considered.

CONSEC

Input/output-integer-default=0. A composite number equal to 10*(value of NSTEP the last time MAXBIS was reached) + (the number of consecutive time steps which have reached MAXBIS). If CONSEC=5, solution process is terminated.

ITERID

Input/output-integer-no default. Nonlinear analysis iteration count.

MU

Input/output-real-default=0.0. The magnitude of the last g-set displacement matrix.

KTIME

Input/output-real-no default. CPU time remaining. If KTIME is positive, KTIME is the time remaining at the start of the stiffness update. If negative, no stiffness update was done since the last exit from NLITER. KTIME still holds the negative of the stiffness update time from the last stiffness update.

LASTUPD

Input/output-integer-default=0. The time step number of the last stiffness update. Set to 0 if the stiffness update is performed due to the CGAP element during the iteration.

NOGONL

Output-integer-default=0. Nonlinear "no-go" flag. Set to +1 to continue or -1 to terminate.

NOTIME

Output-integer-default=0. Time out flag. Set to 1 if there is no time left for further iterations but enough time to perform data recovery.

MAXLP

Input-integer-default=0. Maximum limit allowed for element relaxation iteration and the material subincrement processes.

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UNUSED17

Input-integer-default=0. Unused.

UNUSED18

Input-integer-default=0. Unused.

UNUSED19

Input-integer-default=0. Unused.

TABS

Input-real-default=0.0. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius or 459.69 in Fahrenheit.

LANGLE

Input-integer-default=1. Large rotation calculation method: 1

Gimbal angle

2

Rotation vector

Remarks: 1. NLTRD supports only METHOD="AUTO" and "TSTEP" on the TSTEPNL Bulk Data entry. NLTRD2 supports only METHOD="ADAPT". 2. NLTRD does not support heat transfer, slideline contact, or shell normals. Use NLTRD2. 3. ULNT contains only displacement and velocity vectors at converged time steps during the direct integration. However, upon completion of the subcase, it also contains acceleration for the output time steps.

9.251 NLTRD2 Computes transient nonlinear analysis solution matrices and tables Computes transient nonlinear analysis solution matrices and tables. Applicable to dynamic structural or transient heat transfer analysis.

Format: NLTRD2

CASECC,PDT,YS,ELDATA,KELMNL, KDD,GM,MPT,DIT,KBDD, DLT1,CSTM,BGPDT,SIL,USETD, BRDD,MDD,NLFT,RDEST,RECM, BDD,GPSNT,DITID,DEQIND,DEQATN/ ULNT,IFS,ESTNLH,IFD,OESNL1, PNL,TEL,MULNT,MESTNL,BTOPCNV, BTOPSTF,OESNLB1/ KRATIO/S,N,CONV/S,N,STIME/S,N,NEWP/S,N,NEWK/ S,N,OLDDT/S,N,NSTEP/LGDISP /S,N,CONSEC/S,N,ITERID/ ITIME/S,N,KTIME/S,N,LASTUPD/S,N,NOGONL/S,N,NBIS/ MAXLP/TSTATIC/LANGLE/NDAMP/TABS/ SIGMA/NORADMAT/S,N,ADPCON/PBCONT/ S,N,NBCONT $

Input Data Blocks: CASECC

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Table of Case Control command images

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PDT

Dynamic load vectors for transient analysis in the d-set

YS

Matrix of enforced displacements or temperatures

ELDATA

Table of combined nonlinear information data

KELMNL

Table of element matrices for stiffness for nonlinear elements

KDD

Stiffness matrix for the d-set, linear elements only

GM

Multipoint constraint transformation matrix, m-set by n-set

MPT

Table of Bulk Data entry images related to material properties

DIT

Table of TABLEij Bulk Data entry images

KBDD

Tangential stiffness in d-set

DLT1

Table of dynamic loads updated for nonlinear analysis

CSTM

Table of coordinate system transformation matrices

BGPDT

Basic grid point definition table

SIL

Scalar index list

USETD

Degree-of-freedom set membership table for the p-set

BRDD

Damping matrix in the d-set for linear elements only or heat capacitance matrix for both linear and nonlinear elements in the d-set

MDD

Mass (or radiation) matrix for the d-set

NLFT

Nonlinear Forcing function table

RDEST

Radiation element summary table

RECM

Radiation exchange coefficient matrix

BDD

Damping (or heat capacitance) matrix for the d-set for linear elements only

GPSNT

Grid point shell normal table

DITID

Table of identification numbers in DIT

DEQIND

Index table to DEQATN data block

DEQATN

Table of DEQATN Bulk Data entry images

Output Data Blocks: ULNT

Solution matrix from nonlinear transient response analysis in the d-set

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IFS

Matrix of nonlinear element forces at constrained points at the output time steps

ESTNLH

Nonlinear element summary table at converged step

IFD

Matrix of nonlinear element forces at constrained points at the output time steps

OESNL1

Table of nonlinear element stresses in SORT1 format

PNL

Nonlinear load matrix appended from each output time step

TEL

Transient response time output list appended from each subcase

MULNT

Solution matrix from nonlinear transient response analysis in the d-set from the previous subcase

MESTNL

Nonlinear element summary table at current step

BTOPOCNV

Updated contact regions input information table

BTOPOSTF

Updated contact regions topological information table

OESNLB1

Table of slideline contact element stresses in SORT1 format

Parameters: KRATIO

Input/output-complex-default=(1.,0.). Stiffness ratio to be used for time step adjustment.

CONV

Input/output-integer-default=1. Nonlinear analysis convergence flag. On input: 0

Initialization

On output: -1 Convergence has not been achieved. 1

Convergence has been achieved.

STIME

Input/output-real-default=0.0. On initial input, starting time step and on output, accumulated time used for restarts.

NEWP

Output-integer-default=1. New subcase flag. -1 Current subcase has not been completed. 1

NEWK

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Current subcase has been completed.

Input/output-integer-default=1. Stiffness update flag.

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-1 Do not update stiffness. >0 Update stiffness. Represents the number of consecutive time steps which have shown divergence. If this number reaches 5, the solution process is terminated. OLDDT

Input/output-real-default=0.0. Time step increment used in the previous iteration or time step to be used after the matrix update or subcase switch.

NSTEP

Input/output-integer-default=0. Current time step position for subcase, set to 0 at the beginning of the subcase.

LGDISP

Input-integer-no default. Large displacement and follower force flag. -1 No large displacement and follower force effects are considered. 1

Large displacement and follower force effects are considered.

2

Only large displacement effects are considered.

CONSEC

Input/output-integer-default=0. A composite number equal to 10*(value of NSTEP the last time MAXBIS was reached) + (the number of consecutive time steps which have reached MAXBIS). If CONSEC=5, the solution process is terminated.

ITERID

Input/output-integer-no default. Nonlinear analysis iteration count.

ITIME

Input-real-default=0.0. Initial time step at the beginning of a subcase.

KTIME

Input/output-real-no default. CPU time remaining. If KTIME is positive, KTIME is the time remaining at the start of the stiffness update. If negative, no stiffness update was done since the last exit from NLITER. KTIME still holds the negative of the stiffness update time from the last stiffness update.

LASTUPD

Input/output-integer-default=0. The time step number of the last stiffness update. Set to 0 if the stiffness update is performed due to the CGAP element during the iteration.

NOGONL

Output-integer-default=0. Nonlinear "no-go" flag. Set to +1 to continue or -1 to terminate.

NBIS

Input/output-integer-default=0. Current bisection counter.

MAXLP

Input-integer-default=0. Maximum limit allowed for element relaxation iteration and the material subincrement processes.

TSTATIC

Input-integer-default=-1. Static analysis flag. Set to 1 to ignore inertia and damping forces.

LANGLE

Input-integer-default=1. Large rotation calculation method: 1

Gimbal angle

2

Rotation vector

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NDAMP

Input-real-default=0.0. Numerical damping.

TABS

Input-real-default=0.0. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius or 459.69 in Fahrenheit.

SIGMA

Input-real-default=1.0. The Stefan-Boltzmann constant. Used to compute radiant heat flux.

NORADMAT

Input-integer-default=0. Radiation flag. -2 No radiation -1 Initial radiation 1

Single band radiation with constant emissivity

2

Radiation with temperature dependent emissivity

3

Multiple band radiation with constant emissivity

ADPCON

Input-real-default=0.0. Contact penalty value. Scale factor for adjusting penalty values on restart. Update penalty values if positive.

PBCONT

Input-integer-default=0. Slideline contact flag.

NBCONT

Input/output-integer-default=0. Number of bisections due to slideline contact.

Remarks: 1. NLTRD2 utilizes an automatic method of time integration to compute solutions to nonlinear transient problems (METHOD="ADAPT" on the TSTEPNL Bulk Data entry). NLTRD2 performs the time increment and the vector iteration steps until convergence has been attained. NLTRD2 uses line search and quasi-Newton vector techniques when appropriate. 2. NLTRD2 supports only METHOD="ADAPT". NLTRD supports only METHOD="AUTO" and "TSTEP" on the TSTEPNL Bulk Data entry. 3. ULNT contains only displacement and velocity vectors at converged time steps during the direct integration. However, upon completion of the subcase, it also contains acceleration for the output time steps. For thermal analysis, the displacements, velocity and accelerations are temperature, enthalpy, and the enthalpy time derivative.

9.252 NORM Normalize a matrix To normalize a matrix, each column by its largest element or compute the square root of the sum of the squares for each row of a matrix (SRSS).

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Format: NORM

A/ANORM/S,N,NCOL/S,N,NROW/S,N,XNORM/IOPT/ S,N,XNORMD/PRTSWM $

Input Data Block: A

Any matrix (real or complex)

Output Data Block: ANORM

Normalized matrix

Parameters: NCOL

Number of columns in A

NROW

Integer-output-default=0. Number of rows in A.

XNORM

Real-output-default=0.0. Maximum absolute normalizing value over all columns.

IOPT

Integer-input-default=1. Normalization option. 1

Normalize by largest element

2

Compute SRSS

XNORMD

Real double precision-output-default=0.D0. Same as XNORM except in double precision.

PRTSWM

Logical-input-default=TRUE. If PRTSUM=FALSE, System Warning Message 6991 is suppressed. This message is printed when the maximum term exceeds the single precision limit for the machine type. When it is TRUE, the message is printed.

Remarks: 1. If IOPT=1, ANORM is the same as A except each column has been normalized by its maximum absolute value. 2. If IOPT=2, ANORM is a column vector where the i-th row is the sum of the magnitudes of the terms in the i-th row of A.

Examples: 1. Normalize PHIG so that the maximum deflection is 1.0 (or -1.0). NORM

PHIG/PHIG1 $

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2. Compute complex eigenvectors that have been normalized such that the product[CPHG]T [CPHG] produces a square matrix with off-diagonal terms of computational zero, and complex diagonal terms whose magnitude is unity. TRNSP NORM MATMOD DIAGONAL MPYAD MPYAD DIAGONAL

CPHG/CPHGT $ CPHGT/CX2////2 $ CX2,,,,,/INORM22,/28 $ DIAGONALIZE INORM22/NORM22/‘WHOLE‘/-1.0 $ INVERT CPHG,NORM22,/CPHGNORM $ NORMALIZE CPHGNORM,CPHGNORM,/N22/1 $ SHOULD BE IDENTITY IN MAGNITUDE N22/N22MAG/‘WHOLE‘/1.0 $ FIND MAGNITUDES

9.253 NXNADAMS Creates an ADAMS MNF for a superelement. Creates an ADAMS Modal Neutral File (MNF) for a superelement. The output is based on the definitions in the ADAMSMNF case control command and the DTI,UNITS bulk data entry.

Format: NXNADAMS

UNITS,CASES,BGPDTS,GEOM2,GEOM4,USET,LAMA,PHIG, MGGDIAG,PCDB,OGPWG,OGSR1,OGSTRR1,CSTMS,EMVD// SEID/FLXONL/FLXERR/WTMASS/GRDPNT $

Input Data Blocks: UNITS

UNITS data block from the DTI,UNITS bulk data entry

CASES

Case Control table associated with superelement

BGPDTS

Basic Grid Point Definition Table associated with superelement

GEOM2

Table of Bulk Data entries related to element connectivity

GEOM4

Table of Bulk Data entries related to constraints

USET

Table of degree-of-freedom sets

LAMA

Eigenvalue summary table for superelement

PHIG

Matrix of eigenvectors (g-set size) corresponding to LAMA

MGGDIAG

Column vector of diagonal values from superelement mass matrix (g-set size)

PCDB

Plot Control Data Block from OUTPUT(PLOT) case control

OGPWG

Output table of Grid Point Weight Generator of superelement

OGSR1

Output table of grid point stresses of superelement

OGSTRR1

Output table of grid point strains of superelement

CSTMS

Coordinate System Transformation Matrices for superelement

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EMVD

Equivalent modal viscous damping vector.

Parameters: SEID

Input-integer-default=0. Superelement ID number (0 for residual-only analysis).

FLXONL

Output-integer-no default. Value of FLEXONLY keyword from ADAMSMNF case control command. Options are: 0: Continue with solution of residual structure 1: Do not perform solution of residual structure

FLXERR

Output-integer-no default. Error flag. Options are: 0: No error 1: Error occurred creating MNF. Terminate processing.

WTMASS

Input-real-default=1.0. Value of WTMASS parameter from PARAM,WTMASS,value.

GRDPNT

Input-integer-default=-1. Value of GRDPNT parameter from PARAM,GRDPNT,value.

Remarks: The MNF naming convention is as follows: ‘jid_SEID.mnf’, where jid is the “job ID” of the run (that is, the name of the job input file) and SEID is the superelement ID number (that is, the SEID parameter). The location of the created MNF is the same as the jid.f06 file.

9.254 NXNMATLB Creates an MATLAB .m script file for a superelement. Creates an MATLAB .m script file for a superelement. The output is based on the MBDEXPORT case control command with the MATLAB describer specified.

Format: For the STANDARD case control option: NXNMATLB

CASES,LAMA,PHIG,EMVD,U8DOF,MFORC,// SEID/WTMASS/FLXERR $

For the STATESPACE case control option: NXNMATLB

CASES,AMAT,BMAT,CMAT,EMAT,U7DOF,U8DOF// SEID/WTMASS/FLXERR $

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Input Data Blocks: CASES

Case control table associated with superelement.

LAMA

Eigenvalue summary table for superelement.

PHIG

Mode shape matrix (U8-set) for superelement.

EMVD

Equivalent modal viscous damping matrix for superelement.

AMAT

State-space [A] matrix for superelement.

BMAT

State-space [B] matrix for superelement.

CMAT

State-space [C] matrix for superelement.

EMAT

State-space [E] matrix for superelement.

U7DOF

U7-set DOF vector (input DOF) for superelement.

U8DOF

U8-set DOF vector (output DOF) for superelement.

MFORC

Modal force vector for superelement.

Parameters: SEID

Input-integer-no default. Superelement ID number.

WTMASS

Input-real-no default. Value of WTMASS parameter from PARAM,WTMASS,value.

FLXERR

Output-integer-no default. Error flag. Options are: 0: No error 1: Error

Remarks: This module will generate a MATLAB .m script file.

9.255 NXNRFI Creates a RecurDyn Flex Input (RFI) file for a superelement. Creates a RecurDyn Flex Input (RFI) file for a superelement. The output is based on the definitions in the RECURDYNRFI case control command and the DTI,UNITS bulk data entry.

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Format: NXNRFI

UNITS,CASES,BGPDTS,GEOM2,GEOM4,USET,LAMA,PHIG, MGGDIAG,PCDB,OGPWG,OGSR1,OGSTRR1,CSTMS// SEID/FLXONL/FLXERR/WTMASS/GRDPNT $

Input Data Blocks: UNITS

UNITS data block from the DTI,UNITS bulk data entry

CASES

Case Control table associated with superelement

BGPDTS

Basic Grid Point Definition Table associated with superelement

GEOM2

Table of Bulk Data entries related to element connectivity

GEOM4

Table of Bulk Data entries related to constraints

USET

Table of degree-of-freedom sets

LAMA

Eigenvalue summary table for superelement

PHIG

Matrix of eigenvectors (g-set size) corresponding to LAMA

MGGDIAG

Column vector of diagonal values from superelement mass matrix (g-set size)

PCDB

Plot Control Data Block from OUTPUT(PLOT) case control

OGPWG

Output table of Grid Point Weight Generator of superelement

OGSR1

Output table of grid point stresses of superelement

OGSTRR1

Output table of grid point strains of superelement

CSTMS

Coordinate System Transformation Matrices for superelement

Parameters: SEID

Input-integer-default=0. Superelement ID number (0 for residual-only analysis).

FLXONL

Output-integer-no default. Value of FLEXONLY keyword from RECURDYNRFI case control command. Options are: 0: Continue with solution of residual structure 1: Do not perform solution of residual structure

FLXERR

Output-integer-no default. Error flag. Options are: 0: No error 1: Error occurred creating RFI. Terminate processing.

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WTMASS

Input-real-default=1.0. Value of WTMASS parameter from PARAM,WTMASS,value.

GRDPNT

Input-integer-default=-1. Value of GRDPNT parameter from PARAM,GRDPNT,value.

Remarks: The RFI naming convention is as follows: ‘jid_SEID.rfi’, where jid is the “job ID” of the run (that is, the name of the job input file) and SEID is the superelement ID number (that is, the SEID parameter). The location of the created RFI is the same as the jid.f06 file.

9.256 OFP Output file processor Outputs (print or punch) data blocks prepared by other modules in user-oriented, self-explanatory formats.

Format: OFP

OFP1,OFP2,OFP3,OFP4,OFP5,OFP6, CSTM,EHT,BGPDTVU,ERROR1,DEQATN,DEQIND,DIT// S,N,CARDNO/ODCODE/PVALID/DFLAG/VFLAG/AFLAG/ABSEM $

Input Data Blocks: OFPi

Output table suitable for processing by the OFP module. See Remark 2.

CSTM

Table of coordinate system transformation matrices

EHT

Element hierarchical table for p-element analysis

BGPDTVU

Basic grid point definition table for a superelement and related to geometry with view-grids added

ERROR1

Error-estimate table updated for current superelement or adaptivity loop

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

DIT

Table of TABLEDi Bulk Data entry images

Output Data Blocks: None.

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Parameters: CARDNO

Input/output-integer-default=0. Punch file line counter. CARDNO is incremented by one for each line written to the punch file and is also written into columns 73-80 of each line.

ODCODE

Input-integer-default=-1. Output device code override. See Remark 4. ODCODE overrides the code stored in the DBi‘s according to the following table: ODCODE

Output directed to:

1

Print

2

Plot

3

Print and Plot

4

Punch

5

Print and Punch

6

Plot and Punch

7

Print, Plot, and Punch

PVALID

Input-integer-default=0. P-element adaptivity loop identification number.

DFLAG

Input-integer-default=0. Displacement output flag. = 0 output displacement “as is” = 1 output displacement as “relative motion” = 2 do not output displacement

VFLAG

Input-integer-default=0. Velocity output flag. = 0 output velocity “as is” = 1 output velocity as “relative motion” = 2 do not output velocity

AFLAG

Input-integer-default=0. Acceleration output flag. = 0 output acceleration “as is” = 1 output acceleration as “relative motion” = 2 do not output acceleration

ABSEM

Input-integer-default=1. Enforced motion code for header labeling (0=constraint modes method; 1=absolute displacement method).

Remarks: 1. Any or all data blocks can be purged. 2. DMAP modules READ (LAMA, OEIGS, LAMX, CLAMX), CEAD (CLAMA and OCEIGS), and LAMX (LAMB) are matrix operation modules that prepare OFP formatted data blocks. Modules SDR2, SDR3, VDR, VDRE, ADR, CURV, DDRMM, DRMH3, ELFDR, GPFDR,

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GPWG, LAMX, MDATA, SDRCOMP, SDRX, and SDRHT also prepare OFP formatted data blocks. 3. Parameter ODCODE is not honored by data blocks LAMA, OEIGS, LAMX, CLAMA, and OGPWG, which are created by READ, CEAD, LAMX, and GPWG. 4. CSTM, EHT, BGPDTVU, and ERROR1 are required if p-elements are specified and only for data recovery; that is, displacement, stress, strain, and so on. 5. CSTM, DEQATN, DEQIND, and DIT are required if the CORD3G Bulk Data entry is present and only for element data recovery; that is, displacement, stress, strain, and so on.

Example: Print the OUG1 table from the SDR2 module. OFP OUG1/ $

9.257 OPTGP0 p-element analysis preprocessor Preprocesses the input design optimization shape basis vectors for p-element analysis.

Format: OPTGP0

GEOM1M,GEOM2M,MEDGE,EDOM,UNUSED5,UNUSED6,UNUSED7, DEQATN,DEQIND/ EDOMM/ DELG $

Input Data Blocks: GEOM1M

Table of Bulk Data entry images related to geometry and updated for the current p-level

GEOM2M

Table of Bulk Data entry images related to element connectivity and scalar points and updated for the current p-level

MEDGE

Edge table for p-element analysis

EDOM

Table of Bulk Data entries related to design sensitivity and optimization

unused5

Unused and can be purged

unused6

Unused and can be purged

unused7

Unused and can be purged

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

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Output Data Block: EDOMM

Table of Bulk Data entries related to design sensitivity and optimization updated for p-element analysis

Parameter: DELG

Input-real-default=0.1. Scale factor on perturbed length.

