Abaqus Vibrations Tutorial

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©2009 Jayson Martinez & Hormoz Zareh 1 Portland State University, Mechanical Engineering Abaqus/CAE Vibrations Tutorial Problem Description The table frame, made of steel box sections, is fixed at the end of each leg. Determine the first 10 eigenvalues and natural frequencies. WARNING: There is no predefined system of units within Abaqus, so the user is responsible for ensuring that the correct values are specified. Here we use SI units

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Abaqus Vibrations Tutorial

Transcript of Abaqus Vibrations Tutorial

  • 2009JaysonMartinez&HormozZareh1PortlandStateUniversity,MechanicalEngineering

    Abaqus/CAEVibrationsTutorial

    ProblemDescription

    Thetableframe,madeofsteelboxsections,isfixedattheendofeachleg.Determinethefirst10eigenvaluesandnaturalfrequencies.

    WARNING:ThereisnopredefinedsystemofunitswithinAbaqus,sotheuserisresponsibleforensuringthatthecorrectvaluesarespecified.HereweuseSIunits

  • 2009JaysonMartinez&HormozZareh2PortlandStateUniversity,MechanicalEngineering

    AnalysisSteps1. StartAbaqusandchoosetocreateanewmodeldatabase2. InthemodeltreedoubleclickonthePartsnode(orrightclickonpartsandselectCreate)

    3. IntheCreatePartdialogbox(shownabove)namethepartand

    a. Select3Db. SelectDeformablec. SelectWired. Setapproximatesize=5(Notimportant,determinessizeofgridtodisplay)e. ClickContinuef. Createthesketchshownbelow

  • 2009JaysonMartinez&HormozZareh3PortlandStateUniversity,MechanicalEngineering

    4. InthetoolboxareaclickontheCreateDatumPlane:OffsetFromPrinciplePlaneicona. SelecttheXYPlaneandenteravalueof1fortheoffset

    5. InthetoolboxareaclickontheCreateWire:Planaricona. Clickontheoutlineofthedatumplanecreatedinthepreviousstepb. Selectanyoneofthelinestoappearverticalandontherightc. InthetoolboxareaclickontheProjectEdgesicond. SelectallofthelinesintheviewportandclickDone

    6. InthetoolboxareaclickontheCreateDatumPlane:3pointsicon(clickonthesmallblacktriangleinthebottomrightcorneroftheicontogetallofthedatumplaneoptions)

    a. Select3pointsonthetopofthegeometry

  • 2009JaysonMartinez&HormozZareh4PortlandStateUniversity,MechanicalEngineering

    7. InthetoolboxareaclickontheCreateWire:Planaricona. Clickontheoutlineofthedatumplanecreatedinthepreviousstepb. Selectanyoneofthelinestoappearverticalandontherightc. Sketchtwolinestoconnectfinishthewireframeofthetabled. ClickonDone

    8. DoubleclickontheMaterialsnodeinthemodeltree

    a. Namethenewmaterialandgiveitadescriptionb. ClickontheMechanicaltabElasticityElasticc. DefineYoungsModulus(210e9)andPoissonsRatio(0.25)

  • 2009JaysonMartinez&HormozZareh5PortlandStateUniversity,MechanicalEngineering

    d. ClickontheGeneraltabDensitye. Density=7800f. ClickOK

    9. DoubleclickontheProfilesnodeinthemodeltreea. NametheprofileandselectBoxfortheshapeb. ClickContinuec. Enterthevaluesfortheprofileshownbelowd. ClickOK

    10. DoubleclickontheSectionsnodeinthemodeltree

    a. NamethesectionBeamPropertiesandselectBeamforboththecategoryandthetypeb. ClickContinuec. LeavethesectionintegrationsettoDuringAnalysisd. Selecttheprofilecreatedabove(BoxProfile)e. Selectthematerialcreatedabove(Steel)f. ClickOK

  • 2009JaysonMartinez&HormozZareh6PortlandStateUniversity,MechanicalEngineering

    11. ExpandthePartsnodeinthemodeltree,expandthenodeofthepartjustcreated,anddoubleclickon

    SectionAssignmentsa. Selecttheentiregeometryintheviewportb. Selectthesectioncreatedabove(BeamProperties)c. ClickOK

    12. ExpandtheAssemblynodeinthemodeltreeandthendoubleclickonInstances

    a. SelectDependentfortheinstancetypeb. ClickOK

  • 2009JaysonMartinez&HormozZareh7PortlandStateUniversity,MechanicalEngineering

    13. DoubleclickontheStepsnodeinthemodeltreea. Namethestep,settheproceduretoLinearperturbation,andselectFrequencyb. ClickContinuec. Givethestepadescriptiond. SelectLanczosfortheEigensolvere. SelecttheradiobuttonValueunderNumberofeigenvaluesrequestedandenter10f. ClickOK

