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- Page 11 and 12: 1.3 Result Definitions CHAPTER 1 In
- Page 13 and 14: Plot Type Description CHAPTER 1 Int
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- Page 17 and 18: Other Definitions Term Definition P
- Page 19 and 20: 1.4 Capabilities and Limitations CH
- Page 21 and 22: Create CHAPTER 1 Introduction to Re
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- Page 29 and 30: Use Templates CHAPTER 1 Introductio
- Page 31 and 32: Post/Unpost CHAPTER 1 Introduction
- Page 33 and 34: Delete Two items may be deleted: Pl
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- Page 37 and 38: 1.6 Results Title Editor CHAPTER 1
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- Page 43 and 44: END FUNCTION CHAPTER 1 Introduction
- Page 45 and 46: END SWITCH DEFAULT SWITCH( var ) CA
- Page 47 and 48: MSC.Patran Reference Manual, Part 6
- Page 49 and 50: CHAPTER 2 Quick Plots No modificati
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- Page 55 and 56: Create only a Deformation Plot 1. F
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Create a Maximum Fringe from Multip
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4. Turn the Animate Fringe toggle O
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MSC.Patran Reference Manual, Part 6
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6. If animation is desired, turn th
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CHAPTER 3 Deformation Plots In addi
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Attribute Description CHAPTER 3 Def
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Option Description Save Deformation
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5. Change the Animate By option pul
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Mask Out Deformation Components 1.
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Z Y X Figure 3-6 Two Deformation Pl
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Z Total Deformation (all components
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MSC.Patran Reference Manual, Part 6
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6. Optionally select the target ent
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In addition to targeting the above
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Attribute Description Display (Edge
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CHAPTER 4 Fringe Plots Averaging Me
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Animate a Static Fringe Plot 1. Fro
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Display a Transient Fringe Animatio
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Display Multiple Animations in the
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MSC.Patran Reference Manual, Part 6
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5. After performing steps 1-4 you h
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5.3 Display Attributes CHAPTER 5 Co
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5.4 Plot Options CHAPTER 5 Contour
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5.5 Contour Plot Example CHAPTER 5
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Create a Contour plot with contour
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MSC.Patran Reference Manual, Part 6
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CHAPTER 6 Marker Plots For both Mod
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6.2 Target Entities CHAPTER 6 Marke
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6.3 Display Attributes CHAPTER 6 Ma
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Table 6-3 Vector Display Attributes
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6.4 Plot Options CHAPTER 6 Marker P
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6.5 Examples of Usage CHAPTER 6 Mar
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Create a Tensor Plot of Principal S
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Put a Scalar, Vector or Tensor on a
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4. Repeat this process for as many
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MSC.Patran Reference Manual, Part 6
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Method Scalar cursor plots display
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CHAPTER 7 Cursor Plots 7. Optionall
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Cursor Report Setup CHAPTER 7 Curso
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Cursor Report Format. Below are des
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CHAPTER 7 Cursor Plots %Em.n.p% Exp
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$GV: The name and value of an assoc
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7.2 Target Entities CHAPTER 7 Curso
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7.4 Plot Options CHAPTER 7 Cursor P
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7.5 Examples of Usage CHAPTER 7 Cur
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5. Press the Apply button. 6. Once
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5. Press the Apply button. Apply Fi
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MSC.Patran Reference Manual, Part 6
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5. For Result Y-axis values, option
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8.2 Target Entities CHAPTER 8 Graph
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Attribute Description CHAPTER 8 Gra
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Attribute Description CHAPTER 8 Gra
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Option Description Extrapolation Me
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Graph of Results Versus Results (No
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Add Curve to Existing Graph 1. Foll
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Graph of Beam or Edge Results The m
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Save a Graph Plot Modify a Plot Dis
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MSC.Patran Reference Manual, Part 6
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CHAPTER 9 Animation Animation optio
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CHAPTER 9 Animation Animation Inter
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9.4 Animating Existing Plots CHAPTE
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9.5 Examples of Usage CHAPTER 9 Ani
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MSC.Patran Reference Manual, Part 6
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6. At this point you could press th
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The following quantities are also r
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CHAPTER 10 Reports In addition to s
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CHAPTER 10 Reports Edit This is an
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Table 10-2 Value Format Strings for
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Table 10-3 Value Format Strings for
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Option Description Extrapolation Me
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Report of Transient Displacement Da
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Create a MSC.Patran .nod Formatted
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TITLE 810 1468 -2.524668e-03 257 3
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11. Turn Pagination OFF. 12. Make t
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CHAPTER 10 Reports View Global Vari
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MSC.Patran Reference Manual, Part 6
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11.2 Combined Results CHAPTER 11 Cr
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11.3 Derived Results CHAPTER 11 Cre
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Average/Sum. Once the Apply button
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For tensor results you have the cho
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CHAPTER 11 Create Results User Defi