Remarks: OPTGP0 preprocesses the shape basis vectors defined at the p-element geometry level for both the GMCURV or POINT option and generates DVGRID entry images at the grid-n points (a point on an FEEDGE, FEFACE or FEBODY entity with variable number of degrees-of-freedom).

9.258 ORTHOG Generates orthonormal set of vectors Generates an orthonormal set of vectors from a given set of vectors. For example, orthogonalize with respect to an identity matrix or mass matrix.

Format: ORTHOG

A,M/ Q,R/ ORTHOPT/ORTHCON/S,N,ORTHEPS/ORTHREPT/ORTHTOL $

Input Data Blocks: A

Rectangular matrix of m columns (vectors) by n rows to be orthogonalized where m≤n

M

Weighting matrix: symmetric and positive definite

Output Data Blocks: Q

Rectangular matrix of orthogonalized vectors

R

Rectangular matrix whose m by m upper triangle contains an intermediate factor of the process

Parameters: ORTHOPT

Input-integer-default=1. Orthogonalization method. 1

And M is purged, perform Householder Orthogonalization.

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2 ORTHCON

Or M is not purged, perform Matrix Modified Gram-Schmidt method. If ORTHOPT=2 and M is purged, an identity matrix is created for M.

Input-integer-default=1. Matrix Modified Gram-Schmidt termination flag or Householder partitioning vector generation flag. For Householder: 0

R contains the upper triangular matrix.

1

R contains the partitioning vector.

For Matrix Modified Gram-Schmidt termination: 0

Exit the program if M is not at least a positive semi-definite matrix. R is not used and can be purged.

1

Let Rii = -Rii and continue, if M is not at least a positive semi-definite matrix. R contains the partitioning vector

ORTHEPS

Output-real-no default. Level of orthogonality. ORTHEPS is the largest lower triangular term of the matrix R and is computed with the Householder method.

ORTHREPT

Input-real-default=0.707. Matrix Modified Gram-Schmidt algorithm repeat flag. The default is approximately the square root of 0.5.

ORTHTOL

Input-real-default=0.0. Linear dependence tolerance. By default, ORTHTOL is set to the square root of the minimum machine value.

Remarks: ORTHOG generates an orthonormal set of vectors [Q] from a given set of vectors [A] such that: [A] = [Q][R] and if [M] is not given: [Q]T[M] [Q] = [I] or if [M] is not given: [Q]T[Q] = [I] where [I] is an identity matrix.

9.259 OUTPRT Constructs sparse load reduction and sparse data recovery partitioning vectors.

Format: OUTPRT

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CASECC,ECT,BGPDT,SIL,XYCDB,DYNAMIC,MATPOOL,PG,VGFD, TABEVP,TABEVS,SETMC,TEXTSE/ PVGRID,PVSPC,PVMPC,PVLOAD,PVCODES,TEXTOU/ S,N,SDRMETH/NOSE/SDROVR/SDRDENS/MCSET/ MCFLAG/IRTYPE/MATTYP/APP $

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

Input Data Blocks: CASECC

Table of Case Control command images

ECT

Element connectivity table

BGPDT

Basic grid point definition table

SIL

Scalar index list

XYCDB

Table of x-y plotting commands

DYNAMIC

Table of Bulk Data entry images related to dynamics

MATPOOL

Table of Bulk Data entry images related to hydroelastic boundary, heat transfer radiation, virtual mass, DMIG, and DMIAX entries

PG

Static load matrix applied to the g-set

VGFD

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to frequency-dependent elements

TABEVP

Cross-reference table between ESTDVP records and element and design variable identification numbers

TABEVS

Cross reference table between ESTDVS records and element and design variable identification numbers

SETMC

Modal contribution set definitions

TEXTSE

Directory table for external superelement

Output Data Blocks: PVGRID

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to elements or grids specified on the following Case Control commands: •

DISPLACEMENT

•

VELOCITY

•

ACCELERATION

•

FORCE

•

STRESS

•

STRAIN

•

SPCFORCE

•

MPCFORCE

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•

MPRES

•

GPFORCE

•

ESE

•

EKE

•

EDE

•

GPKE

•

MODCON

•

PANCON

PVSPC

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to elements or grids specified on the SPCFORCE Case Control command

PVMPC

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to elements or grids specified on the MPCFORCE Case Control command

PVLOAD

Partitioning vector with ones at rows corresponding to degrees-of-freedom at which static and dynamic loads are applied.

PVCODES

Modal contributions output request codes corresponding to selections contained in PVGRID (MCFLAG=0 or 1). For MCFLAG=2, this is a 3-column matrix wherein column 1 is a list of output request codes, column 2 is a list of element IDs, and column 3 is a list of element item codes.

TEXTOU

Modified directory table for external superelement. Created only when TEXTSE exists, MCFLAG=2, and IRTYPE=9, 10, or 11.

Parameters: SDRMETH

NOSE

Output-integer-no default. Data recovery method flag: -1

Sparse data recovery

0

Full (or standard) data recovery

1

No data recovery is requested or required.

Input-integer-default=0. Set to -1 if there are no superelements; 0 otherwise. Superelement presence flag.

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SDROVR

Input-character-default=‘AUTO’. Override for data recovery method flag, SDR: AUTO

Choose full or sparse data recovery based on SDRDENS.

FULL

Choose full data recovery.

SPARSE

Choose sparse data recovery.

SDRDENS

Input-integer-default=0. Sparse data recovery ceiling density. If the density of PVGRID is greater than SDRDENS divided by 100, choose full data recovery.

MCSET

Input-integer-default=0. Modal contribution set to use.

MCFLAG

IRTYPE

-1

Use all sets in SETMC

0

Ignore SETMC

>0

Use set=MCSET in SETMC

Input-integer-default=0. Modal contribution set usage flag. 0

grids and elements

1

grids only

2

elements only

3

acoustic/fluid points only

Input-integer-default=0. Response type. 9

element stress

10

element strain

11

element force

MATTYP

Input-integer-default=0. External superelement matrix type.

APP

Input-character-default=‘ ’. Analysis type.

Remarks: 1. PVCODES is only created for MCFLAG=1 or 2. 2. If TEXTSE is present, external superelement processing is assumed. Therefore, all other input data blocks will be ignored except SETMC, and MCFLAG must be either 1 or 2. 3. If TEXTSE is present, MCFLAG=2, and IRTYPE=9, 10, or 11, TEXTOU will be created. The values of IRTYPE and MATTYP must be consistent with the type of data contained in the TEXTSE data block.

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9.260 OUTPUT2 Output a table or matrix into a FORTRAN readable file Writes a table or matrix data block(s) onto a binary or "compressed ASCII" (or “neutral”) file for user postprocessing or for subsequent input (via INPUTT2) into another NX Nastran run.

Format: OUTPUT2

DB1,DB2,DB3,DB4,DB5//ITAPE/IUNIT/LABL/MAXR/ NDDLNAM1/NDDLNAM2/NDDLNAM3/NDDLNAM4/NDDLNAM5/HNAME1/ HNAME2/HNAME3/HNAME4/HNAME5 $

Input Data Blocks: DBi

Any data block (table or matrix) name to be output. DBi cannot be a factor matrix (forms 4, 5, 10, 11, 13, and 15). Any or all of the input data blocks can be purged.

Parameters: ITAPE

Input-integer-default=0. ITAPE is used to select the file positioning option as follows: +n

Skip forward n data blocks before writing (used only if file has no label).

0

Data blocks are written starting at the current position. If this is the first use, no label is written.

-1

Rewind IUNIT before writing, and label file.

-3

Rewind IUNIT, print data block names and write after the last data block on IUNIT (file must have a label).

-9

Write a final EOF on IUNIT (must be used before -3 option and as last I/O use of unit), then rewind IUNIT.

IUNIT

Input-integer-no default. IUNIT is the FORTRAN unit number on which the data blocks are to be written. Siemens PLM Software does not recommend IUNIT=0. See Remark 7.

LABL

Input-character-default = ‘XXXXXXXX’ LABL is used for file identification. The label is written only if ITAPE=-1, and is checked only if ITAPE=-3.

MAXR

Input-integer-default=2 * BUFFS IZE words. Maximum physical record size. (See Remarks.)

NDDLNAMi

Input-character-default=blank. NDDL names corresponding to DB1 through DB5. If DBi is a matrix, the corresponding NDDLNAMi is ‘MATRIX’ (See Remarks.)

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HNAMEi

Input-character-default=blank. Name of the data block as it needs to appear in the output2 file.

Remarks: 1. A data block (table or matrix) consists of logical records: •

In matrices, each column is contained in one logical record. Each record begins with the row position of the first nonzero term in the column followed by the first through the last nonzero term in the column.

•

In tables, the contents of logical records vary according to the table but are described in the data block descriptions.

2. The FORTRAN binary file consists of physical records of data from the data block and KEYs that are provided to assist in the reading of the file. Each physical record of data is separated by one-word records called KEYs. The KEYs indicates one of the following depending on its location in the binary file: KEY

Description

>0

The length of the next physical record. It can also indicate the start of a new logical record.

0

End-of-File (data block) (EOF) or End-of-Data (EOD)

0

23

KEY

Data

24

1

KEY < 0 (EOR)**

25

1

KEY = 1 (Start new logical record)

26

KEY

Next Logical Record Type = 0

27

1

KEY > 0

28

KEY

Data

29

1

KEY < 0 (EOR)**

.

.

.

.

Repeat Physical Records 25-29 for Additional Records in Table

Additional Records of Table

.

.

n-7

1

KEY = 1 (Start new logical record)

Last Logical Record of Table

n-6

KEY

Next Logical Record Type = 0

n-5

1

KEY > 0

n-4

KEY

Data

n-3

1

KEY < 0 (EOR)**

DMAP Programmer’s Guide

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Description

Logical Record 4 of Table

Logical Record 5 of Table

Descriptions of DMAP Modules and Statements

Physical record number

Length

n-2

1

KEY = 1 (Start new logical record)

n-1

KEY

Next Logical Record Type = 0

n

1

KEY = 0 (EOF)

Contents

Description

If Last “Next Logical Record Type" = 0, this is the end of the table.

Note *If more data exists for the column or logical record, KEY>0 and the physical records 22, 23, and 24 are repeated as many times as necessary to complete the column or logical record. •

Format for Matrices (Records 20 though n) Physical record number

Length

Contents

20

1

KEY=1 (Start new logical record)

21

KEY

Next Logical Record Type

Description

1 : matrix column (string records)2 : factor matrix 3 : factor matrix 22

1

KEY > 0 Number of non-zero terms in next string in word unit

23

KEY+1

First non-zero row, followed by non-zero terms

24

1

KEY > 0 Number of non-zero terms in next string in word unit

25

KEY+1

First non-zero row, followed by non-zero terms.

Logical Record 4 of Matrix=first column

First Column First String Record

First Column Second String Record

Repeat String Records 22-23 for Additional Strings in Column n-2

1

KEY > 0 Number of non-zero terms in next string in word unit

n-1

KEY+1

First non-zero row, followed by non-zero terms.

n

1

KEY 0 and binary format) and repeated for each nonzero column, i=ICOL through NCOL. Word number

•

Type

Meaning

1

Integer

Column number (ICOL)

2

Integer

Row position of first nonzero term (IROW)

3

Integer

Number of words in the column (NW). See Remark 3.

4 through (NW+3)

Real or Complex

Column element values, single or double precision

Records 2, 3, 4, and so on for nonsparse and ASCII format, (IUNIT > 0), are repeated for each nonzero column, ICOL through NCOL. Records 3, 4, and so on, are also repeated for each group of r values (see DIGITS parameter). Record number 2

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DMAP Programmer’s Guide

Word number

Type

Meaning

1

Integer

Column number (ICOL)

2

Integer

Row position of first nonzero term (IROW)

3

Integer

Number of words in the column (NW). See Remark 3.

Descriptions of DMAP Modules and Statements

Record number

Word number

3, 4, and so on

•

1 through NW

Type

Meaning

Real or Complex

Column element values, single or double precision

Records 2, 3, 4, and so on for sparse, binary, and string header format (IUNIT < 0, and BIGMAT = FALSE). Word number

Type

Meaning

1

Integer

Column number (ICOL)

2

Integer

Zero

3

Integer

Number of words in the column (NW). See Remark 3.

4 through (NW+3)

Integer

String header (IS)*

Real or Complex

A string of nonzero values, single or double precision

*IS = IROW + 65536(L + 1) where IROW is the row position of the first term in the string and L is the length of the string, see Remark 3. For example, a string of six words beginning in row 4 has IS=458756. L and IROW can be derived from IS by:

•

Records 2, 3, 4, and so on for sparse, binary, and regular string format (IUNIT < 0, and BIGMAT = TRUE). Word number

Type

Meaning

1

Integer

Column number (ICOL)

2

Integer

Zero

3

Integer

Number of words in the column (NW). See Remark 3.

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Type

Word number 4 through (NW+3)

•

2

Length of string, L, plus 1. See Remark 3.

Integer

Row position of first term in string (IROW)

Real or complex

A string of nonzero values, single or double precision

Repeated for each string.

Word number

Type

Meaning

1

Integer

Column number (ICOL)

2

Integer

Zero

3

Integer

Number of words in the column (NW). See Remark 3.

3

1

Integer

String header (IS)*

4

1 through NW

Real or Complex

A string of nonzero values, single or double precision

Records 2, 3, 4, and so on for sparse, ASCII, and regular string format (IUNIT < 0, and BIGMAT = TRUE) are repeated for each nonzero column. Records 3 and 4 are repeated for each string. Record 4 is also repeated for each group of r values (see DIGITS parameter). Record number 2

3

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Integer

Records 2, 3, 4, and so on for sparse, ASCII, and string header format (IUNIT < 0, and BIGMAT = FALSE) are repeated for each nonzero column. Records 3 and 4 are repeated for each string. Record 4 is also repeated for each group of r values (see DIGITS parameter). Record number

•

Meaning

Word number

Type

Meaning

1

Integer

Column number (ICOL)

2

Integer

Zero

3

Integer

Number of words in the column (NW). See Remark 3.

1

Integer

Length of string, L, plus 1. See Remark 3.

2

Integer

Row position of first term in string (IROW)

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

Record number 4

Word number 1 through NW

Type

Meaning

Real or Complex

A string of nonzero values, single or double precision

2. A record with the last column number plus +1 and at least one value in the next record is written on IUNIT. 3. The number of words in the column, NW (or string, L), is the number of elements in the column (or string) times the number of words per type. Number of words per type is given in the table below. For example, a column with seven real double precision elements is 14 words long. Type

Number of words

1 – Real single precision

1

2 – Real double precision

2

3 – Complex single precision

2

4 – Complex double precision

4

4. Siemens PLM Software recommends the ASSIGN FMS statement for assigning the FORTRAN unit (see “Making File Assignments” in the NX Nastran Installation and Operations Guide). Selection of a proper value for IUNlT is machine dependent. 5. If the nonsparse format (IUNIT > 0) is selected, zero terms are explicitly present after the first nonzero term in any column until the last nonzero term. 6. Null columns are not output. 7. An entire column must fit in memory. 8. The FORTRAN binary file option (FORM = UNFORMATTED on the ASSIGN FMS statement) is the preferred method when the file is to be used on the same computer. The ASCII format FORM = FORMATTED on the ASSIGN FMS statement allows use of the file on another computer type. 9. The output format of these files can be read by the INPUTT4 module. 10. OUTPUT4 files can be read using a utility FORTRAN subroutine called GETIDS, which is provided in the utility directory. (See “Building and Using MATTST ” in the NX Nastran Installation and Operations Guide.) GETIDS is in the file called mattst.f or mattst.for. The program must be modified if the ASCII format is desired. The program is designed to read matrices less than 65536 rows (BIGMAT = FALSE). 11. Sparse factor matrices (forms 4, 5, 10, 11, 13, and 15) cannot be processed by OUTPUT4.

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12. If you select any of the options for endianness using the ASSIGN FMS statement, the resulting files are fortran readable only on systems having the same endianness. The only way to read these files on the same machines is to use the INPUTT4 command.

9.262 PARAM Performs specified operations on integer DMAP parameters.

Format: PARAM

//OP/S,N,OUT/IN1/IN2 $

Parameters: OP

Input-character-no default. An operation code from the following tables.

OUT

Output-integer-default = 1. The parameter name.

IN1

Input-integer-default = 1. The first input value used to compute OUT according to the tables in Remark 2.

IN2

Input-integer-default = 1. The second input value used to compute OUT according to the tables in Remark 2.

Remarks: 1. Since the release of MSC Nastran Version 66, all of the options of this module have equivalent formats, as noted below, that use the assignment statement, functions, expressions, and operators. Many of these are analogous to FORTRAN statements. See the “Direct Matrix Abstraction” chapter of the DMAP Programmer’s Guide for additional information. 2. The following tables give OUT as a function of inputs OP, IN1, and IN2. Arithmetic Operations ADD

SUB

MPY

DIV

NOT

OUT

IN1+IN2

IN1–IN2

IN1*IN2

IN1/IN2

-IN1(1)

Equivalent DMAP Assignment Statement

OUT= IN1+IN2

OUT= IN1–IN2

OUT= IN1*IN2

OUT= IN1/IN2

OUT=-IN1

OP

(1) If IN1=0, then OUT=-1

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Logical Operations OP

AND

IMPL

OR

OUT

-1

+1

+1

+1

-1

-1

-1

+1

-1

+1

-1

-1

IN1

=0 ) THEN $ IF ( RSPRINT>=0 ) OFP OXRESP//S,N,CARDNO $ XYTRAN XYCDBDR,OXRESP,,,,/XYPLTSS/‘RSPEC‘/‘PSET‘/ S,N,PFILE/S,N,CARDNO/S,N,NOXYPLT/TABID $ IF ( NOXYPLT>=0 ) XYPLOT XYPLTSS// $ ENDIF $ RECORD>=0 ENDDO $ RECORD-1

9.287 SCALAR Matrix element extractor Extracts a specified element from a matrix for use as a parameter.

Format: SCALAR

A//S,N,NROW/S,N,NCOL/S,N,VALUED $

Input Data Block: A

Any matrix (real or complex)

Output Data Blocks: None.

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Parameters: NROW

Input/output-integer-default=1. Row number of element to be extracted from [A]. See Remark 4.

NCOL

Input/output-integer-default=1. Column number of element. See Remark 4.

VALUED

Output-complex double precision-default=(0.D0,0.D0). Contents of element at NROW-th row and NCOL-th column in matrix [A].

Remarks: 1. If the input is purged, the module returns with a VALUE = (0.,0.). 2. See also the PARAML A//’DMI’ option. 3. Prior to Version 2001, VALUED was a single precision parameter. To convert an old DMAP that uses the SCALAR module for Version 2001, see Example 2. 4. If NROW (or NCOL) is greater than the number of rows (or columns) in A, NROW or (NCOL) is reset to -1 and CDVALUE remains unchanged from its value prior to calling SCALAR.

Examples: 1. Extract the matrix element in row 1 and column 2 of matrix A and assign it to the parameter VALUE. SCALAR

A//1/2/S,N,VALUE $

2. Convert a pre-Version 2001 SCALAR module call to Version 2001. SCALAR A//1/2/S,N,CDVALUE $ $ Add following statements TYPE PARM,,CS,N,CSVALUE $ CSVALUE = SINGL(CDVALUE) $

3. Read the values from a matrix V of unknown length into a parameter. TYPE PARM,,I,N,II $ LOOP COUNTER TYPE PARM,,I,N,VI=1 $ SELECTS COLUMN TO SEARCH DO WHILE (II>=0) $ STOP WHEN II NEGATIVE II = II + 1 $ SCALAR V//1/S,N,II/S,N,VI $ II RESET TO -II WHEN AT END OF MATRIX. IF (II>0) MESSAGE //‘INDEX‘/II/‘VALUE‘/VI $ ENDDO $

9.288 SDP Calculates nondimensional stability and control derivatives Calculates and prints the nondimensional stability and control derivatives and the intercepts of the quasi-steady stability derivatives.

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Format: SDP

CASEA,AECTRL,AERO,CSTMA,EDT, AEDBUXV,AEMONPT,MONITOR,MPARV,MPAERV,MPAEUV, MPSRV,MPSERV,MPSIERV,MPSEUV,MPSIEUV,UXTRIM,AEDBINDX, PRBDOFS/ STBDER,UXDIFV/ MACH/Q/AECONFIG/SYMXY/SYMXZ/LPRINT $

Input Data Blocks: CASEA

A single record (subcase) of CASECC for aerodynamic analysis

AECTRL

Table of aerodynamic model‘s control definition

AERO

Table of control information for aerodynamic analysis

CSTMA

Table of aerodynamic coordinate system transformation matrices for g-set + ks-set grid points

EDT

Element deformation table. Contains aerodynamic model records.

