Strut and Tie Modelling

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12/10/2010

ACI Web Sessions The audio for this web session will begin momentarily and will play in its entirety along with the slides.

Design Using the Strut-and-Tie Method, Part 2(A) ACI Spring 2010 Xtreme Concrete Convention March 21 - 25, Chicago, IL

ACI Web Sessions ACI is bringing you this Web Session in keeping with its motto of “Advancing Concrete Knowledge.” The ideas expressed, however, are those of the speakers and do not necessarily reflect the views of ACI or its committees. Please adjust your audio to an appropriate level at this time.

Fall 2010 ACI Seminars     

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1

12/10/2010

ACI Web Sessions This ACI Web Session includes four speakers presenting at the ACI Xtreme Concrete convention held in Chicago, IL, March 21st through 25th, 2010.

Design Using the Strut-and-Tie Method, Part 2(A)

Additional presentations will be made available in future ACI Web Sessions. Please enjoy the presentations.

ACI Spring 2010 Xtreme Concrete Convention March 21 - 25, Chicago, IL

Daniel Kuchma holds a B.A.Sc., M.A.Sc., and Ph.D., all in civil engineering, from the University of Toronto. Since 1997, he has been an Associate Professor in the department of Civil and Environmental Engineering at the University of Illinois, and has taught courses in structural dynamics, statics, reinforced concrete, and prestressed concrete. His work includes a variety of consulting projects involving offshore structures, hydroelectric dams, towers, buildings and specialty structures. Dr. Kuchma is an active member of ACI, and the Federation International de Beton (fib). He received a National Science Foundation CAREER Award on “Tools and Research to Advance the Use of Strut-andTie Models in Education and Design.” He is also a National Center for Supercomputing Applications Faculty Fellow and University of Illinois Collins Scholar.

Propped Cantilever with Opening Dan Kuchma Sukit Yindeesuk Tjen Tjhin University of Illinois

10

Design problem

Selected truss model 

5625 kN

Externally and internally indeterminate truss

535 mm

5800 kN 5625 kN

A

B

C

2895 mm

D

L

K

O

M

Q

P

E

R

F

570 mm 11

H

1590 1015 mm mm

I 2030 mm

3659 kN

41 T 36 k

U G

4000 mm 3229.5 kN

S

N

J 1015 1350 mm mm

N

418.8 kN

49 degrees

12

2

12/10/2010

Outline of Presentation

ACI design; calculation of nominal capacity

Calculated plastic truss capacity



Calculated non-linear truss capacity



Predicted capacity and behavior by nonlinear finite element analysis

Reinforcement and strut/node dimensions selected to provide adequate capacity 46

3409 3265

2662 -486 3 3650

2535 15 4

3650 0 43

-4090

209 -2 54 3860

70

5615

821 52 0 -421 -45

Observations and Conclusions

69

7 94 -6

-38

Measured capacity and behavior by experimental testing

1243 -536 0 2083

-4

-7500 -3860 -3796 -79 2146 35





-38



Member forces determined assuming equal stiffness of member forces

-87 3716 3410





1582 1670 -305

ACI design; calculation of nominal capacity

144 1781 1828



-821

-949

13

Calculated plastic truss capacity

ACI design; calculation of nominal capacity



Occurs at top right tie; Pn = 7500 kN



Utilization rates shown in figure 0.452 0.039

0.02 1.01(O/S) 0.924

0.496

0.429

0.01

0.89 0.92

0.524

0.525

0.942 0.0 16 0.04

54

0.990 0.6 33

86

0.078 0. 03 3

Member stress-strain characteristics

0.227 1.01(O/S) 0. 07 0.054 5 0.

0.764

96 0.4

28 0.3

2 39 0.

