Pushover Robot

PushOver Analysis 1. Start Robot Millennium

INITIAL DEFINITIONS 2. Open "PushOver ENG.rtd” file supplied together with testing path .

TRUSS MEMBERS

The novelty of 14.5 version is the possibility of using truss elements for other structure types than Truss 2D and Truss 3D. 3. Open the dialog box Advanced bar properties from the menu Geometry / Additional attributes. 4. Assign truss property to every bracing in the structure : In the open dialog box open the following options: truss bars – only axial forces act, other options inactive Introduce bracing numbers and bars: 7 to10 , 61 to 64 to the list of members field Confirm the definition with Apply button 5. Close the dialog box Adavanced bar properties.

LOAD CASES DEFINITION

The novelty is the possibility of self weight generation always on the entire structure i.e. after creating new bar or panel its number is automatically entered to the load list. 6. In the top tool bar unfold combo box Layouts and switch to the layout: Structure model >> Loads. 7. Switch to the dialog box: Load cases and define the self weight load: Load case 1 : In the combo box Nature select dead Enter self weight in the name field Press New button

FOR INTERNAL USE ONLY

DEFINITION OF PUSHOVER ANALYSIS CASES The novelty in the 14.5 version is the possibility of creating the case of PushOver analysis. This case allows to estimate the state of structure after earthquake basing on curve (being the result of the analysis) and on assigned code coefficients defining the seismic zone. 8. Open the window analysis types (top tool bar Analysis parameters icon or top menu : Analysis /Analysis types) 9. Define Modal case : Click Define a new case button In the window: New case definition set analysis type: Modal and confirm by clicking OK In the window Modal Analysis parameters leave default settings Confirm by clicking OK button 10. Define cases of the Push Over analysis : PushOver 1 Click Define a new case button In the window New case definition set the analysis type : PushOver and confirm by clicking OK button In the new open window PushOver set the following parameters: Name of the case : PushOver 1 Node number : 3 direction : UX+ method of load definition : according to unit acceleration in the given direction maximum displacement : 8 [in] using Parameters button open Non-linear Analysis Algorithm options window and set the following: number of load increment : 20 click Save settings in preferences button - which means that the modification of Arclength method parameters will relate to consecutive PushOver cases Confirm parameters modification by clicking OK confirm PushOver case analysis by clicking OK The case of the PushOver analysis is used for defining the curve : sum of reactions vs control displacement of the node. Above mentioned parameters indicate that the curve will be defined for the node 3 on the global direction UX. At the same time, load increment for this case will be performed until the UX displacement of the node 3 exceeds 8 [in], then, the analysis will stop. The analysis can be interrupted before, for ex. if there's no convergence because of an exceeding load. PushOver 2 click Define new case button in the window: New case definition set the analysis type : PushOver and confirm by clicking OK button in the new open window: PushOver set the following parameters: name of the case : PushOver 2 node number : 27 direction : UY+ maximum displacement : 12 [in] method of load definition : according to unit acceleration in the given direction select Non-linear analysis option confirm by clicking OK button close the window: analysis types

FOR INTERNAL USE ONLY

DEFINIITION OF ADDED MASSES FOR THE MODAL ANALYSIS EXAMPLE 11. From the Cases combo-box (upper toolbar), select the modal case, it means the case number 2 From the right toolbar, open the Loads Definition dialog box and on the Node tab select the Added masses icon: introduce the masses : mX = 22 [kip] mY = 22 [kip] mZ = 22 [kip] accept the definition by pressing the Add button apply the masses to all the nodes in the structure to the Apply to edition field enter the numbers of all the nodes or enter the all command accept by pressing the Apply button 12. Close the loads definition dialog box.

DEFINITION OF NON LINEAR HINGES Non linear hinges, used in the PushOver analysis, are applied to bars in order to model non-linear structure character. Those hinges can describe elasticity, plasticity and structural stability.

13. In the upper tool bar unfold combo-box Layouts and switch to the layout: Structure model >> Start. 14. From the text menu open the dialog box for non-linear hinges definition – Geometry / Additional attributes / Non-linear hinges. 15. Define the following non-linear hinge: In the dialog box Non-linear hinges enter the definition of a new hinge by selecting the icon: New hinge type on the tool bar. In the Label field enter: Hinge_1 Open the dialog box for Definition of non-linear hinge model with an appropriate button and define the following model: Model_MY Non-linear hinges models are not related to a concrete hinge. Each model can be used for any hinge definition. PushOver curves tab In the field: Model name enter: Model_MY Create new model by clicking Add button New model will appear in the list in the bottom part of the Functions tab. Definition / modification of models parameters is possible after selecting from the list (selected model is marked with an arrow) and switching to the Points and Parameters tab. Points tab