AEDBUXV

Matrix of vehicle states

AEMONPT

Aerodynamic monitor points

MONITOR

Structural monitor points

MPARV

Rigid monitor point loads on aerodynamic model

MPAERV

Elastic restrained monitor point loads on aerodynamic model

MPAEUV

Elastic unrestrained monitor point loads on aerodynamic model

MPSRV

Rigid splined monitor point loads on structural model

MPSERV

Elastic restrained monitor point loads on structural model

MPSIRV

Inertial restrained monitor point loads on structural model

MPSEUV

Elastic unrestrained monitor point loads on structural model

MPSIUV

Inertial unrestrained monitor point loads on structural model

UXTRIM

UX vector at trim

AEDBINDX

Aeroelastic database index for monitor point data

PRBDOFS

Partitioning matrix to partition the "active" URDDI from the "inactive". Active URRDI are assigned a 1.0 value and are connected to the SUPORT degrees-of-freedom.

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Output Data Block: STBDER

Table of aerostatic stability derivatives for a single subcase

UXDIFV

Derivative interpolation factors matrix at UX = UXREF

Parameters: MACH

Input-real-default=no default. Mach number.

Q

Input-real-default=no default. Dynamic pressure.

AECONFIG

Input-character-no default. Aerodynamic configuration.

SYMXY

Input-integer-no default. Aerodynamic x-y symmetry flag.

SYMXZ

Input-integer-no default. Aerodynamic x-z symmetry flag.

LPRINT

Input-logical-default=TRUE. Print flag for stability derivatives.

Remarks: Each stability derivative has four forms based on: •

The aerodynamic model without any consideration of the structural model

•

The aerodynamics after they have been transferred to the structure but before any elastic effects are computed

•

The aerodynamics after they have been transferred to the structure and elastic deformations have been included. It is assumed that the model is restrained at the support points for this derivative.

•

The aerodynamics after they have been transferred to the structure and elastic deformations have been included. Movement of the supported degrees of freedom is included in this derivative.

9.289 SDR1 Computes solution and single-point forces Computes and appends the solution (displacements, velocities, acceleration) and single-point forces of constraint at the g-set for each boundary condition. Also appends applied loads.

Format: SDR1

9-536

USET,PG,UL,UOO,YS,GOA,GM,PS,KFS,KSS,QR,RGPV,KOA/ UG,PGT,QG/ NSKIP/APP/NOQG $

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

Input Data Blocks: USET

Degree-of-freedom set membership table for g-set

PG

Static load matrix applied to the g-set

UL

Displacement matrix in l-set

UOO

Displacement matrix in o-set due to applied loads on the o-set with the a-set fixed (set to zero)

YS

Matrix of enforced displacements or temperatures

GOA

Omitted degree-of-freedom transformation matrix, o-set by a-set

GM

Multipoint constraint transformation matrix, m-set by n-set

PS

Static load matrix partitioned to the s-set

KFS

Stiffness matrix partition (f-set by s-set) from KNN

KSS

Stiffness matrix partition (s-set by s-set) from KNN

QR

Matrix of determinate support forces

RGPV

Sparse data recovery partitioning vector

KOA

o-set and a-set matrix partition of stiffness matrix

Output Data Blocks: UG

Displacement matrix in the g-set appended for all boundary conditions

PGT

Static load matrix applied to the g-set appended for all boundary conditions

QG

Single-point constraint forces of constraint matrix in the g-set appended for all boundary conditions

Parameters: NSKIP

Input-integer-no default. The first subcase of the current boundary condition.

APP

Input-character-no default. Analysis type. Allowable values: ‘STATICS’

Statics

‘REIG’

Normal modes

‘FREQRESP’

Frequency response

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‘TRANRESP’

Transient response

‘CEIGEN’

Complex eigenvalues

‘MMREIG’

Normal modes for matrix method

‘BKL0’

Pre-buckling (statics)

‘BKL1’

Buckling

‘DYNAMIC’

Dynamics

Input-integer-default=0. Single point forces of constraint matrix creation flag. Default of 1 requests computation of the forces. Specify -1 to request no computation.

Remarks: 1. If NSKIP is greater than 1 and the outputs are declared APPEND on the FILE statement, the outputs are appended to outputs from prior executions of SDR1. 2. PG, YS, QR, PS, and RGPV can be purged. 3. If PG is present, PGT must be present. 4. UOO must be present if the o-set exists and APP is equal to ‘STATICS’or ‘BLK0’. 5. GM must be present if the m-set exists. 6. KFS must be present if the s-set exists and QG is present. 7. KSS must be present if YS is present, the s-set exists, and QG is present. 8. UOO, KSS and YS are ignored if APP is not equal to ‘STATICS’or ‘BLK0’. 9. See the NX Nastran User‘s Guide for further discussion of the matrix operations in SDR1. 10. SDR1 can also process matrices with extra points. 11. RGPV must be present for sparse data recovery.

9.290 SDR2 Creates output tables. Creates tables based on output requests for forces of single-point and multipoint forces of constraint, applied loads, displacements, velocities, accelerations, element stresses, element strains, and element forces. These output tables are suitable for printing, plotting, and various other postprocessing.

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Format: SDR2

CASECC,CSTM,MPT,DIT,EQEXIN,SILD, ETT,{OL or EDT},BGPDT,PG,QG,UG,EST,XYCDB, OINT,PELSET,VIEWTB,GPSNT,DEQATN,DEQIND,DITID, PCOMPT,GPKE,BOLTFOR,MDLIST,COMPEST/ OPG1,OQG1,OUG1,OES1,OEF1,PUG,OGPKE1,OEFIIP,OEFIIS,OESRIP,OESRIS/ APP/S,N,NOSORT2/NOCOMP/ACOUSTIC/METRIK/ ISOFLG/GPF/ACOUT/PREFDB/TABS/ SIGMA/ADPTINDX/ADPTEXIT/BSKIP/FREQW/ BTBRS/LANGLE/OMID/SRCOMPS $

Input Data Blocks: CASECC

Table of Case Control command images.

CSTM

Table of coordinate system transformation matrices.

MPT

Table of Bulk Data entry images related to material properties.

DIT

Table of TABLEij Bulk Data entry images.

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers. See Remark 5.

EQDYN

Equivalence table between external and internal grid/scalar/extra point identification numbers. (EQEXIN appended with extra point data.)

SILD

Scalar index list for the p-set. See Remark 5.

ETT

Element temperature table.

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list.

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries.

BGPDT

Basic grid point definition table.

PG

Static load matrix applied to the g-set.

QG

Single-point (or mutipoint-QMG) constraint forces of constraint matrix in the g-set.

UG

Displacement matrix in g-set. For the DSVG1 module and transient analysis, UG can also represent velocity or acceleration.

EST

Element summary table.

XYCDB

Table of x-y plotting commands.

OINT

P-element output control table. Contains OUTPUT Bulk Data entries.

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PELSET

P-element set table, contains SETS DEFINITIONS. Output by PLTSET.

VIEWTB

View information table, contains the relationship between each p-element and its view-elements and view-grids.

GPSNT

Grid point shell normal table.

DEQATN

Table of DEQATN Bulk Data entry images.

DEQIND

Index table to DEQATN data block.

DITID

Table of identification numbers in DIT.

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry.

GPKE

Matrix of grid point kinetic energies.

BOLTFOR

Bolt force data.

MDLIST

List of modes for output selected by effective mass fraction.

COMPEST

Composite solid element summary table.

Output Data Blocks: OPG1

Table of applied loads in SORT1 format.

OQG1

Table of single or multipoint forces-of-constraint in SORT1 format.

OUG1

Table of displacements in SORT1 format.

OES1

Table of element stresses or strains in SORT1 format.

OEF1

Table of element forces in SORT1 format.

PUG

Matrix of translational displacements for plotting purposes.

OGPKE1

Table of grid point kinetic energies in SORT1 format.

OEFIIP

Data block for in-plane ply failure indices.

OEFIIS

Data block for inter-laminar shear failure indices.

OESRIP

Data block for in-plane ply strength ratios.

OESRIS

Data block for inter-laminar shear strength ratios.

Parameters: APP

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Input-character-no default. Analysis type. Allowable values:

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‘STATICS’

Statics

‘REIGEN’

Normal modes

‘FREQRESP’

Frequency response

‘TRANRESP’

Transient response

‘CEIGEN’

Complex eigenvalues

‘MMREIG’

Normal modes for matrix method

‘BKL0’

Pre-buckling (statics)

‘BKL1’

Buckling

‘NLST’

Nonlinear statics

‘GNST’

Geometric nonlinear statics

NOSORT2

Output-integer=default=0. SORT2 format flag. Set to 1 if SORT2 format is requested or XYCDB is present; -1 otherwise.

NOCOMP

Input-integer-default=-1. Composite stress/strain flag.

ACOUSTIC

METRIK

-5

Forces of composites in STRAIN=sid

-2

Forces of composites in STRESS=sid

-1

Stresses for all elements (same as 0 except in DMAP)

0

Stresses for all elements

1

Stresses for non-composites only

2

Strain/curvature and forces of composites in STRESS=sid

3

Strains for all elements and MPC forces

4

Strains for non-composites only

5

Strain/curvature of composites in STRAIN=sid

Input-integer-default=0. Fluid-structure analysis flag. If set to 2, acoustic pressure is computed for fluid elements. 0

No fluid elements exist

1

Penalty or fluid acoustic elements exists

2

Fluid/structure coupling exists

Input-integer-default=-1. Parameter for electromagnetic analysis.

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ISOFLG

Input-integer-default=-1. Parameter for electromagnetic analysis.

GPF

Input-integer-default=-1. Parameter for electromagnetic analysis.

ACOUT

Input-character-default=‘PEAK’ Type of acoustic pressure output in fluid-structural analysis. ‘RMS’

Root-mean-square

‘PEAK’

Peak

PREFDB

Input-real-default=1.0. Peak pressure reference for pressure level in units of dB or dBA.

TABS

Input-real-default=0.0. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius, or set to 459.69 when specifying temperatures in Fahrenheit.

SIGMA

Input-real-default=0.0. The Stefan-Boltzmann constant. Used to compute radiant heat flux.

ADPTINDX

Input-integer-default=-1. P-version analysis adaptivity index.

ADPTEXIT

Output-logical-default=FALSE. Set to TRUE if this is the final.

BSKIP

Input-logical-default=TRUE. Pre-buckling subcase skip flag. If TRUE, skip the first subcase in CASECC.

FREQWA

Input-real-default=0.0. Parameter for electromagnetic analysis.

BTBRS

Input-real-default=0.0. Parameter for electromagnetic analysis.

LANGLE

Input-integer-default=1. Large rotation calculation method: 1

Gimbal angle

2

Rotation vector

OMID

Input-character-default=‘NO’. Material output coordinate system flag. If OMID=‘YES’, stresses, strains, and forces are output in the material coordinate system of CQUAD4, CTRIA3, CQUAD8, and CTRIA6 elements.

SRCOMPS

Input-character-default=’NO’. Requests output of failure indices for composite solid elements. If SRCOMPS=‘YES”, requests output of strength ratios for composite solid elements.

Remarks: 1. Any output can be purged. 2. CSTM can be purged if no coordinate systems are referenced, or if stresses and/or forces are not requested. 3. MPT and EST can be purged if there are no requests for element stresses, strains, or forces.

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4. DIT can be purged if no stress or force requests are present or if no temperature dependent materials are referenced. 5. SDR2 can also process p-set matrices (UP, QP, and PP instead of UG, QG, and PG) as long as EQDYN and SILD are specified. Otherwise, SILD can be purged. 6. ETT can be purged if no thermal loading exists, or there are no requests for stresses or forces. 7. EDT can be purged if there are no element requests for forces or stresses, or if there are no enforced element deformations in the problem. 8. BGPDT can be purged if all displacement (global) coordinate systems are in the basic coordinate system and if there are no requests for element stresses, strains, or forces exist. However, PUG is not computed. 9. LAMA or CLAMA cannot be purged if an eigenvalue or frequency response problem exists. 10. EQEXIN and XYCDB can be purged.

9.291 SDR3 Converts tables in SORT1 (or SORT2) format to SORT2 (or SORT1) format

Format: SDR3

OFP1,OFP2,OFP3,OFP4,OFP5,OFP6/ OFP1X,OFP2X,OFP3X,OFP4X,OFP5X,OFP6X $

Input Data Blocks: OFPi

Output table in SORT1 (or SORT2) format

Output Data Block: OFPiX

Output table in SORT2 (or SORT1) format

Parameters: None.

Remarks: The SORT1 format created by modules like SDR2 is sorted accordingly: element type subcase ( or time step, frequency, and so on element identification number But the SORT1 format which has been reordered from SORT2 inputs by SDR3 is sorted accordingly: subcase ( or time step, frequency, and so on element type element identification number

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9.292 SDRCOMP Calculates laminar stresses Calculates laminar stresses, or strains, and failure indices in composite elements.

Format: SDRCOMP

CASECC,MPT,EPT,ETT,EST,OES1A,OEF1A,DIT,BGPDT,PCOMPT/ OES1C,OEFIT,OEF1AA,OESRT,OGPLYSS,OGPLYFI,OGPSR/ STRNFLG/DESOPT/LOADFAC/SRCOMPS $

Input Data Blocks: CASECC

Table of Case Control command images

MPT

Table of Bulk Data entry images related to material properties

EPT

Table of Bulk Data entry images related to element properties

ETT

Element temperature table

EST

Element summary table

OES1A

Table of element strain/curvatures in SORT1 format for the composite elements only

OEF1A

Table of element forces in SORT1 format for the composite elements only

DIT

Table of TABLEij Bulk Data entry images

BGPDT

Basic grid point definition table

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry

Output Data Blocks: OES1C

Table of composite element stresses or strains in SORT1 format

OEFIT

Table of composite element failure indices

OEF1AA

Table of element forces in SORT1 format for the non-composite elements only

OESRT

Table of composite element strength ratios

OGPLYSS

Table of global ply stresses/strains.

OGPLYFI

Table of global ply failure indices.

OGPSR

Table of global ply strength ratios.

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Parameters: LSTRN

Input-integer-default=0. Laminar strain flag. 0

Compute laminar stresses

1

Compute laminar strains

DESOPT

Input-integer-default=0. Non-composite element force flag. If set to 1, the non-composite element forces are extracted from OEF1A and copied to OEF1AA.

LOADFACR

Input-real-default=0.0. Load factor in nonlinear static analysis.

SRCOMPS

Input-character-default=’NO’ Flag to request output table of ply strength ratios (OESRT).

Remarks: 1. ETT can be purged. However, temperature effects are not included. 2. OEF1AA can be purged if DESOPT=0. 3. LOADFACR is required only for including its value in the header record of OES1C for nonlinear static analysis. This is necessary for proper processing by the DBC module.

9.293 SDREE Data recovery for Element Energy Scans through all of the elemental energy values and applies the user tolerance value, culling out any element data which doesn’t meet the criterion. The elements which pass the tolerance are written to the output table.

Format: SDREE

OEEI/OEEO/XFLAG

Input Data Blocks: OEEI

Input Element Energy data block

Output Data Blocks: OEEO

Output Element Energy data block containing only the elements that meet the user criteria.

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Parameters: XFLAG

Input-integer-default=0. Cull method. 0

Cull elements based on user criterion.

1

Do not cull, perform a simple copy from OEEI to OEEO.

9.294 SDRHT Combines heat flow for CHBDYi elements with heat flux of other elements

Format: SDRHT

UG,OEF1,SLT,EST,DIT,RDEST,RECM,DLT, OEFNL1,MPT,BGPDT,CSTM,SIL,USET,CASECC/ HOEF1/ TABS/SIGMA/NORADMAT $

Input Data Blocks: UG

Temperature matrix in g-set

OEF1

Table of element fluxes in SORT1 format

SLT

Table of static loads

EST

Element summary table

DIT

Table of TABLEij Bulk Data entry images

RDEST

Radiation element summary table

RECM

Radiation exchange coefficient matrix

DLT

Table of dynamic loads

OEFNL1

Table of nonlinear element fluxes in SORT1 format

MPT

Table of Bulk Data entry images related to material properties

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

SIL

Scalar index list

USET

Degree-of-freedom set membership table for g-set

CASECC

Table of Case Control command images

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Output Data Block: HOEF1

Table of element fluxes in SORT1 format updated for CHBDYi elements.

Parameters: TABS

Input-real-default=0.0. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius. or set to 459.69 when specifying temperatures in Fahrenheit.

SIGMA

Input-real-default=0.0. The Stefan-Boltzmann constant. Used to compute radiant heat flux.

NORADMAT

Input-integer-default=-1. Radiation flag. -2

No radiation

-1

Initial radiation (default)

1

Single band radiation with constant emissivity

2

Radiation with temperature dependent emissivity

3

Multiple band radiation with constant emissivity

Remarks: 1. For linear steady state heat transfer, OEF1 is also specified for OEFNL1 and RDEST, RECM, and DLT can be purged. SDRHT UG,OEF1,SLT,EST,DIT,,,, OEF1,MPTS,BGPDTS,CSTMS,SILS,USET,CASECC/ HOEF1/TABS/SIGMA/-1 $

2. In transient heat transfer UG also contains the enthalpy.

9.295 SDRNL Performs stress data recovery for nonlinear elements

Format: SDRNL

CASECC,ESTNL,ELDATA,UNUSED4,UNUSED5,UNUSED6,UNUSED7, CSTM,UGNI,BGPDT/ OESNL1,OESNLB1,UNUSED3/ NLTYPE/UNUSED2/UNUSED3/NSKIP/LINC/UNUSED6/UNUSED7/ UNUSED8 $

Input Data Blocks: CASECC

Table of Case Control command images

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ESTNL

Nonlinear element summary table

ELDATA

Table of combined nonlinear information data

UNUSED4

Unused and can be purged

UNUSED5

Unused and can be purged

UNUSED6

Unused and can be purged

UNUSED7

Unused and can be purged

CSTM

Table of coordinate system transformation matrices

UGNI

Displacement matrix at converged step in the g-set

BGPDT

Basic grid point definition table

Output Data Blocks: OESNL1

Table of nonlinear element stresses in SORT1 format

OESNLB1

Table of slideline contact element stresses in SORT1 format

UNUSED3

Unused and can be purged

Parameters: NLTYPE

Input-integer-no default. Nonlinear analysis type. 0

Statics

1

Transient response

UNUSED2

Input-integer-no default. Unused.

UNUSED3

Input-integer-no default. Unused.

NSKIP

Input-integer-no default. Subcase record number to read in CASECC.

LINC

Input-integer-no default. Number of load increments for this subcase

UNUSED6

Input-integer-default=0.0. Unused.

UNUSED7

Input-integer-default=0.0. Unused.

UNUSED8

Input-integer-default=0.0. Unused.

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9.296 SDRP Computes data for p-elements Computes displacements, element forces, element stresses, and element strains of p-elements at the view-grid points and merges with corresponding output for h-elements.

Format: SDRP

CASECC,EST ,VIEWTB,UG ,OUG1, OES1,OSTR1 ,OEF1,DEQATN,DEQIND, DIT,MPT,MPT,CSTM,ETT,OINT, PELSET,BGPDT,BGPDT,OL,GPSNT,ERROR1, RSQUERY// OUG1VU,OES1VU,OEE1VU,OEF1VU,STATDATA, RSLTSTAT,RSLTDATA,GLBTAB,GLBRSP / ADPTEXIT/ALTSHAPE/APP/SDRPOPT/PVALID/ DESCYCLE/ADPTINDX/ODESMAX/OADPMAX/SEID $

Input Data Blocks: CASECC

Table of Case Control command images

EST

Element summary table

VIEWTB

View information table. Contains the relationship between each p-element and its view-elements and view-grids.

UG

Displacement matrix in g-set. For the DSVG1 module and transient analysis, UG can also represent velocity or acceleration.

OUG1

Table of displacements in SORT1 format

OES1

Table of element stresses in SORT1 format

OSTR1

Table of element strains in SORT1 format

OEF1

Table of element forces in SORT1 format.

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

DIT

Table of TABLEij Bulk Data entry images

MPT

Table of Bulk Data entry images related to material properties

CSTM

Table of coordinate system transformation matrices

ETT

Element temperature table

OINT

p-element output control table. Contains OUTPUT Bulk Data entries.

PELSET

p-element set table. Contains SETS DEFINITIONS.

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BGPDT

Basic grid point definition table

OL

Complex or real eigenvalue summary table, transient response time output list or frequency response frequency output list

GPSNT

Grid point shell normal table

ERROR1

Error-estimate table updated for current superelement or adaptivity loop

RSQUERY

Table of results state query

Output Data Blocks: OUG1VU

Table of displacements in SORT1 format for view grids

OES1VU

Table of element stresses in SORT1 format for view elements

OSTR1VU

Table of element strains in SORT1 format for view elements

OEF1VU

Table of element forces in SORT1 format for view elements

STATDATA

Table of state information when system cell 297=1

RSTLSTAT

Table of result-state information when system cell 297=2

RSLTDATA

Table of actual results data when system cell 297=3

GLBTAB

Table of global responses when system cell 297=-1

GLBRSP

Matrix of global responses when system cell 297=-1

Parameters: ADPTEXIT

Input-logical-no default. Set to TRUE if this is the final adaptivity loop.