0.343 0.69 8 0.774



0.4

0.520 0.188 0.185 0. 01 0.798

0.495

Nominal design strength taken as when first members reaches its capacity

0.039 0.483



14

0.035

15

Calculated plastic truss capacity

16

Calculated non-linear truss capacity



P = 9469 kN



Capacity reaches when a mechanism forms



P = 9301 kN

0.724

0.476 0.014

0.971 0.0 06

0.006

0.08

0.988 0.7 38 0.730

0.468

0.973 0.981 0.015

0.521

0.001 1.002 1.009

1.009 0.997 0.041

0.528

0.016 0. 07

0.714

11

17

0.985

0.988

0.047 0. 03 1 0.019

0.5

0.018

0.012 0.76 2

3 61

0.734

0.922 0.0 25 0.009

0 52 0.

5 60 0.

0.993 0.7 31

0.481 0.267 0.271 0. 01 3 0.959 69 0.3

0.743

0.994

0.115 0.639 0 .0 05 0.003

0

0.025 0.0 11

0.122 0.7 43

48 0.

0.999

0.919 97 0.5

63 0.3

7 52 0.

0.284 0. 03 3

0.

0.274

0.973

Similar demands as by plastic truss model

1.000

Capacity reaches when a mechanism forms

0.008 0.520 0.506



0.489 0.526 0.002

Non-linear stress-strain relationship



0.013 0.562 0.521



0.482

Very different distribution of demands



0.008

18

3

12/10/2010

Predicted capacity and behavior by non-linear finite element analysis

Comparison of strength calculations



Predicted state of cracking at ultimate



P = 16622 kN

Pn Pu

19

20

Predicted capacity and behavior by non-linear finite element analysis 

Predicted capacity and behavior by non-linear finite element analysis

Predicted distribution of steel stress at ultimate



Compressive Demand: ratio of compressive stress to compressive capacity at failure



P = 16622 kN

Stress (Steel):  -truss at crack 46.06 64.52 82.98 101.43

119.89 138.35 156.81 175.27

193.73 212.18 230.64 249.10

267.56 286.02 304.48 322.93

341.39 359.85 378.31 396.77

Vital Signs: Fcm

415.23 433.68 452.14 470.60

0.04 0.08 0.13 0.17

0.21 0.25 0.29 0.33

0.38 0.42 0.46 0.50

0.54 0.58 0.63 0.67

0.71 0.75 0.79 0.83

21

Measured capacity and behavior by experimental testing 

0.88 0.92 0.96 1.00 22

Measured capacity and behavior by experimental testing 

Reinforcing cage

23

Test Setup

24

4

12/10/2010

Measured capacity and behavior by experimental testing 

Comparison of strength calculations

Mode of failure

Pn Pu

25

Observations and Conclusions 1.

Truss member design forces in statically indeterminate strut-and-tie models depend on the relative stiffness of members

2.

Plastic truss capacity can be modestly larger than when the first member reaches its capacity

3.

Truss models cannot provide a good estimate of deformation; much softer than in reality

4.

Non-linear finite element analysis can predict well the behavior of complex STM designed regions

26

Questions

27

Hakim Bouadi is a Senior Associate with Walter P Moore & Associates in Houston, Texas, which provides structural, structural diagnostics, civil, traffic and transportation engineering, and parking consulting services to clients worldwide.

28

STM Design of two Link Beams at a Medium-Rise Building Hakim Bouadi, Ph.D., P.E. Asif Wahidi, Ph.D., P.E. WALTER P MOORE

5

12/10/2010

Outline

148'-0"

    

Building Overview

351'-0"

Building Overview Link Beam Overview Link Beam with Moderate Shear Link Beam with High Shear Conclusions

142'-0"

256'-0"

Hospital building Location: Las Vegas, Nevada Lateral design controlled by seismic forces

31

STM Design of two Link Beams at a Medium-Rise Building

31

WALTER P MOORE

32

STM Design of two Link Beams at a Medium-Rise Building

Building Overview

32

WALTER P MOORE

Shear Wall Overview

48'-7"

 Shear walls with link beams above openings  Link beam: deep beams per ACI 318 definition  Review link beam at roof and at level 3

18'-0"

18'-0"

18'-0"

15'-0"

351'-0"

15'-0"

15'-0"

15'-0"

15'-0"

15'-0"

148'-0"

48'-7"

256'-0"

18'-0"

142'-0"

Plan size: about 500 ft by 400 ft Lateral resisting system: shear walls Controlling lateral loads: seismic forces

33

STM Design of two Link Beams at a Medium-Rise Building

33

WALTER P MOORE

34

STM Design of two Link Beams at a Medium-Rise Building

34

WALTER P MOORE

.

