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  • FINITE ELEMENT ANALYSIS IN ABAQUS Siddhartha Ghosh* and Swapnil B. Kharmale** * Assistant Professor, ** Research Scholar (PhD Student ) Department of Civil Engineering Indian Institute of Technology, Bombay
  • ABAQUS : GeneralABAQUS is a highly sophisticated, general purpose finite element program,designed primarily to model the behavior of solids and structures underexternally applied loading. Salient features of ABAQUS Capabilities for both static and dynamic problems The ability to account all types of nonlinearities viz. material non-linearityand geometric non-linearity A very extensive element library, including a full set of continuum elements,beam elements, shell and plate elements A sophisticated capability to model contact between solids Capabilities to model a number of phenomena of interest, includingvibrations, coupled fluid/structure interactions, acoustics, buckling problems,and so on. (From:www.abaqus.comand and www.engin.brown.edu/courses/en www.engin.brown.edu/courses/en175/abaqustut/abaqustut)
  • ABAQUS : GeneralThe ABAQUS suite consists of three core products: ABAQUS/Standard,For traditional implicit finite element analyses such as static, dynamics,thermal, all powered with the widest range of contact and nonlinear materialoptions ABAQUS/ExplicitFor transient dynamics and quasi-static analyses using an explicit approach staticappropriate in many applications such as drop test, crushing and manymanufacturing processes. and ABAQUS/CAE (Complete Abaqus Environment) nvironment)It provides a complete modelling and visualization environment for ABAQUSanalysis products. It has direct access to CAD models, advanced meshingand visualization
  • ABAQUS : GeneralHere we focus on ABAQUS/Standard Solver Structure Command Line ABAQUS CAE ABAQUS STANDARDNow we will model and analysis a single story Steel Plate Shear Wall (SPSW1) throughABAQUS/CAE(Note that it could be possible to create the model through command line which will bediscussed later)
  • ABAQUS/CAE LayoutYou can start ABAQUS CAE from the START menu or with a command line by typingabaqus cae in a Command window. Following figure shows how an ABAQUS/CAE looks Title bar Menu bar Tool bar Context bar View port Canvas & Drawing Toolbox area Area Prompt area Message area
  • ABAQUS CAE modulesI)PREPROCESSING Part Create individual parts Property Create and assign material properties Assembly Create and place all parts instances Step Define all analysis steps and the results you want Interaction Define any contact information Load- Define and place all loads and boundary conditions Mesh Define your nodes and elementsII)ANALYSIS Job Submit your job for analysisIII)POSTPROCESSING Visualization- View your results
  • 3-Dimensional FEM Problem Dimensional (Pushover Analysis of SPSW) To start learning ABAQUS CAE we will work through modelling asingle story Steel Plate Shear Wall (SPSW1) specimen whichincludes geometric nonlinearity (initial out-of-plane deformationsduring fabrication). The specimen is subjected to monotonic lateralload (Non-linear static pushover analysis) Problem StatementTo find the ultimate load carrying capacity (Lateral load) of singlestory steel plate shear wall (SPSW by non-linear static push over (SPSW1)analysis.
