Бруяка В.А. - Инженерный анализ в Ansys Workbench. Учебное пособие. Часть 1 - 2010, страница 5

5.27:. 5.28,-:;.-–.;;.,206.2075.7.Element Shape (MECHANICALANSYSVMESH (-ANSYS.Part RelevanceSMRTSIZEPart Proximity (Number ofLESIZE.(Hex-dominant),.ID45,ANSYS(hex-to-tet).KREFINE, LREFINE,ESIZE.SMRTSIZE.-.ANSYS Workbench.1.?2.3.4.-..,,?5..ANSYSANSYSAnsys Workbench?-,6.-.:,,,,,-???)-Defaults??Statistics?208,,ANSYS,.Shape Checking ()SHPP, LSTET,ON.(SHPP, LSTET,ON)(Standard),.(SHPP, LSTET,OFF)(Aggressive),.Mapped Face Meshing (MSHKEY,1MSHAPE., SOL-,..(SHPP, OFF),)VSWEEP.)SMRTSIZE.ANSYS..Sizing (Element Size –Element Divisions –)ASIZE.Sphere of Influence ANSYSContact SizingAESIZE,RefinementAREFINE.Element SizeProximity and Curvature)209-7..6..Relevance Center.,Relevance.--.8.Sizing(?9..,.)-..10.11.«,?-Extrude.»,Workbench»«».:-.;.)Extrude..Refinement,.-,.13.«,(Sweep Method).12.Refinement.(bench»(.)Work.

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6.65.( . 6.66):Calculate Stress;Calculate Strain;Calculate Contact;Calculate Results At.. 6.66:(Stress),tact).(Strain),(Calculate Results At)(Con-,:All Time Points –Last Time Point –Equally Spaced Time Point –.;;-(Number Of Time Points).ANSYS,,. 6.65,1000.Line Search.:6.3.5.Analysis Data Management(();;,Solver Files Directory...248-249. 6.67).,Future Analysis-,Unit.-,( .: None)(. 6.68).(Solver Unit System)Manual.Solver Unit System.Prestressed analysis.Scratch Solver Files Directory,,,. 6.67.-Workbench. 6.1.-,-.Save ANSYS dbANSYS.,Mechanical APDL (ANSYS).Delete Unneeded FilesWorkbench“Yes”,.