Link Beam Overview

Roof Link Beam  External forces applied at nodes  Shear force equal to about:

4.25  f c ' bw d

   

 Beam under constant shear and moment reversal  Forces on nodes obtained from global lateral analysis  Reduce forces to ends

35

STM Design of two Link Beams at a Medium-Rise Building

35

WALTER P MOORE

36

External nodes at location of wall reinforcement Horizontal tie at location of reinforcement Vertical tie at mid-span Improvement: Extend model into wall

STM Design of two Link Beams at a Medium-Rise Building

36

WALTER P MOORE

6

12/10/2010

Forces on Members

Design of Struts and Ties

 Force resolved by analysis  Check struts  Design ties  Check nodes  Detailing

37

STM Design of two Link Beams at a Medium-Rise Building

37

WALTER P MOORE

 Strut and tie dimensions from geometry  Struts: fan shaped  Capacity of struts checked at strut and at nodes  Tie force resisted by reinforcement

38

Design of Struts and Ties

STM Design of two Link Beams at a Medium-Rise Building

38

WALTER P MOORE

Node Capacity

• Vertical tie: 8#5 stirrups As 

Fu

 fy



187  4 . 15 in 2 0 . 75  60

 Nodal dimensions from geometry  Node type CCT due to tension force in wall reinforcement  Check capacity on each face

• Horizontal tie: 4 #7 As 

Fu

 fy



94.9  2.18 in 2 0.7560

• Develop beyond extended nodal zone

 0.85  n f c' wb  0.75  0.85  0.8  5.5  8.5  12  286 kips

• Strut Fu   0.85 s f 'c b w  0.75  0.85  0.60  5.5 8.5 12  215 kips

39

STM Design of two Link Beams at a Medium-Rise Building

39

WALTER P MOORE

40

Node Capacity

STM Design of two Link Beams at a Medium-Rise Building

40

WALTER P MOORE

Design: Roof Link Beam,

 Node type CTT due to tension force in wall reinforcement  Check capacity on each face  0.85 n f c' wb  0.75  0.85  0.6  5.5  7  12  176 kips

41

STM Design of two Link Beams at a Medium-Rise Building

41

WALTER P MOORE

42

STM Design of two Link Beams at a Medium-Rise Building

42

WALTER P MOORE

7

12/10/2010

Link Beam at Level 3

Forces for Level 3 Link Beam

15'-0"

48'-7"

15'-0"

 Shear force equal to about: 15'-0"

10  f c ' bw d

18'-0"

18'-0"

 Design using STM  Follow also Chapter 21 of ACI: Seismic Design/Detailing

 Shear force equal to about:

10  f c ' bw d

   

 Design using STM  Follow also Chapter 21 of ACI: Seismic Design/Detailing

43

STM Design of two Link Beams at a Medium-Rise Building

43

WALTER P MOORE

44

Model for Level 3 Link Beam

STM Design of two Link Beams at a Medium-Rise Building

45

WALTER P MOORE

STM Design of two Link Beams at a Medium-Rise Building

44

WALTER P MOORE

Design for Level 3 Link Beam  Forces resolved through geometry  Symmetric design due to load reversal  Tie force resisted by reinforcement (4#11 and 2#9)  Strut force resisted by concrete and reinforcement

 External nodes at location of wall reinforcement  Transfer forces through “X” configuration

45

External nodes at location of wall reinforcement Horizontal tie at location of reinforcement Vertical tie at mid-span Improvement: Extend model into wall