ALTSHAPE

Input-integer-default=0. Specifies set of displacement functions in p-element analysis. ALTSHAPE=0 selects the MacNeal set and 1 selects the Full Product Space set.

APP

Input-character-no default. Analysis type. Allowable values:

SDRPOPT

9-550

‘STATICS’

Statics

‘REIGEN’

Normal modes

‘FREQ’

Frequency response

‘TRANSNT’

Transient response

‘CEIGEN’

Complex eigenvalues

Input-character-no default. Principal stress/strain computation selection:

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‘SDRP’

Compute in SDRP

‘OFP’

Compute in OFP

PVALID

Input-integer-no default. p-value set identification number.

DESCYCLE

Input-integer-no default. Design cycle analysis counter.

ADPTINDX

Input-integer-no default. p-version analysis adaptivity index.

ODESMAX

Input-integer-no default. Total number of design cycles performed.

OADPMAX

Input-integer-no default. Total number of adaptivity cycles performed.

SEID

Input-integer-no default. Superelement identification number.

Remarks: 1

If disk space is critical, SDRPOPT can set to ‘OFP’to delay computation of principal stresses and strains to the OFP module.

2

The scope of SDRP processing depends on the value system cell 297: 0

Traditional NASTRAN data recovery

1,2,3 On-the-fly data recovery -1

Global Response (that is, find the minimum/maximum values of certain data recovery quantities)

9.297 SDRX Modifies CBAR, CBEAM and CBEND element results Modifies CBAR, CBEAM and CBEND element forces, stresses, and strains due to CBARAO and PLOAD1 Bulk Data entries. Also computes intermediate station output. Applicable to static and normal modes analysis only.

Format: SDRX

CASECC,OEF1,OES1,GEOM2,GEOM3,EST,CSTM,MPT,DIT,BGPDT, OSTR1/ OEF1X,OES1X,OSTR1X/ S,N,NOXOUT/ICAM $

Input Data Blocks: CASECC

Table of Case Control command images

OEF1

Table of element forces in SORT1 format

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OES1

Table of element stresses in SORT1 format

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM3

Table of Bulk Data entry images related to static and thermal loads

EST

Element summary table

CSTM

Table of coordinate system transformation matrices

MPT

Table of Bulk Data entry images related to material properties

DIT

Table of TABLEij Bulk Data entry images

BGPDT

Basic grid point definition table

OSTR1

Table of element strains in SORT1 format

Output Data Blocks: OEF1X

Table of displacements in SORT1 format for view grids

OES1X

Table of element stresses in SORT1 format updated for PLOAD1 loads and intermediate station output

OSTR1X

Table of element strains in SORT1 format augmented with strains for 1-D elements

Parameter: NOXOUT

ICAM

Output-integer-no default. SDRX update flag. 0

OEF1X, OES1X, and OSTR1X are updated

-1

OEF1X, OES1X, and OSTR1X are not updated Input-Integer-Default=0 When set to 1, process all constraint and attachment modes

Example: Excerpt from subDMAP SEDRCVR: SDRX CASEDR,OEF1,OES1,GEOM2S,GEOM3S,EST,CSTMS,MPTS,DIT,BGPDTS,OSTR1/ OEF1X,OES1X,OSTR1X/S,N,NOXOUT $ EQUIVX OEF1/OEF1X/NOXOUT $ EQUIVX OES1/OES1X/NOXOUT $ EQUIVX OSTR1/OSTR1X/NOXOUT $

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9.298 SDRXD Modifies CBAR, CBEAM and CBEND element results Modifies CBAR, CBEAM and CBEND element forces, stresses, and strains due to CBARAO and PLOAD1 Bulk Data entries. Also computes intermediate station output. Applies to transient and frequency response analysis only.

Format: SDRXD

CASECC,OEF1,OES1,GEOM2,GEOM3,EST,CSTM,MPT,DIT, UG,DLT,OL,BGPDT,OSTR1/ OEF1X,OES1X,OSTR1X/ S,N,NOXOUT/APP/COUPMASS $

Input Data Blocks: CASECC

Table of Case Control command images

OEF1

Table of element forces in SORT1 format

OES1

Table of element stresses in SORT1 format

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM3

Table of Bulk Data entry images related to static and thermal loads

EST

Element summary table

CSTM

Table of coordinate system transformation matrices

MPT

Table of Bulk Data entry images related to material properties

DIT

Table of TABLEij Bulk Data entry images

UG

Displacement matrix in g-set

DLT

Table of dynamic loads

OL

Transient response time output list or frequency response frequency output list

BGPDT

Basic grid point definition table

OSTR1

Table of element strains in SORT1 format

Output Data Blocks: OEF1X

Table of displacements in SORT1 format for view grids

OES1X

Table of element stresses in SORT1 format updated for PLOAD1 loads and intermediate station output

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OSTR1X

Table of element strains in SORT1 format augmented with strains for 1-D elements

Parameters: NOXOUT

Output-integer-no default. SDRX update flag.

APP

0

OEF1X, OES1X, and OSTR1X are updated

-1

OEF1X, OES1X, and OSTR1X are not updated

Input-character-no default. Analysis type. Allowable values:

COUPMASS

‘FREQRESP’

Frequency response

‘TRANRESP’

Transient response

Input-integer-default=-1. Coupled mass generation flag. -1

Lumped

0

Coupled

Example: SDRX CASEDR,OEF1,OES1,GEOM2S,GEOM3S,EST,CSTMS,MPTS, DIT,BGPDTS,OSTR1/ OEF1X,OES1X,OSTR1X/S,N,NOXOUT $ EQUIVX OEF1/OEF1X/NOXOUT $ EQUIVX OES1/OES1X/NOXOUT $ EQUIVX OSTR1/OSTR1X/NOXOUT $

9.299 SDSA Partitions design model to superelements Partitions the design model (that is, the design optimization Bulk Data entries) to superelements.

Format: SDSA

EDOM,EPTS,EQEXINS,SEMAP,MPTS/ EDOMS/ SEID/PEID/S,N,OBJSID/DESOBJ/S,N,DESVAR/ S,N,DRESP/S,N,TWGTFL/S,N,TVOLFL $

Input Data Blocks: EDOM

Table of Bulk Data entries related to design sensitivity and optimization

EPTS

Table of Bulk Data entry images related to element properties for the superelement specified by SEID

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EQEXINS

Equivalence table between external and internal grid/scalar identification numbers for the superelement specified by SEID

SEMAP

Superelement map table

MPTS

Table of Bulk Data entry images related to material properties for the current superelement

Output Data Block: EDOMS

Table of Bulk Data entries related to design sensitivity and optimization for the superelement specified by SEID

Parameters: SEID

Input-integer-default=0. Superelement identification number.

PEID

Input-integer-default=0. Primary superelement identification number.

OBJSID

Output-integer-default=-1. Superelement identification number associated with DESOBJ. Set to -1 for all cases unless you specify the DESOBJ command in a particular superelement subcase.

DESOBJ

Input-integer-default=0. DESOBJ Case Control command set identification number.

DESVAR

Output-integer-default=0. Retained DVPRELi or DVGRID entry flag for superelement SEID. Set to -1 if there are retained design variable perturbations.

DRESP

Output-integer-default=0. Retained DRESP1 entry flag for superelement SEID. Set to -1 if there are retained design responses.

TWGTFL

Output-integer-default=0. Total weight flag.

TVOLFL

Output-integer-default=0. Total volume flag.

Remarks: SDSA is intended to be executed in a superelement DMAP loop driven by SEP2DR. See subDMAP DESINIT for an example.

9.300 SDSB Generates superelement processing list Generates the superelement processing list to direct the pseudo-load and response sensitivity calculations.

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Format: SDSB

SLIST,EDOM*,CASECC,UNUSED4,UNUSED5/ DSLIST/ S,N,DMRESD/S,N,NOSEDV/S,N,NOSERESP $

Input Data Blocks: CASECC

Table of Case Control command images

SLIST

Superelement processing list to matrix generation, assembly, and reduction

EDOM*

Family of EDOM tables for all superelements

unused4

Unused and can be purged

unused5

Unused and can be purged

Output Data Block: DSLIST

Superelement processing list to direct the pseudo-load and response sensitivity calculations

Parameters: DMRESD

Output-integer-default=-1. Design model flag. If set to -1, the design model is limited to the residual structure.

NOSEDV

Output-integer-default=0. Pseudo-load generation flag based on the SEDV Case Control command. Set to -1 if pseudo-loads are not requested for any superelement.

NOSERESP

Output-integer-default=0. Response sensitivity calculation flag based on the SERESP Case Control command. Set to -1 if response sensitivities are not requested for any superelement.

Example: Excerpt from subDMAP DESINIT: DBVIEW EDOMF=EDOMS WHERE (wildcard) $ IF ( NOT(RSONLY) AND NOEDOM>0 ) SDSB SLIST,EDOMF,CASEXX,,/DSLIST/S,N,DMRESD/ S,N,NOSEDV/S,N,NOSERESP $

9.301 SDSC Prints correlation table for normalized design sensitivity coefficient matrix

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Format: SDSC

DSCMCOL// OBJSID/DESOBJ/UNUSED3/EIGNFREQ $

Input Data Block: DSCMCOL

Correlation table for normalized design sensitivity coefficient matrix

Output Data Blocks: None.

Parameters: OBJSID

Input-integer-default=0. Superelement identification number associated with DESOBJ. Set to -1 for all cases unless you specify the DESOBJ command in a particular superelement subcase.

DESOBJ

Input-integer-default=0. DESOBJ Case Control command set identification number.

UNUSED3

Input-integer-default=1. Unused.

EIGNFREQ

Input-integer-default=0. Eigenvalue/frequency response type flag. 1

Eigenvalue (radian/time)

2

Frequency (cycle/time)

9.302 SECONVRT Modifies Bulk Data entry records Modifies those Bulk Data entry records which define coordinate systems, orientation vectors, and load vectors by grid point identification number; for example, CORD1j to CORD2j, FORCEi to FORCE, MOMENTi to MOMENT, replace GO on CBAR, CBEAM, CBEND, CBUSH and CGAP with X1, X2, X3.

Format: SECONVRT

BGPDT,GEOM1,GEOM2,GEOM3/ GEOM1N,GEOM2N,GEOM3N $

Input Data Blocks: BGPDT

Basic grid point definition table

GEOM1

Table of Bulk Data entry images related to geometry

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GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM3

Table of Bulk Data entry images related to static and thermal loads

Output Data Blocks: GEOM1N

Modified GEOM1 with CORD1j records converted to CORD2j records

GEOM2N

Modified GEOM2 with GO replaced by X1, X2, and X3 on CBAR, CBEAM, CBEND, CBUSH and CGAP records

GEOM3N

Modified GEOM3 with FORCEi and MOMENTi records converted to FORCE and MOMENT records

Parameters: None.

Remarks: System cell 350 controls execution of the SECONVRT module. -1

No converson

0

Convert and echo all converted entries in the f06

>0

Convert and echo the first n converted entries in the f06 where n is the value of system cell 350

9.303 SEDR Partitions tables for superelements Partitions the solution matrix, Case Control and Plot Control tables for each superelement.

Format: SEDR

SEMAP,CASECC,PCDB,DRLIST,XYCDB,SLT,ETT, MAPS*,UGD,BGPDTD,GDNTAB/ UA,CASEDR,PCDBDR,XYCDBDR/ APP/SEID/S,N,NOUP/S,N,NOSORT1/S,N,NOUG/ S,N,NOOUT/S,N,NOPLOT/S,N,NOXYPLOT/QUALNAM/NCUL $

Input Data Blocks: SEMAP

Superelement map table

CASECC

Table of Case Control command images

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PCDB

Table of model (undeformed and deformed) plotting commands

DRLIST

Superelement processing list for data recovery

XYCDB

Table of x-y plotting commands

SLT

Table of static loads

ETT

Element temperature table

MAPS*

Family of MAPS (superelement upstream to downstream boundary coordinate system, secondary (mirror, identical, and repeated), and release transformation matrix)

UGD

Displacement matrix in g-set for the downstream superelement

BGPDT

Basic grid point definition table

GDNTAB

Table of grid points generated for p-element analysis

Output Data Blocks: UA

Solution matrix on the boundary (a-set) of the superelement (identification number equal to output value of SEID)

CASEDR

Table of Case Control command images for the superelement (identification number equal to output value of SEID)

PCDBDR

Table of model (undeformed and deformed) plotting commands for the superelement (identification number equal to output value of SEID)

XYCDBDR

Table of x-y plotting commands for a superelement (identification number equal to output value of SEID)

Parameters: APP

Input-character-no default. Analysis type. Allowable values: ‘STATICS’

Statics

≠‘STATICS’

Not statics

SEID

Input-integer-default=0. Superelement identification number.

NOUP

Output-integer-default=0. Upstream superelement flag. Set to -1 if there are no superelements connected upstream from the current superelement.

NOSORT1

Output-integer-default=0. SORT1 format flag. Set to -1 if SORT1 format is not requested for current superelement.

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NOUG

Output-integer-default=0. UG presence flag. Set to -1 if UG already exists for the current superelement.

NOOUT

Output-integer-default=0. Output request flag. Set to -1 if no output requests are specified for the current superelement.

NOPLOT

Output-integer-default=0. Plot request flag. Set to -1 if no deformed plot requests are specified for the current superelement.

NOXYPLOT

Output-integer-default=0. X-Y plot request flag. Set to -1 if no x-y plot requests are specified for the current superelement.

QUALNAM

Input-character-default=‘SEID’ Name of qualifier to be used in selecting MAPS.

NCUL

Input-integer-no default. Number of columns desired in the solution matrix for the residual structure. Usually determined by the PARAML module.

9.304 SEDRDR Drives superelement data recovery loop

Format: SEDRDR

DRLIST,SEMAP// S,N,LASTSE/S,N,SEID/S,N,PEID/S,N,SEDWN/S,N,NODR/ NOSE/S,N,SETYPE/S,N,RSEID/S,N,SCNDRY/S,N,EXTRN/ SEDRCNTL/NOPGHD $

Input Data Blocks: DRLIST

Superelement processing list for data recovery

SEMAP

Superelement map table

Output Data Blocks: None.

Parameters: LASTSE

Output-integer-default=0. Last superelement flag. Set to -1 if the current superelement is the last to process.

SEID

Input/output-integer-default=0. Superelement identification number and initialization flag. On input: -1

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-2

Same as -1 except do not print UIM 7321

≥0

Previous superelement identification number

On output: ≥0

Current superelement identification number

PEID

Output-integer-default=0. Primary superelement identification number.

SEDWN

Output-integer-default=0. Downstream superelement identification number.

NODR

Output-integer-default=0. Data recovery request flag. Set to -1 if there is no data recovery requested for any superelement.

NOSE

Input-integer-default=0. Superelement presence flag. Set to -1 if there are no superelements.

SETYPE

Output-character-default=’ ’ Superelement type as specified on the SEBULK Bulk Data entry. ‘REPEAT’

Repeated

‘MIRROR’

Mirror

‘COLLTR’

Collector

‘EXTRNA’

External

‘PRIMARY’

Primary

RSEID

Output-integer-default=0. Repeated superelement identification number as specified on the SEBULK Bulk Data entry.

SCNDRY

Output-integer-default=0. Secondary (identical or mirror) superelement flag. Set to -1 if superelement is defined by the CSUPER Bulk Data entry with PEID>0.

EXTRN

Output-integer-default=0. External superelement flag. Set to -1 if superelement is defined by the CSUPER Bulk Data entry with PEID=0.

SEDRCNTL

Input-character-default=’ ’ Processing list selection.

NOPGHD

’‘

All superelements are processed (default).

‘CURR‘

Only the superelements specified by the SEID parameter are processed.

Input-integer-default=0. Page header superelement label print control. 0

Print page header and UIM 7321.

-1

Do not print page header and UIM 7321.

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-2

Same as -1 and do not print .f04 label.

-3

Same as -2 and do not print superelement label in SUBTITLE line of page header.

Remarks: SEDRDR processes each superelement, specified in DRLIST, in the order of data recovery; that is, downstream to upstream or residual structure to tip superelements.

Example: Compose a DMAP loop to process all superelements starting at the residual structure and ending with the tips. PARAML SEMAP//‘PRES‘////S,N,NOSE $ LPFLG=0 $ INITIALIZE DO WHILE ( LPFLG>=0 ) $ IF ( NOSE0 overrides SID value specified in CASES.

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9.310 SEP2CT Partitions Case Control and Plot Control tables for each superelement

Format: SLIST,CASECC,PCDB,UNUSED4,XYCDB/ CASES,PCDBS,XYCDBS/ APP/SEID $

SEP2CT

Input Data Blocks: SLIST

Superelement processing list to matrix generation, assembly, and reduction

CASECC

Table of Case Control command images

PCDB

Table of model (undeformed and deformed) plotting commands

UNUSED4

Unused and can be purged

XYCDB

Table of x-y plotting commands

Output Data Blocks: CASES

Table of Case Control command images for the current superelement (identification number equal to output value of SEID)

PCDBS

Table of model (undeformed and deformed) plotting commands for the current superelement (identification number equal to output value of SEID)

XYCDBS

Table of x-y plotting commands for the current superelement (identification number equal to output value of SEID)

Parameters: APP

SEID

Input-character-no default. Analysis type. Allowable values: ‘STATICS’

Statics

≠‘STATICS’

Not statics

Input-integer-default=0. Superelement identification number.

9.311 SEP2DR Drives superelement generation, assembly, and reduction loop Drives the superelement generation, assembly, and reduction loop. Also drives the pseudo-load generation loop.

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Format: SEP2DR

Input Data Blocks: SLIST

Superelement processing list to matrix generation, assembly, and reduction

DSLIST

Superelement processing list to direct the pseudo-load and response sensitivity calculations

SEMAP

Superelement map table

Output Data Blocks: None.

Parameters: SEID

Input/output-integer-default=0. Superelement identification number and initialization flag. On input: -1

Initialization

-2

Same as -1 except do not print UIM 7321

≥0

Previous superelement identification number

On output: ≥0

Current superelement identification number

PEID

Output-integer-default=0. Primary superelement identification number.

SEDWN

Output-integer-default=0. Downstream superelement identification number.

LASTSE

Output-integer-default=0. Last superelement flag. Set to -1 if the current superelement is the last to process.

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NOMAT

Output-integer-default=0. Matrix generation flag. Set to -1 if no matrix generation is requested for the current superelement based on the SEMG or SEALL Case Control commands.

NOASM

Output-integer-default=0. Matrix assembly flag. Set to -1 if no matrix assembly and reduction is requested for the current superelement based on the SEKR or SEALL Case Control commands.

NOLOAD

Output-integer-default=0. Load generation flag. Set to -1 if no load generation is requested for the current superelement based on the SELG or SEALL Case Control commands.

NOLASM

Output-integer-default=0. Load assembly flag. Set to -1 if no load assembly and reduction is requested for the current superelement based on the SELR or SEALL Case Control commands.

NOUP

Output-integer-default=0. Upstream superelement flag. Set to -1 if there are no superelements connected upstream from the current superelement.

SCNDRY

Output-integer-default=0. Secondary (identical or mirror) superelement flag. Set to -1 if superelement is defined by the CSUPER Bulk Data entry with PEID>0.

EXTRN

Output-integer-default=0. External superelement flag. Set to -1 if superelement is defined by the CSUPER Bulk Data entry with PEID=0.

NOMR

Output-integer-default=0. Mass and damping assembly flag. Set to -1 if no mass and damping assembly and reduction is requested for the current superelement based on the SEMR or SEALL Case Control commands.

SEP2CNTL

Input-character-default=‘SLIST’ Processing list selection.

NOPSLG

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‘ALL’

All superelements are processed.

‘PSLGDV’

Only superelements specified on the SEDV Case Control commands

‘DSLIST’

Only superelements specified on the SERESP Case Control commands

‘SLIST’

Only superelements specified on the SEALL, SEMG, SEKR, SELG, SELR, or SEMR Case Control commands

‘SEDWN’

All superelements that have SEDWN as their downstream superelement

‘CURR’

Only the superelement specified by SEID parameter is processed

Output-integer-default=0. Pseudo-load generation flag. Set to -1 if no load generation is requested for the current superelement based on the SEDV or SERESP Case Control commands.

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NOPGHD

Input-integer-default=0. Page header and eject flag. 0

Print page header in f06 and label in f04.

-1

Do not print page header in f06.

-2

Do not print page header in f06 and label in f04

PARTSE

Output-logical-default=FALSE. Partitioned superelement flag. Set to TRUE if the current superelement is a partitioned superelement.

SETYPE

Output-character-default=’ ’ Superelement type as specified on the SEBULK Bulk Data entry. ‘REPEAT’

Repeated

‘MIRROR’

Mirror

‘COLLTR’

Collector

‘EXTRNA’

External

‘PRIMARY’

Primary

RSEID

Output-integer-default=0. Repeated superelement identification number as specified on the SEBULK Bulk Data entry.

NSENQSET

Output-integer-default=0. Number of SENQSET degrees-of-freedom allocated to the current superelement.