  • Details of SPSW SPSW1
  • Lateral Force- Deformation Behavior of SPSW
  • Selection of Element for Modelling SPSW SPSW1Infill Panel By using 3-Dimensional ShellElementBoundary Element By using 3-Dimensional Beam Element
  • PART MODULE Create a new part as Infill_Panel 3-D planar Type : Deformable Basic feature: shell Approximate size: 6x6 (Note :- ABAQUS follows consistent unit so be specific to keep same unit. Here we kept SI units i.e. m for length N for force etc)
  • Part:- Infill_PanelThe following picture shows how a Part Infill_Panel look
  • Create another new part as Boundary_Element 3-D planar Type : Deformable Part:Boundary_Element Boundary_Element Basic feature: wire Approximate size: 6 x6
  • Infill_Panel and Boundary_Element Parts in ABAQUS/CAE
  • Property ModuleWe will add the material Steel and give it values E= 2.0E+11N/m2 Poissons ratio = 0.3, YieldStress = 2.0E+08N/m2,Plastic strain=0 (Note that elastically-perfectly plastic relationship is used forsteel)We will create section called Shellsection and give it category of Shell ,ContinuousShell/Homogenous and assign a thickness of 0.0025 with thickness integration point 5 0025mAssign material to this section
  • Property Module (Continued) Also create section called Boundarysection_col and Boundarysection_bea and give it category of Beam Create profile namely Columns and Beams using I- shaped cross section Assign same material to this section also Boundarysection_colI-Section profile for Columns I-Section profile for Beams Section
  • Property Module (Continued) Assign Shellsection to part named Infill_Panel Assign Boundarysection_col and Boundarysection_bea with Columns and Beams profile to part named Bounary_Element Assembly Module Now we will create two independent instances usingparts Infill_Panel and Boundary_Element Its easy to mesh the assembly as a whole usingindependent instances
  • Step ModuleBy default there is a Initial Step in Abaqus (i.e. System made step) which is used to define the .Boundary ConditionsWe will add a step after system made initial step called Transverse loadThe procedure type is General and type is Static. The nlgeom=Yes means geometricnonlinearity is on to account for large deformationsKeep the Output Request as preselected (By Default)
  • Step Module (Continued)After step called Transverse Load create a next analysis step Lateral LoadThe procedure type is General and type is Static Riks . Again nlgeom=Yes meansgeometric nonlineaarity is on to account for large deformations
  • Interaction Module In this module we will define the contact between two independent part namely Infill_Paneland Boundary_ElementCreate surface Infill_Panel_Master in part Infill_Panel
  • Similarly create surface Boundary_Element_Slave in part Boundary_Element Once these surfaces are created we can provide contact between them throughInteraction module Selection of Master surface
  • Selection of Slave surface
  • Interaction between two parts namely Infill_Panel and Boundary_Element
  • Creating Boundary Conditions in Initial StepCreate boundary conditions in Initial step (System made step)There are two type of Boundary conditions for this problem namelyBottom extreme nodes are fixed (U1=U2=U3 3=UR1=UR2=UR3=0)Edges are restrained in z-direction (U3=0)
  • Bottom extreme nodes are fixed (U1=U =U2=U3=UR1=UR2=UR3=0 i.e. Encastre)
  • Edges are restrained in z z-direction (U3=0)
  • Mesh ModuleNow we will mesh the assemblyBefore that we will assign the shell element to Infill_Panel part. The shell element is S4RAlso assign the beam element to Boundary_Element part. The beam element is B31
  • Assigning S4R Element to Infill_Panel part R
  • Assigning B31 Element to Boundary_Element part
  • Mesh Module (Continued) After assigning proper element to each of part next step is seeding. Here we are using mesh of 20x20 for Infill_Panel part and we will discritize each boundaryelement into 20 parts. So for whole assembly mesh density will be 20x20.
  • Meshing of whole Assembly of SPSW SPSW1
  • Load ModuleSTEP:- Transverse Load :- Apply a concentrated load (named as CFORCE-1)of 2N at middlenode in negative z-direction (i.e. Along 3-axis)
  • Load Module (Continue) STEP:- Lateral Load :- Apply a concentrated load (named as CFORCE-2)of 1000N at theTOPNODES in positive x-direction (i.e. Along 1-axis). axis). Remember here we kept the displacement contro thus load magnitude mentioned above is used trolas load control during initial part of analysis
  • Job ModuleWe will create a job called SPSW1Once this has been created just submit the job.The analysis should only take a couple of minutes.
  • Here you have an option toselect analysis viz Fullanalysis or Explicit analysisor RestartSubmitting job after elapsedtime
  • Visualization Module (Post processing) Once your analysis is complete we want to see the results. First we will see the deformed shape of SPSW1 in Step Transverse Load. (Remember this step is created to have initial out plane deformation (due to fabrications). So the out-of deformed shape is somewhat similar to buckling of plate )
  • Visualization Module (Continued)