46

Detailing for Level 3 Link Beam

STM Design of two Link Beams at a Medium-Rise Building

46

WALTER P MOORE

Summary for Level 3 Link Beam

 development length of beyond extended nodal zone extended by 25%  Minimum web reinforcement  Appendix A  ACI Chapter 21 (controls)  Enclose Tie reinforcement with stirrups

47

STM Design of two Link Beams at a Medium-Rise Building

47

WALTER P MOORE

48

STM Design of two Link Beams at a Medium-Rise Building

48

WALTER P MOORE

8

12/10/2010

STM Design of two Link Beams at a Medium-Rise Building

Conclusions  STM use for link beam design  Different models are possible  Model can be extended into the wall to follow force transfer  Check detailing (in addition to design)

Thank you Hakim Bouadi, Ph.D., P.E. Asif Wahidi, Ph.D., P.E. WALTER P MOORE

49

STM Design of two Link Beams at a Medium-Rise Building

49

WALTER P MOORE

MIC-Earlington Heights Connector Metrorail

Richard Beaupre received his Bachelor of Science and Engineering from the University of Florida and his Master of Science from the University of Texas at Austin. While at the University of Texas he was involved in research pertaining to deviation saddle behavior and design for externally post-tensioned segmental concrete girder bridges. He is currently a senior bridge engineer for URS Corporation in Tampa, Florida, where he is responsible for design of steel and concrete bridges, ship impact designs, structural modeling, and quality control. He is experienced in design of major bridge structures, including cable-stayed, posttensioned segmental concrete and movable.

Richard Beaupre, PE Robert (Bob) Anderson, PE Velvet Bridges, PE URS Corporation Tampa, Florida

Diaphragm for a Segmental Concrete Bridge ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Introduction

Project Overview

• Many Areas of a Concrete Segmental Bridge can be Classified as a “D” Region – Pier Diaphragms – Interior Segment Diaphragms at Deviation Points for External Tendons – Openings in Flanges and Webs – Pile Caps ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

9

12/10/2010

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Superstructure Requirements

Miami Intermodal Center MIC-EARLINGTON HEIGHTS METRORAIL EXTENSION

• 130’ Spans in Miami Intermodal Center • 225’ Span to Clear the Miami River with a 40’ Vertical Clearance • 180’ Span for the South Florida Railroad Corridor • 256’ Span to Cross to SR112 and the Future Dade Expressway • Height Restrictions Set by FAA Airspace near MIA

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Superstructure Types

Guideway Structures Overview  72” Florida U-Beams - Single Track Guideway

• • • •

72” Florida Prestressed U-Beams Segmental Concrete Boxes 30” Cast-In-Place Concrete Slabs Single Track and Dual Track CrossSections

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Guideway Structures Overview  72” Florida U-Beams - Dual Track Guideway

ACI 2010, Chicago, IL

Guideway Structures Overview  Single Track Guideway (Units 1 thru 4 & 14)

ACI 2010, Chicago, IL

10

12/10/2010

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Guideway Structures Overview

Diaphragm Example

 Dual Track Guideway (Units 5 thru 9 & 11 thru 13)

• • • •

ACI 2010, Chicago, IL

Layout Function Boundary Forces Strut-Tie Model

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Diaphragm Example

Layout

• Unit 8

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Pier Diaphragm Function

Layout

• Transfer Loads from the Webs to the Support around Access Openings • Distribute Tendon Anchorage Forces to the Cross-section

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

11

12/10/2010

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Rapid Transit Live Load Vehicle • Full Live Load Weight of 120 kips • Train – 2 to 8 Vehicles

ACI 2010, Chicago, IL

Diaphragm Loadings

Shear Factored Loading Case Kips/Box (kN/Box)

(kN*m/Box)

Strength I (Maximum Shear)

3,291

(14,638)

21

(28)

Extreme Event III (Maximum Torsion)

2,634

(11,716)

5,355

(7,260)

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

Diaphragm Unit Loads for Shear

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

Diaphragm Unit Loads for Torsion

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Strut-Tie Model Steps • Step 1:

Determine strut-and-tie arrangement based on boundary forces

• Step 2:

Solve for the member forces

• Step 3:

Determine the amount of steel for ties

• Step 4:

Arrange tie steel

• Step 5:

Check anchorage zone for the ties

• Step 6:

Check diagonal struts

• Step 7:

Check nodal zones

ACI 2010, Chicago, IL

Torsion KipFt/Box

Pier Diaphragms Reference: Schlaich et. al., ”Towards a Consistent Design of Structural Concrete”, PCI Journal, Vol. 32, No. 3, May-June 1987

ACI 2010, Chicago, IL

12

12/10/2010

MIC-Earlington Heights Connector Metrorail

Model Members with Shear Unit Loads

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

Model Members with Torsion Unit Loads

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Material Properties

Results for Shear Only

• Concrete: f’c=8,500 psi (58.7 MPa) • Reinforcement: fy= 60,000 psi (414 MPa)

ACI 2010, Chicago, IL

Extreme Event III V=2634 k (11,716 kN)

Unit Force

Kips

(kN)

Kips

(kN)

1

0.450

740.9

(3295.3)

593.0

(2637.5)

2

0.267

439.4

(1954.4)

351.7

(1564.2)

3

0.267

4

439.4

(1954.4)

351.7

(1564.2)

0.450

740.9

(3295.3)

593.0

5

-0.792

-1302.7

(-5794.4)

-1042.6

(-4637.7)

6

-0.467

-768.5

(-3418.1)

-615.0

(-2735.7)

(2637.5)

7

-0.467

8

-768.5

(-3418.1)

-615.0

(-2735.7)

-0.792

-1302.7

(-5794.4)

-1042.6

(-4637.7)

9

-1.000

-1645.5

(-7319.2)

-1317.0

(-5858.0)

10

-1.000

-1645.5

(-7319.2)

-1317.0

(-5858.0)

11

-0.363

-596.5

(-2653.2)

-477.4

(-2123.5)

12

-0.363

-596.5

(-2653.2)

-477.4

(-2123.5)

13

0.000

0.0

(0.0)

0.0

14

0.000

0.0

(0.0)

0.0

(0.0)

15

1.020

1678.7

(7466.9)

1343.6

(5976.2)

16

0.001

0.9

(4.2)

0.7

(3.3)

17

1.020

1678.7

(7466.9)

1343.6

(5976.2)

18

0.001

0.9

(4.2)

0.7

(3.3)

(0.0)

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

Results for Torsion Only Member

Unit Force

1

-0.015

2

-0.009

Strength I T=21 k-ft (28 kN-m) Kips (kN) -0.3 (-1.4) -0.2

(-0.8)

MIC-Earlington Heights Connector Metrorail

Results for Shear and Torsion Combined

Extreme Event III T=5354 k-ft (7258 kN-m) Kips (kN) -81.1 (-360.8) -48.1

1

Strength I Kips (kN) 740.5 (3293.9)

(-214.0)

2

439.2

(1953.5)

Member

Extreme Event III Kips (kN) 511.8 (2276.7) 303.6

3

439.2

(1955.2)

0.015

0.3

(1.4)

81.1

(360.8)

4

741.2

(3296.8)

674.1

(2998.3)

5

-0.027

-0.6

(-2.5)

-142.6

(-634.4)

5

-1303.3

(-5796.8

-1185.3

(-5272.1)

(749.3)

6

-767.8

(-3415.1)

-446.6

(-1986.4)

0.009

0.2

(0.8)

48.1

6

0.031

0.7

(2.9)

168.5

7

-0.031

-0.7

(-2.9)

-168.5

7

(-749.3)

8

-769.1 -1302.1

(-3421.0)

399.8

(1350.2)

(214.0)

4

3

ACI 2010, Chicago, IL

Strength I V=3291 k (14,638 kN)

Member

-783.5

(1778.2)

(-3485.0)

8

0.027

0.6

(2.5)

142.6

(634.4)

(-5791.9)

-900.0

(-4003.3)

9

-0.105

-2.2

(-9.8)

-562.3

(-2501.2)