Remarks: 1. SEP2DR processes each superelement, specified in SLIST or DSLIST, in the order of matrix generation; that is, upstream to downstream or tip superelements to the residual structure. 2. If SEP2CNTL=‘PSLGDV’or ‘DSLIST‘, DSLIST must be specified as the first input; otherwise, ‘SLIST’is specified.

Example: Compose a DMAP loop to process all superelements starting at the tips and ending with the residual structure. PARAML SEMAP//‘PRES‘////S,N,NOSE $ LPFLG=0 $ INITIALIZE DO WHILE ( LPFLG-1 ) $ IF ( NOSE0 overrides SID value specified in CASES.

9.313 SEP3 Examines Case Control and determines superelement processing Examines Case Control and determines which superelements are to be processed for generation, assembly, and reduction of stiffness, mass, and damping, and load matrices.

Format: SEP3

CASECC,EMAP/ SLIST/ S,N,NOSECOM/S,N,SEID/NOSE/S,N,NOMAT/S,N,NOASM/ S,N,NOLOAD/S,N,NOLASM/S,N,NOMR/UNUSED9 $

Input Data Blocks: CASECC

Table of Case Control command images

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Superelement map table

Output Data Block: SLIST

Superelement processing list for matrix generation, assembly, and reduction

Parameters: NOSECOM

Output-integer-default=0. Superelement Case Control command flag. Set to -1 if there are no SEALL, SEMG, SEKR, SELG, SELR, or SEMR commands specified in CASECC.

SEID

Output-integer-default=0. Initialization flag. If there are superelements, SEID is set to -1 to initialize SEP2DR; otherwise 0.

NOSE

Input-integer=default=0. Superelement presence flag. Set to -1 if there are no superelements.

NOMAT

Output-integer-default=0. Matrix generation flag. If there are no superelements, NOMAT is set to -1 if no SEMG and no SEALL Case Control commands are specified.

NOASM

Output-integer-default=0. Matrix assembly flag. If there are no superelements, NOASM is set to -1 if no SEKR and no SEALL Case Control commands are specified.

NOLOAD

Output-integer-default=0. Load generation flag. If there are no superelements, NOLOAD is set to -1 if no SELG and no SEALL Case Control commands are specified.

NOLASM

Output-integer-default=0. Load assembly flag. If there are no superelements, NOLASM is set to -1 if no SELR and no SEALL Case Control commands are specified.

NOMR

Output-integer-default=0. Mass and damping assembly flag. If there are no superelements, NOMR is set to -1 if no SEMR and no SEALL Case Control commands are specified.

UNUSED9

Input-integer-default=0. Unused.

Remarks: If there are no superelements, SLIST is not created and can be purged.

9.314 SEP4 Examines table and data base information for superelement processing Examines the Case Control and Plot Control tables, queries the data base for existing solution matrices, and determines which superelements are to be processed for data recovery.

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Format: SEP4

CASECC,PCDB,EMAP,XYCDB,UG*,PUG*,QG*/ DRLIST/ UNUSED1/QUALNAM/S,N,NODR/S,N,SEID/S,N,NOSEPLOT/ SEP4CNTL $

Input Data Blocks: CASECC

Table of Case Control command images

PCDB

Table of model (undeformed and deformed) plotting commands

SEMAP

Superelement map table

XYCDB

Table of x-y plotting commands

UG*

Family of displacement matrices in g-set for all superelements

PUG*

Family of matrices of translational displacements for all superelements

QG*

Family of single-point constraint forces of constraint matrices in the g-set for all superelements

Output Data Block: DRLIST

Superelement processing list for data recovery

Parameters: UNUSED1

Input-character-no default. Specify ’ ’

QUALNAM

Input-character-default=‘SEID’ Name of qualifier to be used in selecting UG, PUG, and QG.

NODR

Output-integer-default=0. Data recovery request flag. Set to -1 if there is no data recovery requested for any superelement.

SEID

Input-integer-default=0. Initialization flag. If there are superelements, SEID is set to -1 to initialize SEDRDR; otherwise 0.

NOSEPLOT

Output-integer-default=0. SEPLOT or SEUPPLOT request flag. Set to -1 if there are no SEPLOT or SEUPPLOT commands specified in the OUTPUT(PLOT) section.

SEP4CNTL

Output-integer-default=’ ’ Processing list selection. ‘ALL’

All superelements are processed.

≠‘ALL’

Only superelements specified on the SEDR Case Control command

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Example: DBVIEW UGF =UG WHERE (WILDCARD) $ DBVIEW PUGF=PUG WHERE (WILDCARD) $ DBVIEW QGF =QG WHERE (WILDCARD) $ SEP4 CASECC,PCDB,EMAP,XYCDB,UGF,PUGF,QGF/ DRLIST/ ’‘//S,N,NODRALL/S,N,SEID/S,N,NOUPL $

9.315 SEPDIS Contact solution separation distance output creation.

Format: SEPDIS

CNELM,ECDISP,CASECC/OSPDS/S,N,NVEC $

Input Data Blocks: CNELM

Contact element definition table.

ECDISP

Contact element displacements.

CASECC

Table of case control command images.

Output Data Blocks: OSPDS

Table of initial or final separation distances at the contact grids.

Parameters: NVEC

Input-Integer. Number of solution results to process.

9.316 SEPLOT Assembles plot displacement matrices for superelements Assembles plot displacement matrices for superelements based on the SEPLOT and SEUPPLOT commands.

Format: SEPLOT

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PCDB,SEMAP,SCSTM,BGPDT*,ECT*,PUG*/ BGPDTX,PUGX,PLSETMSG,PLTPAR,GPSETS,ELSET/ QUALNAM/QUALNAMP/S,N,PLTCNT/S,N,NGP/S,N,JPLOT $

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

Input Data Blocks: PCDB

Table of model (undeformed and deformed) plotting commands

SEMAP

Superelement map table

SCSTM

Table of global transformation matrices for partitioned superelements

BGPDT*

Family of basic grid point definition tables for all superelements

ECT*

Family of element connectivity tables for all superelements

PUG*

Family of matrices of translational displacements for all superelements

Output Data Blocks: BGPDTX

BGPDT assembled for superelements defined on the SEPLOT or SEUPPLOT command

PUGX

PUG assembled for superelements defined on the SEPLOT or SEUPPLOT command

PLSETMSG

Table of user informational messages generated during the definition of element plot sets

PLTPAR

Table of plot parameters and plot control

GPSETS

Table of grid point sets related to the element plot sets

ELSET

Table of element plot set connections

Parameters: QUALNAM

Input-character-default=‘SEID’ Name of qualifier to be used in selecting BGPDT and ECT.

QUALNAMP

Input-character-default=‘PEID’ Name of qualifier to be used in selecting PUG.

PLTCNT

Input/output-integer-no default. SEPLOT (or SEUPPLOT) command counter. On input: 0

Initialization

On output: ≥0 NGP

Current SEPLOT (or SEUPPLOT) command

Output-integer-no default. Number of grid points and scalar points in the BGPDTX.

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Output-integer-no default. Number of element plot sets. Set to -1 if there are none.

Example: Excerpt from subDMAP SUPER3: DBVIEW BGPDTF=BGPDTS WHERE (PEID=* AND MODLTYPE=‘STRUCTUR‘) $ DBVIEW ECTF=ECTS WHERE (PEID=* AND MODLTYPE=‘STRUCTUR‘) $ DO WHILE ( PLTCNT>-1 ) $ SEPLOT PCDB,EMAP,scstm,BGPDTF,ECTF,PUGF/ BGPDTX,PUGX,PLTXY,PLTPARY,GPSETSY,ELTSETSY/ ‘PEID‘/‘SEID‘/S,N,PLTCNT/S,N,NSILS/S,N,JPLOT $ PRTMSG PLTXY//PDRMSG $ IF ( JPLOT>=0 ) THEN $ PLOT PLTPARY,GPSETSY,ELTSETSY,CASECC,BGPDTX, PUGX,PUGX,gpect,oes1x/ PLOTY2/NSILS/0/JPLOT/-1/S,N,PFILE $ PRTMSG PLOTY2//PDRMSG $ ENDIF $ JPLOT>=0 ENDDO $ PLTCNT>-1

9.317 SEPR1 Builds a list of partitioned superelement Bulk Data sections

Format: SEPR1

BULK*/ SELIST/ QUALNAM/S,N,SEFLAG $

Input Data Blocks: BULK*

Family of partitioned superelement Bulk Data sections

Output Data Blocks: SELIST

List of partitioned superelement identification numbers

Parameters: QUALNAM

Input-character-default=‘SEID’ Name of qualifier to be used in selecting BULK.

SEFLAG

Output-logical-default=FALSE. Set to TRUE if partitioned superelements are present.

Example: Excerpt from subDMAP IFPL:

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DBVIEW IBULKSF = IBULK WHERE (SEID>0 AND PEID=*) $ SEPR1 IBULKSF/SELIST//S,N,SELIST $

9.318 SEQP Resequencing processor Generates SEQGP entries or a mapping matrix for use in resequencing matrices for efficient matrix decomposition.

Format 1: Geometry Table input SEQP

GEOM1,GEOM2,GEOM4,EPT,MATPOOL,DYNAMIC,CASECC/ GEOM1Q,TIMSIZ,GEQMAP,BNDFIL,SPCPART,LGPART,GEOM2X, GEOM4X/ SEQOUT/SEQMETH//SUPER/FACTOR/ MPCFLG/START/MSGLVL/PEXIST/PSEQOPT/S,N,NTIPS/APP/ S,N,ZCOLLCT/S,N,TIPSCOL/ACMS/S,N,FLUIDSE $

Format 2: Matrix input SEPQ

MAT,GPL,USET,SIL/SEQMAP,,,,,/SEQOUT/METHOD/SETNAME $

Input Data Blocks: GEOM1

Table of Bulk Data entry images related to geometry

GEOM2

Table of Bulk Data entry images related to element connectivity and scalar points

GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership, and rigid element connectivity

EPT

Table of Bulk Data entry images related to element properties

MATPOOL

Table of Bulk Data entry images related to hydroelastic boundary, heat transfer radiation, virtual mass, DMIG, and DMIAX entries. Required for DMIG and virtual mass partitioning with domain solver ACMS=‘YES’

DYNAMIC

Table of Bulk Data entry images related to dynamics. Grid points on DPHASE, DELAY, TIC, and DAREA records are assigned to the residual structure if ACMS=‘YES’

CASECC

Table of Case Control command images. Required for MFLUID set identification number.

MAT

Matrix. Must be square and symmetric.

GPL

External grid/scalar point identification number list

USET

Degree-of-freedom set membership table for g-set

SIL

Scalar index list

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Output Data Block: GEOM1Q

Same as GEOM1 except SEQGP Bulk Data entry records have been added and any pre-existing SEQGP records are removed

TIMSIZ

Table of CPU and disk space estimation parameters

GEQMAP

Table of grid based local equation map indicating which grid resides on which processors/partitions for domain decomposition

BNDFIL

Table containing the local and global boundary grids in the order given by extreme for domain decomposition

SPCPART

Partitioning vector for domain decomposition

SEQMAP

Mapping matrix for resequencing

LGPART

Same as SPCPART except it includes disjoint grid points

GEOM2X

GEOM2 table augmented with fluid data and SPOINTS if ACMS=‘YES‘

GEOM4X

GEOM4 table augmented with new RBE1 and RBE2 records (because all RBE1 and RBE2 elements are split so that each one contains only one m-set grid) for ACMS=‘YES’ Also augmented with SEQSET1 records for ACMS=‘YES’

Parameters: SEQOUT

SEQMETH

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Input-integer-default=0. Output options: 0

No output

1

Print a formatted table of the internal vs. external grid identification number

2

Write the SEQGP entries to the punch file (.pch)

3

Combines 1 and 2

Input/output-integer-default=3. Resequencing method: -1

No resequencing is performed.

1

Active/passive

2

Band

3

For the active/passive and the band options, select the option giving the lowest RMS value of the active columns for each group of grid points (default).

4

Wavefront (Levy)

5

Gibbs-King. See Remark 4.

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6

Automatic nested dissection. See Remark 4.

7

Multiple Minimum Degree of Freedom. See Remarks 3 and 4.

8

Semiautomatic selection. See Remark 5.

On output, METHOD is set to -1 if new sequence results in a lower decomposition time estimate. Otherwise it is set to 0. SETNAME

Input-character-default=‘G’ Degree-of-freedom set name corresponding to the size of MAT (Format 2 only).

SUPER

Input-integer-default=0. Selects coupled or uncoupled sequencing or special handling of multipoint constraints.

FACTOR

Input-integer-default=0. Factor in the computation of the sequenced identification number (SEQID) on the SEQGP. See Remark 7.

MPCFLG

Input-integer-default=0. Controls whether the grid point connectivity created by multipoint constraint Bulk Data entries (MPC, MPCADD, and MPCAX and the rigid element entries; for example, RBAR) is considered during resequencing. -1

Do not consider

0

Consider (default)

>0

Consider only the MPC, MPCADD, and MPCAX entries with a set identification number equal to this parameter‘s value as well as the of the rigid element entries

START

Input-integer-default=0. The number of the grid points at the beginning of the input sequence. See Remark 8.

MSGLVL

Input-integer-default=0. Diagnostic output flag. 0

No

>0

Yes

PEXIST

Input-logical-default=FALSE. If set to TRUE, it specifies the existence of p-elements.

PSEQOPT

Input-character-default=’ ’ Specifies append (default) or insert option for p-elements. See Remark 9.

NTIPS

Input/output-integer-default=0. The number of domains (tip superelements to be created automatically when ACMS=‘YES’ If NTIPS=0, the number of domains is set equal to the number of processors.

APP

Input-character-default=” Analysis type. Allowable values: STATICS

Statics

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REIGEN

Normal modes

FREQRESP

Frequency response

TRANRESP

Transient response

CEIGEN

Complex eigenvalues

ZCOLLCT

Input/output-integer-default=-1. The absolute value is the number of collectors in the last level of a multilevel tree (see ACMS=‘YES). If ZCOLLCT0 and can be purged if SEQOUT=0. 3. Siemens PLM Software recommends SEQMETH=7 for sparse decomposition and sparse forward-backward substitution only. The assembly of stiffness, mass, and damping matrices by the EMA module can be less efficient under this option. Also, if there is insufficient memory available to perform sparse decomposition, regular decomposition is performed and regular decomposition is inefficient under this option. 4. SEQMETH=5, 6, or 7, resequencing is performed even if the CPU estimate is higher than for no resequencing. 5. For SEQMETH=8, the estimates are computed for two sequencing methods that are suitable for the decomposition method selected by the PARALLEL and SPARSE keywords on the NASTRAN statement. Also selects the sequencing method with the lowest estimate. The following table shows the suitable methods for each decomposition method. Decomposition method Non-sparse and non-parallel

1 and 4

Parallel

2 and 5

Sparse

6 and 7

6. Description of SUPER:

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•

If PARAM,SUPER=0, all grid points from the connection table that are not part of the group currently being processed are deleted. This option provides for sequencing only the interior points of a superelement. If any superelements are present, the residual structure is not resequenced. If all of the grid points are in the residual structure, they are resequenced.

•

If PARAM,SUPER=0 or 1, all grid points in the connection table are considered. This option provides for the recognition of passive columns.

•

If PARAM,SUPER=2, all points that are connected to multipoint constraints (via MPC entries) or rigid elements (for example, the RBAR entry) are placed in a special group at the end of the sequence. This option also forces SEQMETH=6 and cannot be selected with other values of SEQMETH. This option is intended primarily for models that have many active columns due to MPCs or rigid elements; for example, a model with disjoint structures connected only by MPCs or rigid elements. See the NX Nastran Numerical Methods User’s Guide for a further discussion of sequencing operations.

7. FACTOR is used as follows: SEQID = FACTOR * GRP + SEQ

where SEQ is a generated sequence number and GRP is a group sequence number. If GRP=0, use GRP(MAX)+1 where GRP(MAX) is the largest group sequence number previously processed. 8. START specifies that the input sequence is the sorted order of the grid point numbers including the effect of any SEQGP entries input by the user. A single SEQGP entry can be input to select the starting point for the new sequence. Otherwise, the first point of lowest connectivity is used as the starting point 9. PSEQOPT has the following values and actions: •

PSEQOPT=‘APPEND’ The list of all p-element grids at the bottom after all the regular grids. APPEND is intended for p-element analysis with p-version preconditioning, that is, SEQMETH = 5, 6 or 7.

•

PSEQOPT=‘INSERT’ Insert the p-element grids in appropriate locations immediately after the regular grid point to which they are associated, which is the default in p-element analysis. INSERT is intended for p-element analysis without p-version preconditioning, that is, SEQMETH = -1, 1, 2, 3 or 4.

Example: The following example generates a mapping matrix (SEQMAP) to resequence the matrix KAA. The following SMPYAD module resequences the rows and columns of KAA. Following the decomposition of the resequenced matrix (KAAX), the MPYAD resequences the right-hand side (PA) and FBS performs the forward/backward substitution on the resequenced right-hand side (PAX). The final MPYAD operation returns the solution (UAX) to the original sequence (UA). SEQP SMPYAD DECOMP MPYAD FBS MPYAD

KAA,,,/SEQMAP,//METHOD $ SEQMAP,KAA,SEQMAP,,,/KAAX/3////1////6 $ KAAX/LAA,/ $ SEQMAP,PA,/PAX/1 $ LAA,, PAX/UAX/ $ SEQMAP,UAX,/UA/ $

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9.319 SETMON Setup the parameters for the dof display in the solution monitor.

Format: SETMON

EQEXIN,USET/MGRID/MDOF/IOPT $

Input Data Blocks: EQEXIN

Equivalence table between external and internal grid/scalar identification numbers.

USET

Degree-of-freedom set membership table.

Parameters: MGRID

Input-integer. Grid ID for display.

MDOF

Input-integer. Grid dof for display.

IOPT

Input-integer. Analysis option. = 0 for direct frequency/transient. = 1 for modal frequency/transient.

9.320 SHPCAS Appends primary model’s case control based on boundary shapes Appends the primary model‘s case control based on auxiliary or geometric model loads (boundary shapes) and construct a vector for partitioning the primary model‘s solution matrices that correspond to the boundary shapes.

Format: SHPCAS

CASECC,YGBNDR/ CASECC1,CVEC $

Input Data Blocks: CASECC

Table of Case Control command images for the primary model

YGBNDR

Boundary shape matrices appended for all auxiliary or geometric models

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Output Data Blocks: CASECC1

Primary model Case Control table appended with extra subcases to account for the boundary shapes

CVEC

Partitioning vector for separating the primary model solutions from boundary shape induced solutions

Parameters: None.

9.321 SMA3 Assembles global stiffness based on general elements in GENEL Bulk Data entry Assembles the global stiffness based on general elements as defined on the GENEL Bulk Data entry and optionally adding to stiffness from regular elements.

Format: SMA3

GEI,KGG/ KGG1/ LUSET/NOGENL/NOSIMP $

Input Data Blocks: GEI

Table of general element data

KGG

Stiffness matrix in g-set with general elements

Output Data Block: KGG1

Matrix. The type (complex or real and single or double precision) of [X] is the maximum of the types of [A], [B..], a, and b. The size of [X] is the size of [A] if [A] is present. Otherwise, it is the size of [B ].

Parameters: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

NOGENL

Input-integer-no default. The number of general elements.

NOSIMP

Input-integer-no default. The number of simple elements. Set to -1 if there are no elements.

Remarks: KGG can be purged.

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9.322 SMPYAD Matrix series multiply and add Multiplies a series of matrices together: [X] = ± [A] [B] [C] [D] [E] ± [F]

Format: SMPYAD

A,B,C,D,E,F/ X/ NMAT/SIGNP/SIGNF/PREC/TA/TB/TC/TD/FORM

Input Data Blocks: A, B, C, D, E

Matrices multiplied from left to right (real or complex)

F

Matrix to be added to the above product (real or complex)

Output Data Block: X

Resultant matrix

Parameters: NMAT

Integer-input-no default. Number of matrices involved in the product; that is, [A][B][C][D][E].

SIGNP

Integer-input-default=1. Sign of the product matrix (that is, [A] [B] [C] [D] [E]): -1 for minus.

SIGNF

Integer-input-default=1. Sign of the matrix. [F], to be added to the product matrix: -1 for minus.

PREC

Integer-input-default=0. Output precision of the final result: 0 for choose proper precision, 1 for single precision, 2 for double precision.

TA, TB, TC, TD

Integer-input-default=0. Transpose indicators for the [A] [B] [C] and [D] matrices: 1 if transposed matrix to be used in the product, 0 if untransposed. The last nonpurged matrix must be untransposed.

FORM

Integer-input-default=0. Form of the X matrix. If FORM is zero, the form of [X] is 1 if the result is square, 2 otherwise. If [X] is known to be symmetric from physical principles, FORM can be set to 6.

Remarks: 1. Except for the final product, all intermediate matrix products are computed in machine precision.