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object –Bearing load –255Behavior –Bend –Body centroids –Body operation –Bolt pretension –Boolean –Both asymmetric –Both symmetric –Boundary –Box –CCalculate contact –Calculate results at –Calculate strain –Calculate stress –Cancel –Chamfer –Children –Circle –Circular –Clear selection –Coarse –Coincident –Collapse features –Components –Compression only support –Concentric –Concept –Cone –Constant –Constrain –Constraint equation –Constraints –,,Construction point –Construction point at intersection –Contact region –Contact sizing –)-Coordinate systems –Copies –Copy –Corner –Coupling –Create –Cross section –Current step number –Cursors –Curve –Cut –Cut material –Cycles –Cyclic –Cylinder –Cylindrical support –;,256(DDefaults –Define by –Defined –Definition –Deformable –;(),257…Delete –Delete unneeded files –Depth –Details –Details of “…” –Diameter –Dimensions –Ellipse –Environment –Equal distance –Equal length –Equal radius –Equally spaced time point –Evenly spaced –Expand –Export –Extend –Extend type –Extrude –,Direct solver –Direction –Direction –Direction vector –Displacement –Displacement convergence –Display names –Display values –Distance –Divisions –Drag –Draw –Dropped –Duplicate –,,FFace delete –Factor –Fast –Fill –Fillet –Fine –Fixed –,,,-,Fixed rotation –Fixed support –Fluid density –Fluid solid interface –EEdge delete –Edit –Elastic support –Element midside nodes –Element size –Elements –(Force –Force convergence –Free –Freeze –Frictionless support –258,259)Full assembly –Full circle –Function –Future analysis –Inertial –Initial size seed –Initial substeps –Initial time step –Integrated –Intersect –Inward thickness –GGeneral –Generalized plane strain –Generate mesh –Geometry –Geometry selection –Global coordinate system –Graph –()-KKept –,Graphics annotation –Grid –LLarge deflection –Last time point –Length –Length/distance –Line –Line body –Line by 2 tangents –Line from points –Line pressure –Line search –»IIgnore axis –Impedance boundary –Import –Imprint faces –,260,,-Loads –,Inertia relief –Iterative solver –JJoint load –,HHealing –Hide sketch –High –Horizontal –Hydrostatic pressure –,–,Look at –Loose –Low –261MMagnitude –Major grid spacing –Manual –Mapped face meshing –;Master geometry –Match control –Maximum substeps –Maximum time step –Medium –Mesh –Mesh control –Message –Method –Midpoint –Mid-surface –-,-Minimum edge length –Minimum reference –Minimum substeps –Minimum time step –Minor-steps per major –Mirror –Model –Modeling –Modify –Moment –Moment convergence –Move –NNamed selection –New section plane –No selection –Nodes –Nonlinear controls –Nonlinear solution –Normal to –Number of steps –Number of time points –…OOff –Offset –On –Operation –Orientation about principalaxis –Origin –Output controls –Outward thickness –,Oval –,262PParallel –Parallelepiped –Parents –Part –Paste –Paste handle –Path –(,263)Pattern –Perpendicular –Please define –Point –Polygon –Polyline –Preadjustment –Preload –Preserve –Pressure –Preview –Preview surface mesh –,Primitives –Principal axis –Print preview –Prism –Profile –Program controlled –Project –Pyramid –,Redo –Reference only –Refinement –Refresh –Relevance –Remote displacement –Remote force –Remove –Rename –Replicate –Report –Reset –Reversed –Revolve –Rigid –Rotate –Rotation –Rotation convergence –,,,,,,,()Rotational velocity –Ruler –QQuadrilaterals –SSave ANSYS db –,RRadial –Radius –Ratio –Rectangle –Rectangle by 3 points –Rectangular –,Scale –Scaling factor –Scope –Scoping method –ANSYS,(,Scratch solver files directory–264265)Section –Select multiple –Select new symmetry axis –Selection –Semi-automatic –Setting –Sew –Shape –Shape checking –Show dependencies –Solver units –Span –Sphere –Spline –Spline edit sphere –Split –Split at select –,,(,,,)Split edge into n equal segments –Split edges –Split edges at all points –Simplify –Simply supported –Sizing –Sketch instance –Sketching toolboxes –Skin/loft –Slave geometry –Slice –Slice by faces –Slice by plane –Slice by surface –Slice off edgesSlow –Smoothing –Snaps per minor –Solid –Solids –Solver controls –Solver files directory –Solver type –Solver unit system –nSplit edges at point –Springs stiffness –Springs stiffness factor –Standard earth gravity –Static structural –Statistics –Step control –Step end time –Substeps –Subtract –Supports –,,,266,-,Suppressed –Surface body –Sweep –Symmetry –,,267-Use global setting –TTabular –Tabular data –Tangent –Tangent line –Tangential –Thermal condition –Thickness –Through all –Time –Time step –Timestamp –Tolerance –Torus –Transformation –Transition –Translate –Tree outline –Triad –Triangles –Trim –Trim 1st –Trim both –Trim none –Type –(User define –,VValue –Vector –Velocity –Vertical –,Y)View advanced options –Visibility –WWeak springs –Wizard –,A, mA –kg, g, t, dat –m, cm, mm, m –N, dyne, N –s–V, mV –UUndo –,, , ,, ,,,,,,Unite –Update –Use advanced size function–268269)-1..,./.2..:, 1982.

– 448 ..., 2005. – 840 ..3..–:.1984. – 428 .4../..–:«5..». –.:, 1970. –.–.:.:,.–..:,6. – . 90-103../..–1975. – 541 .6.,., 1981. – 304 ..:7..,8./.,.–..–,....:.:, 1976. – 464 ..,:.., 1985. – 392 .../.–9.., 1979. – 392 .10..,., 1977. – 349 ././..–.:.–.:,ANSYS WorkbenchI...11. Clough R.W. The finite element method in plane stress analysis.

J. Struct. Div.,24.09.10ASCE, Proc. 2nd A.S.C.E. Conf. on Electronic Computation, Sept. 1960, p. 345-378.60 84 1/16.. . . 15,75. .50..12. Courant R. Variational Method for the Solution of Problems of Equilibrium andVibration. Bull. Amer. Math. Soc., 49, 1943, p. 1-43... . 15,72.137/1013. ANSYS Help.»443100, .443100, .270,.,, 244.., 244.2718.