9

-1647.7

(-7329.0

-1879.3

(-8359.2)

10

0.105

2.2

(9.8)

562.3

(2501.2)

10

-1643.4

(-7309.4)

-754.7

(-3356.9) (-1833.0)

11

0.012

0.3

(1.1)

(290.5)

11

-596.8

(-2652.1)

-412.1

12

-0.012

-0.3

(-1.1)

-65.3

(-290.5)

12

-596.8

(-2654.4)

-542.7

13

0.086

1.8

(8.0)

458.5

(2039.3)

13

1.8

(8.0)

458.5

(2039.3)

14

-0.086

-1.8

(-8.0)

-458.5

(-2039.3)

14

-1.8

(-8.0)

-458.5

(-2039.3)

15

0.700

0.7

3.2

183.8

(817.5)

15

1679.4

(7470.1)

1527.4

(6793.8)

65.3

16

0.0

0.0

0.0

0.0

(0.1)

17

-0.700

-0.7

-3.2

-183.8

(-817.5)

18

-0.0

0.0

0.0

0.0

(-0.1)

(-2414.1)

16

0.9

(4.2)

0.8

(3.5)

17

1678.0

(7463.7)

1159.8

(5158.7)

18

0.9

(4.2)

0.7

(3.2)

ACI 2010, Chicago, IL

13

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MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Ties 1 to 4 – Top Tie According to ACI 318 equation A-1 Fnt>Fut. Where: Fut = Factored Design Force = 741 k (3,297 kN) = 0.75 (Section 9.3.2.6) Fnt = Nominal Strength of a Tie Where no prestressing steel is used, Fnt = Atsfy (Section A.4.1) Using 1 row of 11 – # 11 diameter reinforcing bars.

Tie 13 – Diagonal Tie Similarly for Tie 14 (depending on direction of torsion), Fut = Factored Design Force = 459 k (2,039 kN) = 0.75 (Section 9.3.2.6) Using 10 – # 9 diameter reinforcing diagonal bars. Ats  10 bars  1.00 in 2  10.0 in 2 (6,452 mm2 )

Fnt  0.75  10.0 in 2  60 ksi  450 k (2,669 kN)  459 k (2,039 kN)

Ats  1 rows 11 bars 1.56 in 2  17.2 in 2 (10,064 mm2 )

Fnt  0.75 17.2 in 2  60 ksi  774 k (3443 kN)  741 k (3297 kN)

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Ties 15 and 17 – Hanging Up Tie

Main Tie Reinforcing

Fut = Factored Design Force = 1679 k (7,470 kN) = 0.75 (Section 9.3.2.6) Using 28 – # 8 diameter reinforcing web bars plus 11 - # 11 bars (continue Tie 1 to 4 reinforcement) Ats  28 bars  0.79 in 2  17 . 2 in 2  39.3 in 2 (25,368 mm 2 )

Fnt  0.75  39.3 in 2  60 ksi  1,768 k (7,864 kN)  1,679 k (7,470 kN)

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Nodal Zone Detail at Bearing Support

Strut 14 According to ACI 318 equation A-1 Fns>Fus Where: Fus = Factored Design Force = -459 k (-2,039 kN) = 0.75 (Section 9.3.2.6) Fns = Nominal Strength of a Strut = fceAcs Further, f ce  0.85 s f 'c Where:  s  0.60 (Section A.3.2.2 (b) – bottle shaped struts without reinforcing of A.3.3.1) Therefore, f ce  0.85  0.60  8500 psi  4335 psi (29.9 MPa) Multiply the allowable compressive stress of a strut by the area of concrete available to carry the stress which is limited by the access opening (width is 4.9 in). Acs  4.9 in  28.9 in  141.6 in 2 (0.09 m 2 )

Fns  0.75  4335 psi  141.6 in 2 / 1000  460 k (2,048 kN)  459 k (2,039 kN)