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2. The matrices are post-multiplied from right to left; that is, the first product calculated is the product of matrix n-1 and matrix n. This implies that all purged inputs must be to the right. If the transpose flag is set for the last unpurged matrix, it is ignored without warning. 3. If the input matrices are incommensurate (for example, if the number of columns in A is not equal to the number of rows in B) or incompatible, the User Fatal Message 5423 “ATTEMPT TO MULTIPLY INCOMPATIBLE MATRICES” is issued. 4. The method used by this module is the same as for the MPYAD module except in case of a triple product, where [B] and [F] are symmetric and [A] = [C] and TA = 1; that is, [X] = [A]T[B][A] ± [F], a method that is more efficient than two equivalent MPYAD operations is employed. See Example 3. However, two equivalent MPYAD operations are selected automatically if two MPYADS are more efficient. (Two MPYADs can be forced by setting system cell 129 to 1, with PUTSYS(1,129) specified just before the SMPYAD module. The triple multiply can also be forced by setting system cell 129 to 2 for sparse [B] and to 3 for dense [B].) 5. If any of the matrices involved in the product do not exist, the module does not create any output.

Examples: 1. Compute [X] = [A] [B]T [C] - [F]. SMPYAD

A,B,C,,,F/X/3/1/-1/0/0/1 $

2. Compute [Z] = -[U]T [V]T [W]T [X]T [Y]. SMPYAD

U,V,W,X,Y,/Z/5/-1/0/0/1/1/1/1 $

3. Compute [f]T[M] [f]. SMPYAD

PHI,MAA,PHI, ,,/X/3////1////6 $

9.323 SOLVE Linear system solver Solves the matrix equation [A] [X] = ± [B] or the left-hand solution [X]T[A] = ± [B]T.

Format: SOLVE

A,B,SIL,USET,PARTVEC/ X/ SYM/SIGN/SETNAME $

Input Data Blocks: A

Square, symmetric or unsymmetric, matrix (real or complex)

B

Rectangular matrix (real or complex)

SIL

Scalar index list

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USET

Degree-of-freedom set membership table

PARTVEC

Partitioning vector which is specified when A and B are the zero-th partitions of the set specified by SETNAME

Output Data Block: X

Rectangular matrix. See Remark 1.

Parameters: SYM

Input integer default = 0 selects solution method.

SIGN

0

Use either symmetric or unsymmetric method consistent with symmetric or unsymmetric [A].

1

Use symmetric method

-1

Use unsymmetric method

2

Solve left-hand solution for [X]T

3

Compute inverse of [A]. See Remark 2.

Input integer default = 1. Sign of right-hand side flag.

SETNAME

1

Solve [A] [X] = [B]

-1

Solve [A] [X] = [-B]

Input-character-default = ‘H.’ Degree-of-freedom set name corresponding to A and B.

Remarks: 1. [X] is a rectangular matrix with the same dimensions as [B] and the maximum type of [A] and [B]. 2. If SYM = 3, [B] is ignored. If SYM≠ 3 and [B] is purged, [X] is purged; or if [B] is a null matrix, [X] is a null matrix. 3. By default, the SOLVE module uses sparse matrix methods. See Remark 1 under the DECOMP module description. 4. Parallel processing in this module (Method 1A only) is selected with the NASTRAN statement keyword PARALLEL (or SYSTEM (107)). To force parallel processing, also specify “NASTRAN FBSOPT = -2 SPARSE = 0”. 5. Data blocks USET, SIL, and PARTVEC and parameter SETNAME are required for the most efficient method of decomposition. PVEC is required only if A is not the same size as SETNAME.

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Examples: 1. Solve a system of equations [A] [X] = [P]. SOLVE A,P,,,/X/ $

2. Invert [A]. SOLVE A,,,,/AINV/3 $

3. Solve [X]T [A] = [P]T. SOLVE A,P,,,/X/2 $

9.324 SOLVIT Iterative solver Solves the matrix equation [A] [X] = ± [B] for [X] using a preconditioned conjugate gradient method. The element and the global iterative solutions have different formats, input data blocks, output data blocks, and parameters. The element based solution format is described below, then the global based solution format follows.

Format for element based solution: SOLVIT

KELM,PG,KDICT,SIL,ECT,BGPDT,CSTM,EDT,CASECC,USETB,RG,MPT, YGB,SLT,MDICT,MELM,EPT,,CNELM,ELCNST,ELCTST/UGV,QG,,/ V,Y,ISIGN/V,Y,IOPT/S,N,ITSEPS/V,Y,ITSMAX/V,Y,IPAD/V,Y,IEXT// NSKIP/V,Y,IMSGFL/V,Y,IDEBUG/V,Y,ITSERR/WTMASS $

Input data blocks for element based solution: KELM

Element stiffness matrix

PG

Load vector in g set

KDICT

Element stiffness dictionary

SIL

Scalar index list

ECT

Element connectivity table

BGPDT

Basic grid point data table

CSTM

Coordinate system transformation matrix

EDT

Element data table

CASECC

Case control command images

USETB

Degree-of-freedom set membership table

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RG

Constraint matrix in g set

MPT

Material property table

YGB

Specified non-zero displacements in g set

SLT

Static load table

MDICT

Mass dictionary

MELM

Element mass matrix

EPT

Element property table

CNELM

Glue element definition

ELCNST

Element normal stiffness

ELCTST

Element tangential stiffness

Output data blocks for element based solution: UGV

Displacements - g set

QG

SPC forces - g set

Parameters for element based solution: ISIGN

Not currently used.

IOPT

Input-integer. Preconditioner option

ITSEPS

Input-real-default = 1.0E-6. Convergence parameter epsilon.

ITSMAX

Input-integer-default = 1000. Maximum number of iterations.

IPAD

Not currently used.

IEXT

Not currently used.

ADPTINDX

Not currently used.

NSKIP

Input-integer-default=1. Record number of current subcase in CASECC

IMSGFL

Input-integer-default = 0. Output message flag

IDEBUG

Input-integer=default = 0. Debug flag

ITSERR

Output-integer-default = 0. Iterative solver return code.

WTMASS

Input,Real – Weight to mass factor

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Format for global non-p-version solution: SOLVIT

A,B,XS,PC,USET,KGG,GM,SIL,EQEXIN,EDT,CASECC,EQMAP/ X,R,PC1,EPSSE/ SIGN/ITSOPT/ITSEPS/ITSMAX/IPAD/IEXT/ADPTINDX/ NSKIP/MSGLVL/PREFONLY/S,N,ITSERR/SEID $

Format for global p-version solution: SOLVIT

A,B,XS,PS,USET,USET0,SIL0,SIL,EQEXIN,EDT,CASECC, EQMAP/ X,R,PG,EPSSE/ SIGN/ITSOPT/ITSEPS/ITSMAX/IPAD/IEXT/ADPTINDX/ NSKIP/MSGLVL/PREFONLY/S,N,ITSERR/SEID $

Input data blocks for global solution: A

Square matrix (real or complex, symmetric or unsymmetric)

B

Rectangular matrix (real or complex), the right-hand side

XS

Optional starting vector, same type as B (can be purged)

PC

Optional stepwise preconditioner, same type as A (can be purged.

USET

Degree-of-freedom set membership table. See Remark 3.

KGG

Stiffness matrix - g-set. See Remark 3.

GM

Multipoint constraint transformation matrix. See Remark 3.

USET0

USET table from previous adaptivity index in p-version analysis

SIL

Scalar index list

SIL0

SIL table from previous adaptivity index in p-version analysis

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers. Required for p-version preconditioning only.

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver.

CASECC

Table of Case Control command images. Required if SMETHOD Case Control command is used and NSIP=-1.

EQMAP

Table of degree-of-freedom global-to-local maps for domain decomposition

Output data blocks for global solution: X

Solution matrix. Rectangular matrix having the same dimensions and type as [B].

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R

Residual matrix. Rectangular matrix having the same dimensions and type as [B], the residual [R] = [B] - [A][X].

PC1

Updated stepwise preconditioner matrix. See Remark 6.

EPSSE

Table of epsilon and external work

Parameters for global solution: SIGN

Input-integer-default = 0. Sign flag for [B]. 0 : + [B] 1 : - [B]

ITSOPT

Input-integer-default = 0. Preconditioner flag. 0

Choose optimal method based on type of problem: ITSOPT Type of problem 6 p-version and real [A] and [B] 10 complex [A] and/or [B] 11 non p-version and real [A] and [B]

1

Jacobi preconditioning (default) for real, complex, symmetric and unsymmetric A

2

Incomplete Cholesky preconditioning or user-given preconditioner

3

Reduced incomplete Cholesky preconditioning. preconditioner (available for real symmetric A only)

4

User supplied for real, complex, symmetric A

5

Incomplete geometric, Jacobi hierarchic for real symmetric A

6

Complete geometric, Jacobi hierarchic for real symmetric A

7

Complete geometric, incomplete hierarchic for real symmetric A

10

Block incomplete Cholesky for well-conditioned real symmetric A (default for real A)

11

Block incomplete Cholesky for well-conditioned complex symmetric A (default for complex A)

1, XS and PC must be the solution matrix and pre-conditioner from the previous adaptivity p-level. Also, the USET and SIL from the previous p-level are specified for U and KGG and the USET and SIL from the current p-level are specified for GM and SIL. 8. For frequency response analysis with ITSOPT=10 or 11 (block incomplete Cholesky), IEXT=0 is not available and IEXT=1 is used automatically.

Global solution examples: 1. Solve [A][X]=[B] with Jacobi pre-conditioning with convergence established at 1.E-4 and maximum allowed iterations at 55 specified for the module parameters. SOLVIT

A,B,,,,,,,,,/X,,//1/1.E-4////-1 $

2. Same as 1 except parameters are obtained from the SMETHOD command and ITER entry. SOLVIT

A,B,,,,,,,,EDT,CASECC/X,, $

3. Same as 2 except for p-version analysis. DBVIEW SIL0 = SILS (WHERE PVALID=PVALOLD) $ DBVIEW UL0 = UL (WHERE PVALID=PVALOLD) $ DBVIEW USET0 = USET (WHERE PVALID=PVALOLD) $ DBVIEW PRECON0 = PRECON (WHERE PVALID=PVALOLD) $ SOLVIT KLL,PLI,UL0,PRECON0,USET,USET0,SIL0,SILS, EQEXINS,EDT,CASES/ UL,RUL,PRECON///////ADPTINDX/NSKIP $

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9.325 SSG1 Computes static load matrix. Computes the static load matrix based on static loads, thermal loads, and enforced deformation loads or heat transfer loads. Also generates the acceleration matrix due to inertial loads for design sensitivity analysis.

Format: SSG1

SLT,BGPDT,CSTM,MEDGE,EST,MPT,ETT,EDT,MGG,CASECC, DIT,UG,DEQATN,DEQIND,GPSNT,CSTMO,SCSTM,GEOM4, EPT,PCOMPT,COMPEST/ {PG or AG},PTELEM,SLTH/ LUSET/NSKIP/DSENS/APP/ALTSHAPE/TABS/SEID/LMFACT $

Input Data Blocks: SLT

Table of static loads

BGPDT

Basic grid point definition table

CSTM

Table of coordinate system transformation matrices

MEDGE

Edge table for p-element analysis

EST

Element summary table

MPT

Table of Bulk Data entry images related to material properties

ETT

Element temperature table

EDT

Table of Bulk Data entry images related to element deformation, aerodynamics, p-element analysis, divergence analysis, and the iterative solver. Also contains SET1 entries

MGG

Mass or radiation matrix in g-set

CASECC

Table of Case Control command images

DIT

Table of TABLEij Bulk Data entry images

UG

Displacement matrix in g-set

DEQATN

Table of DEQATN Bulk Data entry images

DEQIND

Index table to DEQATN data block

GPSNT

Grid point shell normal table

CSTM0

Table of coordinate system transformation matrices for the residual structure

SCSTM

Table of global transformation matrices for partitioned superelements

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GEOM4

Table of Bulk Data entry images related to constraints, degree-of-freedom membership and rigid element connectivity. Required for selected SPCD existence checks

EPT

Table of Bulk Data entry images related to element properties

PCOMPT

Table containing LAM option input and expanded information from the PCOMP Bulk Data entry

COMPEST

Composite solid element summary table

Output Data Blocks: PG

Static load matrix applied to the g-set

AG

Acceleration matrix due to inertial loads in the g-set. See DSENS

PTELEM

Table of thermal loads in the elemental coordinate system

SLTH

Table of static loads updated for heat transfer analysis

Parameters: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

NSKIP

Input-integer-default=1. The record number in CASECC corresponding to the first subcase of the current boundary condition.

DSENS

Input-integer-default=-1. Acceleration matrix creation flag. Set to 1 to generate AG, accelerations due to inertial loads.

APP

Input-character-default=‘STATICS’ Analysis type. ‘STATICS’

Generate loads for current boundary condition only.

‘BUCK’

Generate loads for first subcase only.

‘NLST’

Generate loads for nonlinear static or steady state heat transfer analysis.

‘ALL’

Generate loads for all subcases.

ALTSHAPE

Input-integer-default=0. Specifies set of displacement functions in p-element analysis. ALTSHAPE=0 selects the MacNeal set and 1 selects the Full Product Space set.

TABS

Input-real-default=0.0. Absolute temperature conversion. For example, set to 273.16 when specifying temperatures in Celsius, or set to 459.69 when specifying temperatures in Fahrenheit.

SEID

Input-integer-default=0. Superelement identification number.

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LMFACT

Scale factor for the stiffness matrix of Lagrange rigid elements.

Remarks: 1. One static load is built for each CASECC record starting with NSKIP + 1 as long as the boundary conditions are constant. IF NSKIP ≤ 0, it is set to zero. 2. In SLTH the heat transfer loads REFERENCING ELEMENTS (QVOL, QBDY1, QBDY2, QBDY3 and QVECT Bulk Data entries) have been converted to applied load factors and connected grid points. 3. SLT and BGPDT cannot be purged if external static loads or LOAD Bulk Data entries are selected in CASECC. 4. CSTM cannot be purged if any grid point or load references a coordinate system other than basic. 5. EST and MPT cannot be purged if thermal or element deformation loads are selected. 6. ETT cannot be purged if thermal loads are applied. 7. EDT cannot be purged if element deformation loads are selected. 8. MGG cannot be purged if GRAV or RFORCE loads are applied. 9. DIT cannot be purged if temperature-dependent materials are present. 10. UG can be purged, but geometric nonlinear effects are ignored. 11. PTELEM can be purged. 12. CSTM0 and SCSTM are required to support the MB=-1 on the GRAV and RFORCE Bulk Data entries.

9.326 SSG2 Reduces static load and enforced displacement matrices

Format: SSG2

USET,GM,YS,KFS,GOA,DM,PG,KOA/ QR,PO,PS,PA,PL $

Input Data Blocks: USET

Degree-of-freedom set membership table for g-set

GM

Multipoint constraint transformation matrix, m-set by n-set

YS

Matrix of enforced displacements or temperatures

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KFS

Stiffness matrix partition (f-set by s-set) from KNN

GOA

Omitted degree-of-freedom transformation matrix, o-set by a-set

DM

Rigid body transformation matrix for the r-set to the l-set

PG

Static load matrix applied to the g-set

KOA

o-set and a-set matrix partition of stiffness matrix

Output Data Blocks: QR

Matrix of determinate support forces

PO

Static load matrix partitioned to the o-set

PS

Static load matrix partitioned to the s-set

PA

Static load matrix reduced to the a-set

PL

Static load matrix reduced to the l-set

Parameters: None

Remarks: 1. GM cannot be purged if the m-set is present. 2. DM cannot be purged if the r-set and l-set are present. 3. PO cannot be purged if the o-set is present. 4. PS cannot be purged if the s-set is present. 5. QR and PL can be purged. 6. If there is no m-set, s-set, o-set, or r-set. no outputs are produced. 7. If QR or PS are computed to be null, QR or PS are purged. 8. If there is no r-set and PL is specified, PA is copied to PL. 9. If KFS or YS is purged, the outputs do not include the effect of enforced displacements.

9.327 SSG3 Computes static solutions

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Format: SSG3

LLL,UNUSED2,KLL,PL,LOO,UNUSED6,KOO,PO,LSEQ/ UL,UO,RUL,RUO,EPSSE/ NOOSET/UNUSED2/NSKIP/S,N,EPSI/S,N,EXTWORK/SEID $

Input Data Blocks: LLL

Lower triangular factor/diagonal for the l-set from KLL

UNUSED2

Unused and can be purged

KLL

Stiffness matrix reduced to the l-set

PL

Static load matrix reduced to the l-set

LOO

Lower triangular factor/diagonal for the o-set from KOO

UNUSED6

Unused and can be purged

KOO

Stiffness matrix partitioned to the o-set from KFF

PO

Static load matrix partitioned to the o-set

LSEQ

Resequencing matrix based on internal resequencing of KLL in DCMP

Output Data Blocks: UL

Displacement matrix in l-set

UO

Displacement matrix in o-set

RUL

Residual matrix for the l-set

RUO

Residual matrix for the o-set

EPSSE

Table of epsilon and external work.

Parameters: NOOSET

Input-integer-no default. Number of degrees-of-freedom in the o-set or omitted degree-of-freedom flag. Set to -1 if there are none.

UNUSED2

Input-integer-no default. Not used, but specify 0.

NSKIP

Input-integer-default=1. The record number in CASECC corresponding to the first subcase of the current boundary condition.

EPSI

Output-integer-default=1. Static solution error ratio flag. Set to -1 if the error ratio is greater than 1.E-3.

EXTWORK

Output-real-default=0.0. External work.

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Input-integer-default=0. Superelement identification number.

Remarks: 1. KLL can be purged if RUL is purged. 2. LOO, PO and UO can be purged if NOOSET0

Number of element quantities per element type to be output

0

Output all quantities for elements in a group if the absolute value of one or more elements is greater than BIGER

-1

Output sorted quantities with absolute value greater than BIGER

-2

Output filtered quantities with absolute value greater than BIGER

BIGER

Input-real-default=0.0. Minimum absolute value of element quantity to be output.

SRTOPT

Input-integer-default=0. Filter/sort option based on NUMOUT and BIGER. 0

Maximum magnitude

1

Minimum magnitude

2

Maximum algebraic

3

Minimum algebraic

SRTELTYP

Input-integer-default=0. Element type to be filtered and sorted. By default, all element types are filtered and sorted.

SRTTYP

Input-integer-default=0. Item code 1 sort flag. Set to 1 to perform an integer sort on item code 1 which is usually an integer quantity.

Remarks: 1. For further discussion see the DTI,INDTA and PARAM,S1 descriptions in the NX Nastran Quick Reference Guide. 2. SRTTYP=1 is used primarily to sort slideline element output by slave grid point identification number.

9.332 TA1 Combines element data into tables. Combines all of the element data (geometry, connection, and properties) into a table(s) convenient for generation of the element matrices (stiffness, mass, and so on) and output quantities (stress, force, and so on).

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Format: MPT,ECT,EPT,BGPDT,SIL,ETT,CSTM,DIT,ECTA,EHT/ EST,ESTNL,GEI,GPECT,ESTL,VGFD,DITID,NFDICT,COMPEST,NSMEST/ LUSET/S,N,NOESTL/S,N,NOSIMP/NOSUP/S,N,NOGENL/SEID/ LGDISP/NLAYERS/S,N,FREQDEP/BSHDAMP/S,N,BSHDMP/NSMID $

TA1

Input Data Blocks: MPT

Table of Bulk Data entry images related to material properties

ECT

Element connectivity table

EPT

Table of Bulk Data entry images related to element properties

BGPDT

Basic grid point definition table

SIL

Scalar index list

ETT

Element temperature table

CSTM

Table of coordinate system transformation matrices

DIT

Table of TABLEij Bulk Data entry images

ECTA

Secondary element connectivity table

EHT

Element hierarchical table for p-element analysis

Output Data Blocks: EST

Element summary table

ESTNL

Nonlinear element summary table

GEI

Table of general element data

GPECT

Grid point element connection table

ESTL

Linear element summary table

VGFD

Partitioning vector with ones at rows corresponding to degrees-of-freedom connected to frequency-dependent elements

DITID

Table of identification numbers in DIT

NFDICT

Nonlinear element energy/force index table

COMPEST

Composite solid element summary table

NSMEST

Non-structural mass element summary table

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Parameters: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

NOESTL

Output-integer-no default. ESTL generation output flag. Set to 1 if ESTL is generated; -1 otherwise.

NOSIMP

Output-integer-no default. The number of elements exclusive of general elements. Set to -1 if there are no simple elements.

NOSUP

Input-integer-no default. Element summary table request flag. 1

Generate EST only (usually for linear analysis)

2

Form EST, ESTNL and ESTL (usually for nonlinear analysis)

NOGENL

Output-integer-no default. The number of general elements.Set to -1 if there are no general elements.

SEID

Input-integer-no default. Superelement identification number.

LGDISP

Input-integer-default=1. Large displacement and follower force flag. -1

No large displacement and follower force effects are considered.

1

Large displacement and follower force effects are considered.

2

Only large displacement effects are considered.

NLAYERS

Input-integer-default=6. Number of layers to integrate through the thickness of CQUAD4 and CTRIA3 elements in nonlinear analysis.

FREQDEP

Output-logical-default=FALSE. Frequency-dependent element flag. Set to TRUE if frequency-dependent elements are present.