FOR INTERNAL USE ONLY

Enter the following points while Symmetry option is selected: point B: X=0.01 ; Y=37 point C: X=0.05 ; Y=45 point D: X=0.05 ; Y=8 point E: X=0.09 ; Y=8 Symmetry option allows a fast definition of "symmetrical" models i.e. curve - types on the negative semi-axis is equal to the curve-type on the positive semi-axis as concerns the absolute value. Parameters tab Select model type: moment-rotation and enter the following parameters: Acceptance criteria for positive semi-axis : Immediate occupancy (IO) : 0.01 Life safety (LS): 0.03 Structural Stability (SS) :0.05 If the Symmetry option is checked on the tab, values for the positive semi-axis will be automatically updated. Set the unloading method : elastic Confirm the definition of non-linear hinge model by clicking OK button In the dialog box: Non-linear hinge definition check the MY box and in the appropriate combobox select previously defined hinge model. Confirm the definition with Add button Close the dialog box with appropriate button 16. Apply so defined hinge to selected structure bars by the following method: In the dialog box: Non-linear hinges check the label: Hinge_1 : In the field Coordinate enter x=0.1 ( relatively [x/l] ) Enter numbers of bottom columns and beams from planes: Y1, Y2 and X2 to the field: Current selection i.e. the following selections: Columns : 1, 3, 49, 51, 55, 57-> confirm by clicking Apply button Beams: 53, 54, 65to72 -> confirm by clicking Apply button Then enter x=0.9 ( relatively [x/l] ) in the field: Coordinate Enter numbers of beams situated on the planes Y1, Y2 and X2 into the field Current selection (i.e. beams: 53, 54, 65to72) For this purpose, select Previous selection option on the graphic view from the context menu and move the mouse cursor back to the Current selection field, numbers of selected beams will appear in the edit field Confirm the definition with Apply button The novelty of the 14.5 version the possibility of returning to the previous selection. This option is very useful when we want to perform several different operations for a group of objects. In that case we can easily repeat the selection without selecting objects once again. Close the non-linear hinges dialog box by clicking appropriate button. RESULTS 17. Start calculations from the top tool bar by clicking the icon: Start calculations.. 18. Unfold Screens combo-box in the top tool bar and switch to the Results >> Results screen. 19. Unfold Case selection combo-box in the top tool bar and select the case 3 : PushOver1 20. In the Diagrams dialog box activate the display of Deformations and Moments MY in the new window: Click MY check-box (NTM tab ) Click Deformation check-box (Deformation tab) Click check-box: Open new window and confirm the selection by clicking Apply button Start the window: Case component from the top tool bar (Component selection icon next to the Cases combo-box or text menu : Loads /Select case component) Using slider or the field: Current component display consecutive steps (load increment) of the PushOver1 case. 21. Close the view in the new window.

FOR INTERNAL USE ONLY

RESULTS – DIAGRAMS OF PUSHOVER ANALYSIS 22. Open the window for definition of PushOver analysis diagrams - text menu : Results / Advanced / PushOver Analysis - Diagrams. 23. Click Add button and create the following diagram in the new open window: Displacement UX On the Nodes tab click UX check-box In the Case combo-box select 3: PushOver1 In the Point field enter : Node : 3 Confirm the definition by clicking Add button 24. Close Diagram definition window. 25. Display the diagram in the new window : Move the diagram to the right panel: Presented diagrams using >> button. Click Open new window check-box and click Apply button Move the bar separating tabular part from diagram window down to 1/4 of the screen height Re-scale the diagram to the whole screen (Zoom All icon from top tool bar or context menu : Zoom / Zoom All) Display of main grid lines inactive – select Diagrams Properties / Display main grid lines from the context menu Activate additional information about displayed diagrams – select Table columns option from the context menu and click all check-box, then close the window by clicking OK button 26. Make a screen capture called « UX Displacement – PushOver 1 » 27. Close the diagram window and the dialog-box for the definition of PushOver analysis diagrams. RESULTS – CURVE This option allows to display curves for cases of PushOver analysis. Curves are created for the node designed as control node in the PushOver analysis. The curve is the diagram of reaction sum in the function of node displacement in the selected/control direction.. 28. Open the window for curve definition - text menu : Results /Advanced / Capacity Curve. 29. Display the following diagrams: Displacement – reactions sum On the top toolbar unfold Case selection combo box and select case 3: PushOver1 In the diagram type field select : Displacement - reaction sum click open new window check-box click Apply button Capacity spectrum In the diagram type field select: Capacity spectrum and click Apply button After selecting this option Displacements-Reactions sum diagram will be transformed to ADRS format (Acceleration-Displacement Response Spectrum). Define parameters of structure damping : Viscous damping : 0.05 Select structure type (histeretic damping): B Define demand spectrum and display lines of the constant period and reduced spectrum grid : Seismic coefficient Ca : 0.4 Seismic coefficient Cv : 0.4 Activate the display of constant period lines : 0.5 [s]; 0.8 [s]; 2 [s] Activate reduced spectrum grid 0.05 ; 0.1 ; 0.2 Activate the displaying of the selected demand spectrum click open new window check-box click Apply button increase seismic coefficients Ca and Cv to 0.6 in the dialog-box, press Apply button and check new performance point close the Push Over diagrams spliter viewer FOR INTERNAL USE ONLY

unfold Case selection combo-box in the top toolbar : select case 4 : PushOver2 in the Push Over curves activate the displaying of the selected demand spectrum click open new window check-box press the Apply button and verify the performance point modify the parameters of structure damping by selecting structure type C, click Apply button and check its influence on performance point situation 30. Close the diagram window and the dialog for curve display 31. Save the file under any name.

FOR INTERNAL USE ONLY