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

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12/10/2010

MIC-Earlington Heights Connector Metrorail

Nodal Check at Member 9

MIC-Earlington Heights Connector Metrorail

Total Diaphragm Reinforcement

According to ACI 318 equation A-1 Fnn>Fun Where: Fun = Factored Design Force = 0.75 (Section 9.3.2.6) Fnn = Nominal Strength of a Node = fceAnz Further, f ce  0.85  n f 'c Where:  n  1.0 (Section A.5.2.2 – Nodes bounded by struts and bearing area) Therefore,

f ce  0.85  1.0  8500 psi  7225 psi (49.9 MPa) Multiply the allowable compressive stress on a face of a nodal zone by the area of concrete based on the geometry of the node. Fun = Factored Design Force = 1,879 k (8,359 kN) Anz  28.9 in  39.5 in  1142 in 2 (0.74 m 2 ) (Area of Bearing)

Fnn  0.75  7225 psi  1142 in 2 / 1 000  6188 k (27,525 kN)  1,879 k (8,359 kN)

ACI 2010, Chicago, IL

ACI 2010, Chicago, IL

MIC-Earlington Heights Connector Metrorail

MIC-Earlington Heights Connector Metrorail

Diaphragm Cracking

Summary • Strut-Tie Procedures can be Effectively Utilized for Diaphragm Design • Shear and Torsion Forces are Redirected into Support through the Diaphragm around the Access Opening • After Solving the Truss Forces, Ties can be Designed and Detailed • Struts and Nodes need to be Checked

ACI 2010, Chicago, IL

Daniel Kuchma holds a B.A.Sc., M.A.Sc., and Ph.D., all in civil engineering, from the University of Toronto. Since 1997, he has been an Associate Professor in the department of Civil and Environmental Engineering at the University of Illinois, and has taught courses in structural dynamics, statics, reinforced concrete, and prestressed concrete. His work includes a variety of consulting projects involving offshore structures, hydroelectric dams, towers, buildings and specialty structures. Dr. Kuchma is an active member of ACI, and the Federation International de Beton (fib). He received a National Science Foundation CAREER Award on “Tools and Research to Advance the Use of Strut-andTie Models in Education and Design.” He is also a National Center for Supercomputing Applications Faculty Fellow and University of Illinois Collins Scholar.

ACI 2010, Chicago, IL

Future of ACI STM Provisions and Guidelines Dan Kuchma

University of Illinois at Urbana-Champaign 90

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Location of STM Provisions in ACI318-14? 

Appendix A of ACI318-08



Location of Provisions in ACI318-14



Available Guideline Documents



Challenges to Design by the STM



ACI 445 Committee Document

Appendix A of ACI318-08: Basic Rules

P C A

C

c

f cu

C

>C

T

C

 As fy > T

P 2

T P 2

91

92

Appendix A of ACI318-08: Basic Rules

Appendix A of ACI318-08: Explanatory Materials

Design Strength of Struts = Fns where Fns = f ce  Area of Strut and f ce = 0.85 sfc s = 1.00 for prismatic struts in uncracked compression zones s = 0.40 for struts in tension members s = 0.75 when struts may be bottle shaped and crack control reinforcement* is included s = 0.60 when struts may be bottle shaped and crack control reinforcement* is not included s = 0.60 for all other cases

32 Figures

*crack control reinforcement requirement is vi si n i  0.003

Design Strength of Ties = Fnt where Fnt = Ast fy + Atp(f se + Δfp) Note that the tie reinforcement mu st be spread over a large enou gh area su ch that the tie force divided by the anchorage area (where the height is twice the distance from the edge of the region to the centroid of the reinforcement) is less than the limiting stress for that nodal zone. Design Strength of Each Nodal Zo ne Face = Fnn where F nn = f ce  Area on Face of Nodal Zo ne (perpendicular to the line of action of the associated strut or t ie force) Again fce = 0.85 nf c n = 1.00 in nodes bounded by struts and bearing areas n = 0.80 in nodes anchoring a tie in one direction only n = 0.60 in nodes anchoring a tie in more than one direction

93

Location of STM Provisions in ACI318-14? 