BSHDAMP

Input-character-default=‘DIFF’. Determines if the PBUSH/PBUSHT bulk entry fields GE2-GE6 and TGEID2-TGEID6 are considered. = SAME The fields GE2-GE6/TGEID2-TGEID6 are ignored, only the fields GE1/TGEID1 are considered and BSHDMP on the EMG module is assigned a value of 0. = DIFF The fields GE2-GE6/TGEID2-TGEID6 are considered. If all PBUSH/PBUSHT GE2-GE6/TGEID2-TGEID6 fields are blank, BSHDMP on the EMG module is assigned a value of 0. Otherwise, BSHDMP=1.

BSHDMP

Output-integer-default=0. BUSH structural damping strategy for EMG module. See BSHDAMP above and BSHDMP on EMG module for details.

NSMSID

Input-integer-default=0. Set identification number from the NSM Case Control command.

Remarks: 1. MPT, ESTL, and ESTNL can be purged if NOSUP=1.

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2. ECTA and EHT can be purged if p-elements or interface elements are not present. 3. GEI, ESTL, ESTNL, and DITID can be purged as long as EST is purged. 4. VGFD can be purged. 5. DITID can be purged as long as DIT is purged.

9.333 TABEDIT Performs editing operations on table data blocks Edits an existing table data block according to user-input directives. String-formatted records are generally not acceptable. Three types of editing operations are possible: 1. Delete, add, or replace entire records. New records come from the IFP module or from user input. 2. Delete, add, or replace word strings to a specified record. New data comes from user input. 3. Merge-edit two records of fixed-length word groups such as would be generated by IFP.

Format: TABEDIT

TOLD,CONTROL,TA,TB,TC/TNEW/ MSGLVL/DUPWG/UNUSED3/UNUSED4 $

Input Data Blocks: TOLD

Table data block to be edited. Cannot be purged, and in general, contains string-formatted records.

CONTROL

Table data block containing directives that control the editing process as described under Remarks (it usually comes from DTI input). If CONTROL is purged, TNEW is copied from TOLD.

TA,TB,TC

Secondary tables to be merged into TOLD. Can be purged.

Output Data Block: TNEW

Updated table data block from the edit process. Cannot be purged.

Parameters: MSGLVL

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Input-integer-default=0. Print activity option. 0 DUPWG

No print activity occurs

Input-integer-default=0. Duplicate word group option and applicable only to the Merge-Edit option. =0

Duplicate word groups are dropped from TOLD.

=1

Duplicate word groups are added after TOLD version.

UNUSED3

Input-integer-default=0. Unused.

UNUSED4

Input-integer-default=0. Unused.

Remarks: 1. The input data block CONTROL contains the directives that control the activity of the editing process. One record of CONTROL contains one directive of the form dir (,parameters) where “dir” is one of the directive codes from the table below and “parameters” represents the parametric values that vary with the directive. TABEDIT directives Directive

Remarks

ER

End Record-Edit processing by copying rest of TOLD to TNEW. This directive is optional.

QR, i

Quit Record-Edit processing by copying rest of TOLD onto TNEW through record i and exiting

DR, i or DR ,i ,j

Delete Record i (or records i through j) from TOLD after copying up to record i

IR, i

Insert Records from TOLD after copying up to record i

CR, i, options

Correct Record i (after copying up to record i) by deleting, adding or replacing word groups according to the options as described in Remark 2

KRA,n

Copy n Records from TA, TB, or TC onto TNEW

KRB,n KRC,n SRA,n SRB,n

Skip n Records forward on TA, TB, or TC. Used to position secondary data block TA, TB, or TC for a subsequent KR* operation.

SRC,n

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TABEDIT directives Directive MEA,i,n MEB,i,n

Remarks Merge-Edit the next record on TA, TB, or TC into record i according to IFP specifications for fixed-length word groups of length n.

MEC,i n INT

Interrogate TOLD for number of records and number of words in each record. Also print the first three words of each record.

2. The CR directive requires at least one subdirective from the table below: CR sub-directives Sub-directive

Remarks

QW, i

Quit after copying Word i. Record specified by CR directive is copied through word i and the rest of the record is ignored.

DW, i, j, n,n words

Delete Words i through j of the record specified by the CR directive and replace by the n words that follows on the CR directive record

IW, i, n,n words

Insert after Word i of the record specified by the CR directive the n words that follow on the CR directive record

KWA,n

Copy n Words from TA, TB, or TC onto TNEW

KWB,n KWC,n SWA,n SWB,n

Skip n words forward on TA, TB, or TC. Used to position secondary data block TA, TB or TC for a subsequent KW* operation.

SWC,n AWA,n AWB,n

Append n Words from TA, TB, or TC onto TNEW after copying the rest of the record specified by the CR directive.

AWC,n KRA,n KRB,n KRC,n

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Descriptions of DMAP Modules and Statements

CR sub-directives Sub-directive ARA ARB

Remarks Append the Remaining contents of the current record from TA, TB, or TC onto TNEW after copying the rest of the record specified by the CR directive

ARC 3. TABEDIT copies the name of the input data block to the output data block. Since the name is part of record 0, it can also be changed by TABEDIT commands.

Examples: Let GEOM1 generated by a previous run have a third record consisting of the five GRID entries. GRID,10,0,0.0,0.0,0.0,0,3456,0 GRID,20,0,1.0,1.0,0.0,0,3456,0 GRID,30,0,2.0,2.5,0.0,0,3456,0 GRID,40,0,3.0,3.0,0.0,0,3456,0 GRID,50,0,4.0,4.0,0.0,0,3456,0

A printout of GEOM1 using the TABPRT module (with OPT3=1) shows the following for record 1:

1. Note that the GRID entry for grid point 30 has an error in the y-location coordinate, which should be 2.0 instead of 2.5. Make this correction without going through the conventional XSORT-IFP process by using TABEDIT. Assume GEOM1 was saved on a user tape on the previous run as GEOM1C. DTIIN DTI,DTINDX/CONTROL,,,,,,,,, $ INPUTT2 /GEOM1C,,,,/-1 $ TABEDIT GEOM1C,CONTROL,,,/GEOM1X $ EQUIVX GEOM1X/GEOM1/ALWAYS $ END$ CEND BEGIN BULK DTI,CONTROL,1,CR,1,DW,23,23,1 ,2.0 DTI,CONTROL,2,ER,ENDREC ENDDATA

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2. Repeat Example 1, assuming that GEOM1 was saved on a previous run, by using record substitution. DTIIN DTI,DTINDX/CON,,,,,,,,, $ TABEDIT XGEOM1,CON,GEOM1,,/GEOM1X $ EQUIVX GEOM1X/GEOM1/ALWAYS $ END $ CEND BEGIN BULK DTI,CON,1,DR,1,ENDREC DTI,CON,2,KRA,1,ENDREC (all GRID entries, including the correction) ENDDATA

3. Repeat Example 2 by using word substitution. DTIIN DTI,DTINDX/CON,,,,,,,,, $ TABEDIT XGEOM1,CON,GEOM1,,/GEOM1X $ EQUIVX GEOM1X/GEOM1/ALWAYS $ END $ CEND BEGIN BULK DTI,CON,1,CR,1,DW,20,26,0 ,SWA,3,KWA,7 GRID,30,0,2.0,2.0,0,3456,0 ENDDATA

4. Repeat Example 1, assuming that GEOM1 was written onto a user file during the previous run, by using the merge-edit feature. DTIIN DTI,DTINDX/C,,,,,,,,, $ INPUTT2 GEOM1OLD,,,,/-1 $ TABEDIT GEOM1OLD,C,GEOM1,,/GEOM1X $ EQUIVX GEOM1X/GEOM1/ALWAYS $ END $ CEND BEGIN BULK DTI,C,1,MEA,1,8,ENDREC GRID,30,0,2.0,2.0,0.0,0,3456,0 ENDDATA

9.334 TABPRT Formatted table printer Formatted print of selected table data blocks.

Format 1: TABPRT

TABLE//KEY/OPT1//OPT3 $

Format 2: (KEY=’USET’) g-set TABPRT

USET,BGPDT//USET/OPT1/OPT2// SETSTR1/SETSTR2/SETSTR3/SETSTR4 $

TABPRT

USET,EQEXIN,SIL//USET/OPT1/OPT2// SETSTR1/SETSTR2/SETSTR3/SETSTR4 $

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p-set TABPRT

USETD,EQDYN,SILD//USET/OPT1/OPT2/ SETSTR1/SETSTR2/SETSTR3/SETSTR4 $

ks-set TABPRT

AEUSET,AEBGPDT//USET/OPT1/OPT2/ SETSTR1/SETSTR2/SETSTR3/SETSTR4

$

Format 3: (KEY=’SEMAP’) TABPRT

SEMAP,ESTDATA,TIMSIZ,SGPDT// ’SEMAP’/OPT1/OPT2 $

Input Data Blocks: TABLE

Table data block

USET

Degree-of-freedom set membership table for g-set

EQEXIN

Equivalence table between external and internal grid/scalar identification numbers

SIL

Scalar index list

BGPDT

Basic grid point definition table

USETD

Degree-of-freedom set membership table for p-set

EQDYN

Equivalence table between external and internal grid/scalar/extra point identification numbers

SILD

Scalar index list for p-set

AEUSET

Degree-of-freedom set membership table for ks-set

AEBGPDT

Basic grid point definition table for the ks-set

ESTDATA

Table of superelement estimation data overrides

TIMSIZ

Table of CPU and disk space estimation parameters

SGPDT

Superelement basic grid point definition table

Parameters: KEY

Input-character-default=‘FINDIT’. Identifies the generic name of the data block.

OPTi

Input-integer-default=0. Print control parameters.

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Format 1: OPT1

Input-integer-integer-default=0 OPT1=0. No blank lines between entries. OPT≠0. One blank line between each entry. Input-integer-default=0. Set selection flag for the row sort (OPT1=0 or 10).

SETSTRi

-1

All sets in the following table

0

Mutually exclusive sets only; that is, sets M, SB, SG, O, Q, R, C, BE, BF, E, SA, K, and A.

>0

Obsolete method for selecting mutually exclusive sets only according to the sum of their decimal equivalent numbers in the following table. For supersets and a more user-friendly method, use SETSTRi. In order to select specific sets to be printed, add the corresponding decimal equivalent numbers. For example, sets R, O, and M, OPT2=8+4+1=13. SetName

EquivalentDecimalNumber

Q

4194304

BE

2097152

C

1048576

K

262144

SA

131072

E

2048

SB

1024

SG

512

R

8

O

4

BF

2

M

1

Input-character-default=’ ’ Set name string for the row sort (OPT1 = 0 or 10). SETSTR1 through SETSTR4 form a single string of set name(s) that is 32 characters in length. For example, SETSTR1=‘M R N SG’and SETSTR2=‘A Q’specifies that the m, r, n, sg, a, and q sets be printed.

There are two table print options controlled by OPT3. If OPT3=0 (default);

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TABPRT

TABLE//KEY/OPT1 $

format statements built into TABPRT are used to print TABLE, as selected by KEY. These formats are limited to only those values of KEY listed in the table below. KEY

TABLE BGPDT

BDPDT

CSTM

CSTM

EQDYN

EQEXIN

EQEXIN

EQEXIN

ETT

ETT

GPDT

GPDT

GPL

GPL

GPLD

GPLD

GPTT

GPTT

SEMAP

SEMAP

any

FINDIT

USET

USET

If OPT3≠ 0; TABPRT

TABLE//NDDLNAME/OPT1//OPT3 $

the printout is identical to the TABPT module printout with the addition on NDDL item name labels appearing above each value. NDDLNAME must be any data block name listed on the DATABLK statement in the NDDL sequence. If NDDLNAME is not found in the NDDL sequence, the printout contains no item name labels. OPT3

Input-integer-default=0. If OPT3≠0, the table is printed in a format similar to the TABPT module with the following options: 1

Print with labels defined under the DATABLK statement for data block name specified for parameter KEY

2

Same as OPT3=1 and any data with an undefined format is printed as "???"

3

Same as OPT3=2 except only print records with undefined formats

-1

Print without labels

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Format 2: (KEY=’USET’): Input-integer-default=0. OPT1

Controls the tabular printout of the degree of freedom sets. Sequence

Print

None

Internal

External

USETPRT

None (default)

-1

Row sort only

0

Column sort only

1

Row and column sort

2

Row sort only

10

Column sort only

11

Row and column sort

12

The degrees of freedom can be listed in ascending order according to their internal or external sequence number, but not both. The external sequence number is the grid, scalar, or extra point identification number. The internal sequence number is the number assigned after resequencing. For a given sequence, there are two types of tables that can be printed: row sort and column sort. For row sort, a table is printed for each set selected by USETSEL. An example of row sort (USETPRT = 0 or 10) is shown below: U S E T

D E F I N I T I O N

-11=

-22-1

-3-

T A B L E -4-

( I N T E R N A L S E Q U E N C E , R O W S O R T ) A DISPLACEMENT SET -5-6-7-8-9-10-

2-2

For column sort, a single table is printed for the following sets: SB, SG, L, A, F, N, G, R, O, S, M, E. An example of column sort (USETPRT = 1 or 11) is shown below: U S E T D E F I N I T I O N T A B L E ( I N T E R N A L S E Q U E N C E , C O L U M N S O R T ) EXT GP. DOF INT DOF INT GP. SB SG L A F N G R O S M E -------------------------------------------------------------------------------------------------------1 - 1 11 G 1 1 1 1 - 2 22 2 2 2 - 3 31 3 3 3 - 4 42 4 4 4 - 5 53 5 5 5 - 6 64 6 6 6

Input-integer-default = 0. Specifies the sets that are printed in the row sort (OPT1 = 0 or 10). In order to select specific sets to be printed, you must sum their corresponding decimal equivalent numbers. For example, sets A, L, and R are selected with OPT2 = 128+256+8 = 392.

OPT2

OPT2 -1

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OPT2

Sets printed

0

Mutually exclusive sets only; that is, sets M, SB, SG, O, Q, R, C, B, E, SA, K, and A.

>0

Selected sets according to the sum of their decimal equivalent numbers in the following table

Table 9-1. Set Names and Their Decimal Equivalents. Set name

Decimal equivalent number

Set name

Decimal equivalent number

V

33554432

P

4096

FR

16777216

E

2048

T

8388608

SB

1024

Q

4194304

SG

512

B

2097152

L

256

C

1048576

A

128

J

524288

F

64

K

262144

N

32

SA

131072

G

16

KS

65536

R

8

D

32768

O

4

FE

16384

S

2

NE

8192

M

1

Format 3: Input-integer-default = 0. OPT1

If OPT2=0, 2, 3, or 5, OPT1 chooses a subset of record 2 for printing as follows:

OPT1 value 0

Selection within record 2 All parts (GRID list and summaries of GRID list)

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OPT1 value

Selection within record 2

1

Only GRID List

2

Only Summaries of GRID List

-g

GRID List for Pattern Starting with Entry GRID ID = G (if any)

10X+010X+2

Same as 0 or 2 but with Summary List.Selection based on X X = 0, 1, 3, 5, or 7 - 1st Summary (sorted by 1st GRID) X = 0, 2, 3, 6, or 7 - 2nd Summary (sorted by count) X = 0, 4, 5, 6, or 7 - 3rd Summary (sorted by superelement)

100+X

List all point IDs for any unique connection list produced by X

200+X

Same as 100+X except that additional pure interior points are not listed.

300+X

Same as 200+X except that additional nonresidual points are not listed

400+X

Same as 100+X except that additional scalar points are not listed.

500+X

Same as 200+X except that additional scalar points are not listed

600+X

Same as 300+X except that additional scalar points are not listed

If OPT2 = 4, OPT1 chooses CSUPER entry as follows: OPT1 value

Meaning

>0

Write CSUPER Bulk Data entries for superelement OPT1

≤ 0

Write CSUPER Bulk Data entries for residual structure but give SEID = - OPT1 Integer-default = 0. Print/punch selection as follows:

OPT2 OPT2 value

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Meaning of selection

-1

No output (1, 2 and a record for each superelement)

0

Print contents of all records (1, 2 and a record for each superelement) of SEMAP except last two

1

Print only Record 1 contents

2

Print contents of Records 1 (except for OPT1 < 0) and 2 (see OPT1 for selection options within Record 2)

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Descriptions of DMAP Modules and Statements

OPT2 value

Meaning of selection

3

Print contents of Records 1, 2 and a record for each superelement giving a list of internal points, a list of external points, a list of elements, and estimation data for the superelement. The third part of each superelement record (containing the lists of primary superelement points to which a secondary superelement is connected) is omitted.

4

Punch CSUPER entries according to OPT1 (see Remarks)

5

Print only Records 1 (except for OPT1 < 0), 2 (see OPT1 for selection options within Record 2), and estimation data for each superelement

Remarks: 1. If OPT2 = 4, CSUPER entries are written on the punch file according to OPT1. Field 2 (SEID) is selected by OPT1. Field 3 is 0. All other data fields contain the sorted list of grid points for either the selected superelement (OPT1 > 0) or the residual structure (OPT1 ≤ 0). Continuation mnemonics are generated in the form +xxxxyyy where xxxx is the left-adjusted SEID and yyy is a right-adjusted record count. Two examples are shown below. TABPRT TABPRT

EMAP//’SEMAP’/1/4 $ EMAP//’SEMAP’/-100/4 $

1

2

3

4

5

6

7

8

9

CSUPER

1

0

11

13

14

CSUPER

100

0

1

3

4

11

13

14

21

24

31

34

51

53

54

61

64

71

74

230

330

630

730

10

2. If OPT2 = 0,3 or 5 and TIMSIZ is supplied, TABPRT produces an estimation printout for each superelement except the residual structure. The equations used along with the semi-empirical constants are printed as well as dominant CPU time estimates, space estimates, and wall clock estimates. These estimates are valid for “large” superelements only and should be adjusted for anomalous characteristics. Estimate totals are also provided at the end of the SEMAP printout. If ESTDATA is also supplied, the constants of the estimating equations are adjusted. This technique is described on the Bulk Data entry DTI,ESTDATA. 3. Under Format 1, the generic data block name is used, but the actual DMAP name for the same or equivalent information is also acceptable. For example, in the superelement solution sequence, data blocks BGPDTS, CSTMS, EQEXINS, and GPLS are created and can be printed with TABPRT. If ‘FINDIT’ (default) is specified, the KEY is taken from the header of the data block.

Examples: 1. Print coordinate system transformation matrix table. TABPRT

CSTM//’CSTM’ $

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2. Print grid point list table. TABPRT

GPL//’GPL’ $

3. Print basic grid point definition table. TABPRT

BGPDT// $

4. Print GEOM3X table with labels taken from DATABLK statement in the NDDL. TABPRT

GEOM3X//’GEOM3’///1 $

5. Print USET list for g-set and s-set in internal order using row sort. TABPRT

USET,BGPDT//’USET’/0/18 $

6. Print USET for the mutually exclusive sets in internal order using column sort. TABPRT

USET,BGPDT//’USET’/1 $

7. Print all SEMAP information except the grid list and secondary superelement boundary sequencing list. TABPRT

EMAP//’SEMAP’/2/3 $

8. Punch CSUPER entries for the residual structure with SEID field set to 100. TABPRT

EMAP//’SEMAP’/-100/4 $

9. Print only estimation data for all superelements. TABPRT

EMAP,,TIMSIZ//’SEMAP’/-99999999/5 $

9.335 TABPT Table printer Prints table or matrix data blocks.

Format: TABPT

TAB1,TAB2,TAB3,TAB4,TAB5/ $

Input Data Blocks: TABi

Data block name

Remarks: 1. Each input data block is treated as a table and its contents are printed on the system output file via a prescribed format. Each word of the table is identified by the module as to type (real, character, integer) and an appropriate format is used (10 items per line). 2. The trailer data items for the table are also printed. 3. A warning message is issued if all TABi do not exist.

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4. TABPT can be used to print matrices. 5. TABPT can occasionally misidentify real numbers or character values. The TABPRT module with OPT3 ≠ 0 properly identifies real numbers and character values. 6. The TABPRT module with OPT3 ≠ 0 also prints tables like TABPT with labels above each item.

Examples: TABPT TABPT

GEOM1/ $ GEOM1,GEOM2,GEOM3,GEOM4/ $

9.336 TAFF Creates tables for follower force stiffness

Format: TAFF

SLT,BGPDT/ ESTF,GPECTF/ LUSET/LOADID/LOADIDP/LOADFACR/NBLOCK $

Input Data Blocks: SLT

Table of static loads

BGPDT

Basic grid point definition table

Output Data Blocks: ESTF

Element summary table for follower force stiffness

GPECTF

Grid point element connection table for follower force stiffness

Parameters: LUSET

Input-integer-default=0. The number of degrees-of-freedom in the g-set.

LOADID

Input-integer-default=0. Load set identification number for the current subcase.

LOADIDP

Input-integer-default=0. Load set identification number for the previous subcase.

LOADFACR

Input-real-default=0.0. Load factor in nonlinear static analysis.

NBLOCK

Input-integer-default=10. Number of spill blocks to form if “out-of-memory” algorithm is used.