    14. DoubleclickontheBCsnodeinthemodeltreea. NametheboundaryconditionedFixedandselectSymmetry/Antisymmetry/Encastreforthetypeb. ClickContinuec. SelecttheendofeachlegandpressDoneinthepromptaread. SelectENCASTREfortheboundarycondition(ENCASTREmeanscompletelyfixed/clamped)e. ClickOK

  • 2009JaysonMartinez&HormozZareh8PortlandStateUniversity,MechanicalEngineering

    15. InthemodeltreedoubleclickonMeshfortheTableframepart,andinthetoolboxareaclickontheAssignElementTypeicon

    a. SelectStandardforelementtypeb. SelectLinearforgeometricorderc. SelectBeamforfamilyd. ClickOK

    16. InthetoolboxareaclickontheSeedParticona. Settheapproximateglobalsizeto0.1

    17. InthetoolboxareaclickontheMeshParticona. ClickYesinthepromptarea

  • 2009JaysonMartinez&HormozZareh9PortlandStateUniversity,MechanicalEngineering

    18. InthemenubarselectViewPartDisplayOptionsa. ChecktheRenderbeamprofilesoptionb. ClickOK

    19. ChangetheModuletoPropertya. ClickontheAssignBeamOrientationiconb. SelecttheportionsofthegeometrythatareperpendiculartotheZaxisc. ClickDoneinthepromptaread. Acceptthedefaultvalueoftheapproximaten1direction(0,0,1)e. ClickOKinthepromptarea

    f. SelecttheportionsofthegeometrythatareparalleltotheZaxis

  • 2009JaysonMartinez&HormozZareh10PortlandStateUniversity,MechanicalEngineering

    g. ClickDoneinthepromptareah. EnteravectorthatisperpendiculartotheZaxisfortheapproximaten1direction(i.e.0,1,0)

    i. ClickOKfollowedbyDoneinthepromptarea20. InthemodeltreedoubleclickontheJobnode

    j. NamethejobTableFramek. ClickContinuel. Givethejobadescriptionm. ClickOK

  • 2009JaysonMartinez&HormozZareh11PortlandStateUniversity,MechanicalEngineering

    21. Inthemodeltreerightclickonthejobjustcreated(TableFrame)andselectSubmitn. WhileAbaqusissolvingtheproblemrightclickonthejobsubmitted(TableFrame),andselectMonitor

    o. IntheMonitorwindowcheckthattherearenoerrorsorwarnings

    i. Ifthereareerrors,investigatethecause(s)beforeresolvingii. Iftherearewarnings,determineifthewarningsarerelevant,somewarningscanbesafely

    ignored

    22. Inthemodeltreerightclickonthesubmittedandsuccessfullycompletedjob(TableFrame),andselectResults

  • 2009JaysonMartinez&HormozZareh12PortlandStateUniversity,MechanicalEngineering

    23. InthemenubarclickonViewportViewportAnnotationsOptionsp. ThelocationsofviewportitemscanbespecifiedonthecorrespondingtabintheViewportAnnotations

    Optionsq. ClickOK

    24. Displaythedeformedcontouroverlaidwiththeundeformedgeometryr. Inthetoolboxareaclickonthefollowingicons

    iii. PlotContoursonDeformedShapeiv. AllowMultiplePlotStatesv. PlotUndeformedShape

    25. InthemenubarclickonResultsStep/Frames. ChangethemodebydoubleclickingintheFrameportionofthewindowt. Observetheeigenvaluesandfrequenciesu. Leavethedialogueboxopentobeabletoswitchthemodeshapeswhileanimating

  • 2009JaysonMartinez&HormozZareh13PortlandStateUniversity,MechanicalEngineering

    26. InthetoolboxareaclickonAnimationOptionsv. ChangetheModetoSwingw. ClickOKx. AnimatebyclickingonAnimate:ScaleFactoriconinthetoolboxarea

    27. ClickonadifferentFrameintheStep/Framedialogueboxtochangethemode28. ExpandtheTableFrame.odbnodeintheresulttree,expandtheHistoryOutputnode,andrightclickon

    Eigenfrequency:y. SelectSaveAsz. Name=Frequencies

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    aa. RepeatforEigenvaluebb. ObservetheXYDatanodesintheresulttree

    29. InthemenubarclickonReportXY

    cc. Selectfrom=AllXYdatadd. HighlightEigenvaluesee. ClickontheSetuptabff. ClickSelectandspecifythedesirednameandlocationofthereportgg. ClickApplyhh. ClickontheXYDatatabii. HighlightFrequenciesjj. ClickOK

  • 2009JaysonMartinez&HormozZareh15PortlandStateUniversity,MechanicalEngineering

    30. Openthereport(.rptfile)withanytexteditor

    Note:Eigenvaluesthatareidenticalindicatesimilarvibrationmodes,activatedindifferentplanes.