Separate appendix like in ACI318-08



Separate 318 referenced document



94

Available Guideline Documents 

Basic rules put into main body of code and “application guidelines” in a separate document

95

Design Examples 

SP-208



Second SP



Textbook Materials



Journal Papers



fib Bulletin 3

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Challenges to Design by the STM 

Selection of Shape of the STM Model



Determination of Member Forces in Indeterminate Models



Design for Multiple Load Cases



Uncertainty in Nodal Zones Dimensions



Time Consuming Geometric Calculations



Selecting What Needs to be Checked and Not Checked



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Performance under Overloads

Challenges to Design by the STM 

Selection of Shape of the STM Model

97

Challenges to Design by the STM 

98

Challenges to Design by the STM

Selection of Shape of the STM Model



Selection of Shape of the STM Model

99

100

Challenges to Design by the STM

Challenges to Design by the STM





Selection of Shape of the STM Model



Determination of Member Forces in Indeterminate Models



Design for Multiple Load Cases



Uncertainty in Nodal Zones Dimensions



Time Consuming Geometric Calculations



Selecting What Needs to be Checked and Not Checked



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Performance under Overloads

Selection of Shape of the STM Model

101

102

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Challenges to Design by the STM

Challenges to Design by the STM



Selection of Shape of the STM Model



Selection of Shape of the STM Model



Determination of Member Forces in Indeterminate Models



Determination of Member Forces in Indeterminate Models



Design for Multiple Load Cases



Uncertainty in Nodal Zones Dimensions



Time Consuming Geometric Calculations



Selecting What Needs to be Checked and Not Checked



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Performance under Overloads

5800 kN 535 mm

5625 kN

A

B

C L

K

2895 mm

D

O

M

Q

P

E

R

570 mm

41 T 36 k

U G

H

1590 1015 mm mm

I 2030 mm

3659 kN

N

F

4000 mm 3229.5 kN

S

J 1015 1350 mm mm

N

418.8 kN

49 degrees

103

104

Challenges to Design by the STM

Challenges to Design by the STM



Selection of Shape of the STM Model



Selection of Shape of the STM Model



Determination of Member Forces in Indeterminate Models



Determination of Member Forces in Indeterminate Models



Design for Multiple Load Cases



Design for Multiple Load Cases



Uncertainty in Nodal Zones Dimensions



Uncertainty in Nodal Zones Dimensions



Time Consuming Geometric Calculations



Time Consuming Geometric Calculations



Selecting What Needs to be Checked and Not Checked



Selecting What Needs to be Checked and Not Checked



Designing for Good Performance Under Service Loads



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Validity of Design in Complex Models



Performance under Overloads



Performance under Overloads

105

106

Challenges to Design by the STM

Challenges to Design by the STM



Designing for Good Performance Under Service Loads



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Validity of Design in Complex Models



Performance under Overloads



Performance under Overloads

107

108

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Challenges to Design by the STM

Challenges to Design by the STM



Designing for Good Performance Under Service Loads



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Validity of Design in Complex Models



Performance under Overloads



Performance under Overloads

109

110

Challenges to Design by the STM

Challenges to Design by the STM

45% of Pn

68% of Pn



Designing for Good Performance Under Service Loads



Designing for Good Performance Under Service Loads



Validity of Design in Complex Models



Validity of Design in Complex Models



Performance under Overloads



Performance under Overloads

111

Content of Potential ACI Committee 445 Document 

112

Click on the text below to go to the web page.

Selection of model shape 

Examples of good strut-and-tie model shapes for a large number of common design situations



Guidance for complex shapes



Use of predictions of stress trajectories and topology optimization



Selecting relative member stiffness in indeterminate situations



Design for multiple load cases and load reversals



Determination of nodal zone geometries



Determination of what to check and not to check



Evaluation of performance under service loads; minimum reinforcement recommendations



Validation of ACI code-calculated capacity



Other design requirements

Seminar Schedule

Online CEU Program

Bookstore

Web Sessions

ACI eLearning

Conventions

Concrete Knowledge Center

113

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