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9.337 TAHT Adds records to element summary and grid point element connection table Adds to the element summary table and the grid point element connection table appropriate records for loads with control nodes on QVOL, QVECT, and QBDY3 Bulk Data entries.

Format: TAHT

Input Data Blocks: SLTH

Table of static loads updated for heat transfer analysis

DLTH

Table of dynamic loads updated for heat transfer analysis

EPT

Table of Bulk Data entry images related to element properties

SIL

Scalar index list

ESTNL

Nonlinear element summary table

GPECT

Grid point element connection table

DIT

Table of TABLEij Bulk Data entry images

Output Data Blocks: ESTNL1

Nonlinear element summary table updated for heat transfer analysis

GPECT1

Grid point element connection table for heat transfer analysis

Parameters: LUSET

Input-integer-no default. The number of degrees-of-freedom in the g-set.

NOSIMP

Output-integer-no default. The number of elements exclusive of general elements. Set to -1 if there are no simple elements.

LOADID

Input-integer-no default. Load set identification number for the current subcase.

STIME

Input-real-default=0.0. On initial input, starting time step and on output, accumulated time used for restarts.

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Remarks: DIT can be purged if DLTH does not reference tables in DIT.

9.338 TASNP1 Computes the shell normal vectors on a superelement‘s boundary

Format: TASNP1

BGPDTS,GPECTS,GEOM1S,CSTMS/ SNORMS $

Input Data Blocks: BGPDTS

Basic grid point definition table for a superelement

GPECTS

Grid point element connection table for a superelement

GEOM1S

Table of Bulk Data entry images related to geometry for a superelement

CSTMS

Table of coordinate system transformation matrices for a superelement

Output Data Block: SNORMS

Table of shell normal vectors on a superelement‘s boundary

Parameters: None.

Remarks: TASNP1 is intended to be executed for each superelement if partitioned superelements are present.

9.339 TASNP2 Computes grid point shell normal vectors at superelement boundaries Computes the grid point shell normal vectors and, if superelements are present, processes shell normals at superelement boundaries.

Format: Format without or ignoring superelements:

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TASNP2

Descriptions of DMAP Modules and Statements

BGPDT,GPECT,GEOM1,CSTM,,,/ GPSNT/ SNORM/SNORMPRT/-1/’’$

Format for superelement: TASNP2

BGPDTS,GPECTS,GEOM1S,CSTMS,SEMAP,SCSTM,SNORM*/ GPSNTS/ SNORM/SNORMPRT/SEID/QUALNAM $

Input Data Blocks: BGPDT

Basic grid point definition table

BGPDTS

Basic grid point definition table for a superelement

GPECT

Grid point element connection table

GPECTS

Grid point element connection table for a superelement

GEOM1

Table of Bulk Data entry images related to geometry

GEOM1S

Table of Bulk Data entry images related to geometry for a superelement

CSTM

Table of coordinate system transformation matrices

CSTMS

Table of coordinate system transformation matrices for a superelement

SEMAP

Superelement map table

SCSTM

Table of global transformation matrices for partitioned superelements

SNORM*

Family of shell normal vectors at superelement boundaries

Output Data Blocks: GPSNT

Grid point shell normal table

GPSNTS

Grid point shell normal table for a superelement

Parameters: SNORM

Input-real-no default. Maximum angle between grid point normal and shell normal. If angle is less than SNORM, grid point normal is computed.

SNORMPRT

Input-integer-no default. Grid point shell normal print/punch flag. 0 No print or punch 1 Punch

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2 Print only 3 Print and punch SEID

Input-character-no default. Name of qualifier to be used in selecting SNORMS.

QUALNAM

Input-integer-no default. Superelement identification number.

Remarks: If there are partitioned superelements present, TASNP1 must be executed for all superelements. When this is complete, TASNP2 is executed in a separate superelement loop for all superelements.

9.340 TIMETEST Provide timing data Provides timing data for various unit operations that can be used to compare and evaluate computer and compiler performance.

Format: TIMETEST

TIMTS,A,B,C/TOUT,/N/M/T/OPT/CASE $

Option 1: I/O timing TIMETEST

,,,,/,/N/M/T/2/CASE $

Option 2: Arithmetic timing TIMETEST

,,,,/,/N/M/T/2/CASE $

Option 3: Matrix timing TIMETEST

TIMTS3,,,/T3OUT,/N/M/T/3 $

Option 4: Kernel timing TIMETEST

TIMTS4,,,/T4OUT,/N/M/T/4 $

Option 5: MPYAD timing for CASE=1 TIMETEST

TIMTS5,,,/TOUT5,/N/5/1 $

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MPYAD timing CASE=2 (new) TIMETEST

TIMTS5,A,B,C/TOUT5,/N/M/T/5/2 $

Option 6: KERNBD generation TIMETEST

T3OUT,T4OUT,T7OUT,T8OUT/TOUT6,/ / / /6/CASE $

Option 7: Sparse kernel timing TIMETEST

TIMTS3,,,,/TOUT7,/N/M/ /7 $

Option 8: Element timing TIMETEST

TIMTS8,,,/TOUT8,/ / / /8/CASE $

Input Data Blocks: TIMTS3

Table created with DTI entries as follows:

1

2

DTI

3

TIMTS3

IREC

4 CASE

5 M

6 N

7

8

9

10

P

CASE

=

Record number (null records are ignored so records can be numbered by tens for convenience in making changes) IREC

CASE

=

“L” normal case definition.“K” indicates the last case to be used in the least squares solution for timing constants. Note: If no case value of K is found by the time the tenth case value is read, the tenth case is treated as the last case to be used in the least squares solution for timing constants.

M

=

Number of terms in inner loop

N

=

Number of terms in outer loop

P

=

Number of times kernel is called

TIMTS4 1 DTI

9-628

Table created with DTI entries as follows: 2 TIMTS4

3 IREC

DMAP Programmer’s Guide

4 CASE

5 ROWS

6 COLS

7 DENS

8 STRL

9

10

Descriptions of DMAP Modules and Statements

IREC

Record number (null records are ignored so records can be numbered by tens for convenience in making in making changes)

CASE

“A” normal case definition.“B” indicates the last case to be used in the least squares solution for timing constants. Note If no case value of B is found by the time the tenth case value is read, the tenth case is treated as the last case to be used in the least squares solution for timing constants.

ROWS

Number of rows the matrix is to have

COLS

Number of columns the matrix is to have

DENS

Density to be used in building the matrix

STRL

String length to be used in building the matrix (for CASE=1 only) Table created with DTI entries as follows:

TIMTS5 1

2

DTI

3

TIMTS5

CASE

5 ROWS

6 COLS

7 DENS

8 TYPE

9

10

STRL

(for both cases) Table created with DTI entries as follows:

TIMTS5 1

2

DTI

IREC

4

3

TIMTS5

IREC

4 CASE

5 T

6 CORE

7

8

9

10

METHOD

IREC

Record number (null records are ignored so records can be numbered by tens for convenience in making in making changes)

CASE

“CASE” normal case definition.“END” indicates the last case to be used. Note The T, CORE, and METHOD field are not populated when this form of the case is used.

T

Value to be used

CORE

Size of the core to be used

METHOD

Method to be used

TlMTS8

Element generation and assembly timing.

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Output Data Blocks: TOUT, TOUTi

Timing results

N

Options 1 and 2: n* - Default = 50. External loop index. Options 3, 4, and 5: Scale Factor. Negative value means scale down. Value 0 or 1 means do not change. Positive value means scale up. Options 6 and 8: Not used.

M

Options 1 and 2: m* - Default = 200. Internal loop index. Options 3, 4, and 7: Size - Contains the size of various needed arrays (recommended value range: 128 to 1024). (For example, Workstation machines: 128. Low-end minicomputer (VAX): 256. High-end minicomputer (CONVEX): 512.Super computer (CRAY): 1024). Options 5, 6, and 8: Not used.

T

Options 1 and 2: Default = 2. Data item type (1 = RSP, 2 = RDP, 3 = CSP, 4 = CDP). Options 3-8: Not used.

OPT

All Options: Type of timing data required. 1

Input/Output Operations (default) (old)

2

Arithmetic Operations (old)

3

Matrix Timing Operations (new)

4

Kernel Timing Operations (new)

5

MPYAD Timing Operations CASE = 1 (new). Uses data in DTI file. MPYAD Timing Operations CASE = 2 (new). Uses data defined by remaining arguments.

CASE

6

KERNDB Data Block Generation (new)

7

Sparse Kernel Timing (new)

8

Element Timing (new)

Options 1 and 2: Default = 0. Code indicating which unit operations are to be tested. If OPT = 1, CASE means:

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WRITE

2

READ

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4

READ BACKWARDS

8

BLDPK

16

INTPK

32

PACK

64

UNPACK

128

PUTSTR

256

GETSTR

If OPT = 2, CASE means: 1

RSP

2

RDP

4

CSP

8

CDP

Options 3 and 4: Not used. Option 5: If CASE = 1, use the DTI table. If CASE = 2, use the data defined by the remaining arguments. Option 6: Number of elements Option 7: Not used. Option 8: If CASE = 0, the T8OUT data block is initialized. If CASE = 1, record the cumulated CPU time on the T8OUT data block. Set CASE = 1 before executing the EMG module. If CASE = 2, record the cumulated CPU time on the T8OUT data block. Set CASE = 2 after executing the EMA module.

9.341 TOLAPP Appends nonlinear data and Case Control for data recovery

Format: Format for nonlinear transient analysis (TOLAPPF=0): TOLAPP

CASEXX,MPT,TEL/ TOL,,TOL1/ TOLAPPF/NSOUT $

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Format for nonlinear statics analysis (TOLAPPF=1): TOLAPP

CASECC,MPT,ESTNL/ OLF,CASECCR,/ TOLAPPF//S,N,NSKIP/S,N,NEWP/S,N,POUTF $

Input Data Blocks: CASECC

Table of Case Control command images

CASEXX

Subset of CASECC for current loop

MPT

Table of Bulk Data entry images related to material properties

TEL

Transient response time output list appended from each subcase

ESTNL

Nonlinear element summary table

Output Data Blocks: TOL

Transient response time output list for all subcases

OLF

Nonlinear load factors for all subcases

TOL1

Transient response time output list for the current subcase

CASECCR

Table of Case Control command images for data recovery

Parameters: TOLAPPF

Input-integer-no default. Nonlinear analysis type: 0

Nonlinear transient

1

Nonlinear statics

NSOUT

Input-integer-default=0. Number of time steps to output. By default, all time steps are output.

NSKIP

Input/output-integer-default=1. CASECC record counter or nonlinear transient loop identification number.

NEWP

Input/output-integer-default=1. New subcase flag.

POUTF

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-1

Current subcase has not been completed.

1

Current subcase has been completed.

Output-integer-default=1. Intermediate output flag. Set to -1 if intermediate output is not requested.

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Descriptions of DMAP Modules and Statements

Remarks: 1. If TOLAPPF=0, TOLAPP reads the time values from TEL and appends every NSOUT-th one to TOL. The last time value from TEL is appended regardless of the value of NSOUT. If NSOUT>0, a maximum of NSOUT time values are written to TOL. 2. If TOLAPPF=1, TOLAPP reads a record from CASEXX, modifies it, and appends it to CASECCR. If output has been requested (INTOUT field on the NLPARM Bulk Data entry) for this load factor, TOLAPP appends the current load factor from ESTNL to OLF.

9.342 TRD1 Solves for modal/direct transient analysis displacement, velocity, and acceleration solution.

Format: TRD1

CASECC,TRL,NLFT,DIT,KXX,BXX,MXX,PXT,SILD,USETD, PARTVEC,MIC/ UXT,PNL/ SOLTYP/NOUE/NONCUP/S,N,NCOL/FAC3/SETNAME/S,N,NMODES $

Input Data Blocks: CASECC

Table of Case Control command images

TRL

Transient response list

NLFT

Nonlinear Forcing function table

DIT

Table of TABLEij Bulk Data entry images

KXX

Stiffness matrix in any set. Usually h- or d-set.

BXX

Viscous damping in any set. Usually h- or d-set.

MXX

Mass matrix in any set. Usually h- or d-set.

PXT

Transient response load matrix in h-set (modal) or d-set

SILD

Scalar index list for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

USETD

Degree-of-freedom set membership table for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

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PARTVEC

Partitioning vector with values of 1.0 at the rows corresponding to degrees of freedom which were eliminated in the partition to obtain KXX, and so on. Required for maximum efficiency during symmetric decomposition and if KXX represents a subset of the d-set (SETNAME=‘D‘). PARTVEC is not required if KXX represents the h-set. See SETNAME parameter description below.

MIC

Initial conditions for modal coordinates. Only valid for SOLTYP=’MODAL’.

Output Data Blocks: UXT

Solution matrix from transient response analysis in d- or h-set. For SOLTYP=’PHYSMOD’, this is the initial conditions matrix input by the user in d-set with column 1 being initial displacements and column 2 being initial velocities.

PNL

Nonlinear load matrix appended from each output time step

Parameters: SOLTYP

Input-character-no default. Solution method. ‘MODAL’

Usually for h-set matrices

‘DIRECT’

Usually for d-set matrices

‘IC’

Initial conditions for direct transient analysis.

‘PHYSMOD’Initial conditions for modal transient analysis. ‘DIRMOD’ Same as ‘DIRECT’, but for mode acceleration with initial conditions. NOUE

Input-integer-no default. Number of extra points. Set to -1 if there are no extra points.

NONCUP

Input-integer-default=0. Algorithm selection. NONCUP=-1 requests uncoupled algorithm if SOLTYP=‘MODAL’and KXX, BXX, and MXX are diagonal. NONCUP=-2 requests uncoupled algorithm and off-diagonal terms of KXX, BXX, and MXX is ignored.

NCOL

Input/output-integer-default=0. Number of time steps in the solution matrix UXT prior to execution of TRD1.

FAC3

Input-complex-default=(1.0,0.0). Negative of the reciprocal of the time step increment.

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SETNAME

Input-character-default=‘H’ Degree-of-freedom set name represented by KXX, and so on. If KXX represents, or is a subset of, the d-set, for maximum efficiency, the rows and columns KXX and MXX must correspond to or be a partition of the displacement set specified by SETNAME. If KXX and MXX are a partition, PARTVEC must also be specified.

NMODES

Input-integer-default=0. Number of modes for SOLTYP=’PHYSMOD’ and user has entered modal initial conditions. Must be zero if SOLTYP=’PHYSMOD’ and user has entered non-modal initial conditions.

Remarks: 1. NLFT and PNLD1 cannot be purged if nonlinear loads are selected in CASEXX. 2. NCOL>0 indicates a restart. 3. Only CASECC, TRL, and UXT are required for SOLTYP=PHYSMOD. UXT is the matrix of initial conditions.

9.343 TRD2 Solves for modal/direct, transient, displacement, velocity, and acceleration solution

Format: TRD2

CASECC,TRL,NLFT,DIT,KXX,BXX,MXX,PXT,DSPT1,SILD, USETD,PARTVEC/ UXT,PNL,TOL/ SOLTYP/NOUE/NONCUP/S,N,NCOL/FAC3/TRD2OPT/SETNAME $

Input Data Blocks: CASECC

Table of Case Control command images

TRL

Transient response list

NLFT

Nonlinear Forcing function table

DIT

Table of TABLEij Bulk Data entry images

KXX

Stiffness matrix in any set. Usually h- or d-set.

BXX

Viscous damping in any set. Usually h- or d-set.

MXX

Mass matrix in any set. Usually h- or d-set.

PXT

Transient response load matrix in h-set (modal) or d-set

DSPT1

Design sensitivity processing table

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SILD

Scalar index list for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

USETD

Degree-of-freedom set membership table for the p-set. Required for maximum efficiency during symmetric decomposition and if KXX represents the d-set or a subset of the d-set (SETNAME=‘D‘).

PARTVEC

Partitioning vector with values of 1.0 at the rows corresponding to degrees of freedom which were eliminated in the partition to obtain KXX, and so on. Required for maximum efficiency during symmetric decomposition and if KXX represents a subset of the d-set (SETNAME=‘D‘). PARTVEC is not required if KXX represents the h-set. See SETNAME parameter description below.

Output Data Blocks: UXT

Solution matrix from transient response analysis in d- or h-set

PNL

Nonlinear load matrix appended from each output time step

TOL

Transient response time output list

Parameters: SOLTYP

Input-character-no default. Solution method. ‘MODAL’

Modal; usually for h-set matrices

‘DIRECT’

Direct; usually for d-set matrices

‘IC’

Initial conditions for nonlinear transient analysis

NOUE

Input-integer-no default. Number of extra points. Set to -1 if there are no extra points.

NONCUP

Input-integer-default=0. Algorithm selection. NONCUP=-1 requests uncoupled algorithm if SOLTYP=‘MODAL’and KXX, BXX, and MXX are diagonal. NONCUP=-2, requests uncoupled algorithm and off-diagonal terms of KXX, BXX, and MXX are ignored.

NCOL

Input/output-integer-default=0. Number of time steps in the solution matrix UXT prior to execution of TRD1.

FAC3

Input-complex-default=(1.0,0.0). Negative of the reciprocal of the time step increment.

TRD2OPT

Input-integer-default=1. TRD2 output option.

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1

Output based on TSTEP Bulk Data entry

2

Output based on every time step

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SETNAME

Input-character-default=‘H’ Degree-of-freedom set name represented by KXX, and so on. If KXX represents, or is a subset of, the d-set, for maximum efficiency, the rows and columns KXX and MXX must correspond to or be a partition of the displacement set specified by SETNAME. If KXX and MXX are a partition, PARTVEC must also be specified.

Remarks: 1. TRD2 is intended for design optimization. 2. NLFT and PNLD1 cannot be purged if nonlinear loads are selected in CASEXX. 3. NCOL>0 indicates a restart.

9.344 TRLG Generates applied loads in transient analysis

Format: TRLG

CASECC,USETD,DLT,SLT,BGPDT,SIL,CSTM,TRL,DIT, GMD,GOD,{PHDH or RPX},EST,MPT,MGG,V01P/ {PPT or PPT},PST,PDT,PDT1,{PHT or PXT},TOL,DLTH, YPT,YPO/ S,N,NOSET/S,N,PDEPDO/IMETHOD/STIME/BETA/ S,N,FAC1/S,N,FAC2/S,N,FAC3/TOUT/TABS/OPT $

Input Data Blocks: CASECC

Table of Case Control command images

USETD

Degree-of-freedom set membership table for p-set

DLT

Table of dynamic loads

SLT

Table of static loads

BGPDT

Basic grid point definition table

SIL

Scalar index list

CSTM

Table of coordinate system transformation matrices

TRL

Transient response list

DIT

Table of TABLEij Bulk Data entry images

GMD

Multipoint constraint transformation matrix with extra points, m-set by ne-set

GOD

Omitted degree-of-freedom transformation matrix with extra points, o-set by d-set

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PHDH

Transformation matrix from d-set to h-set (modal)

RPX

Reduction matrix from p-set to h-set (modal) or d-set

EST

Element summary table.

MPT

Table of Bulk Data entry images related to material properties

MGG

Mass or radiation matrix in g-size

V01P

Partitioning vector for sparse load reduction

Output Data Blocks: PPT

Transient response load matrix in the p-set for output time steps

PST

Transient response load matrix in the s-set for output time steps

PDT

Transient response load matrix in the d-set for output time steps

PDT1

Transient response load matrix in the d-set for all time steps

PHT

Transient response load matrix in the h-set (modal) for all time steps

PXT

Transient response load matrix in the h-set (modal) or d-set for all time steps only when RPX is input and TOUT=2

TOL

Transient response time output list

DLTH

Table of dynamic loads updated for heat transfer analysis

YPT

Transient response enforced motion matrix in the p-set

YPO

Transient response enforced motion matrix in the p-set and for the output time steps

Parameters: NOSET

Output-integer-default=-1. Constraint, omit, and support set flag. Set to -1 if NOMSET=-1, NOSSET=-1, NOOSET=-1, NORSET=-1 and no degrees-of-freedom are defined in the a-set (for example, ASETi, QSETi Bulk Data entries); +1 otherwise

PDEPDO

Output-integer-default=-1. Skip factor flag. See NOi on TSTEP Bulk Data entry. 0

Skip factor is >1. Skip factor is 1.

IMETHOD

9-638

Input-integer-default=0. Nonlinear transient analysis flag.

DMAP Programmer’s Guide

Descriptions of DMAP Modules and Statements

0

Linear analysis

-1 AUTO or TSTEP method (NLTRD module) 2

ADAPT method (NLTRD2 module)

STIME

Input-real-default=0.0. Accumulated time used for restarts.

BETA

Input-complex-default=(.33333,0.0). Integration parameter.

FAC1

Output-complex-default=(0.0,0.0). Square of the reciprocal of the time step increment. Imaginary part is always zero.

FAC2

Output-complex-default=(0.0,0.0). Reciprocal of twice the time step increment. Imaginary part is always zero.

FAC3

Output-complex-default=(0.0,0.0). Negative of the reciprocal of the time step increment. Imaginary part is always zero.

TOUT

Input-integer-default=-1. Processing flag.