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CHAPTER 11 Create Results Result Op
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11.5 Examples of Usage CHAPTER 11 C
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7. Select all the layers from which
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Z Y X Z Y X Z Y X Figure 11-3 Avera
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MSC.Patran Reference Manual, Part 6
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6. Select target entities. That is,
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CHAPTER 12 Freebody Plots 1. The MS
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CHAPTER 12 Freebody Plots Freebody
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CHAPTER 12 Freebody Plots Press App
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Entity Description CHAPTER 12 Freeb
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Attribute Description CHAPTER 12 Fr
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12.5 Create Loads or Boundary Condi
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12.6 Tabular Display The Show Sprea
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12.7 Examples of Usage CHAPTER 12 F
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107.08 Display a Freebody Diagram 3
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Create a Load Case Set for Use in a
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Create a Forced Displacement Bounda
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MSC.Patran Reference Manual, Part 6
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CHAPTER 13 Insight Isosurfaces are
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Tool Targets. Insight tools may be
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Capabilities and Limitations Insigh
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CHAPTER 13 Insight Selecting and ma
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Create Select Create from the Actio
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Delete Select Delete from the Actio
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Animation Attributes CHAPTER 13 Ins
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Result Options Form This subordinat
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Isosurface Coordinate Selection The
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Isosurface Attributes None Display
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Streamsurface Attributes Select a c
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Fringe Attributes Turns ON/OFF the
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Tensor Attributes A default name fo
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Marker Attributes Select a color fo
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Insight Control The Insight Control
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Isosurface Control CHAPTER 13 Insig
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Animation Control The following for
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Animation Setup Animation Mode: Ani
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Cursor Results CHAPTER 13 Insight T
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1 Cursor Results File Format CHAPTE
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Insight Spectrum The following form
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MSC.Patran Reference Manual, Part 6
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14.2 Result Case(s) and Definitions
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CHAPTER 14 Numerical Methods You ca
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CHAPTER 14 Numerical Methods Result
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Below are the equations and example
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From the von Mises example above th
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Tresca Shear Stress. Tresca shear s
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CHAPTER 14 Numerical Methods Below
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Table 14-1 Averaging at Nodes from
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Element Node Table 14-2 Averaging a
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14.5 Extrapolation CHAPTER 14 Numer
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CHAPTER 14 Numerical Methods Exampl
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CHAPTER 14 Numerical Methods Exampl
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14.6 Coordinate Systems CHAPTER 14
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CHAPTER 14 Numerical Methods Projec
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Figure 14-6 CQUAD4 Bisector Coordin
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CHAPTER 14 Numerical Methods MSC.Na
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MSC.Patran Reference Manual, Part 6
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Problem 5: Linear Statics, 2D Shell
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Problem 26: Complex Modes, Direct M
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CHAPTER 15 Verification and Validat
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X-Translation Figure 15-3 X-Transla
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CHAPTER 15 Verification and Validat
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CHAPTER 15 Verification and Validat
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XY Stress - Layer 1 Figure 15-10 Cr
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XX Stress - Layer 3 Figure 15-14 Cr
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Problem 3: Linear Statics, Principa
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Stress at b: σ( 10, 5.5) τxy( 10,
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Table 15-10 Stresses* at Position a
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Zero Shear Angle XY Stress Figure 1
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Point a’ Stress Tensor Point b’
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Engineering Data: E=1000. psi v = 0
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Table 15-16 Stresses, CHAPTER 15 Ve
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Radial Stresses Figure 15-30 Fringe
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CHAPTER 15 Verification and Validat
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Global X Displacements Global Y Dis
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Circumerential Stresses Figure 15-3
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σ 3 qb 2 a 2 r 2 - ( - ) r 2 a 2 b
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File(s):/results_vv_files/prob006.b
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Radial Stresses 3 Noded CTRIAX ELem
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Axial Stresses 3 Noded CTRIAX Eleme
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CHAPTER 15 Verification and Validat
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Applied Loads and BCs Radial Displa
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Hoop Stresses Axial Stresses Figure
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Element Forces: P i = EA ------- ×
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X Displacements Figure 15-56 X Tran
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Problem 9: Nonlinear Statics, Large
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CQUAD8 Model with Loads and BCs Fig
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Problem 10: Linear Statics, Thermal
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HEX8 HEX20 WEDGE6 Figure 15-64 Mode
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Problem 11: Superposition of Linear
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CHAPTER 15 Verification and Validat
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Subcase A Vertical Displacement Fig
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Radial Stress Subcase B Hoop Stress
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Hoop Stresses Subcase C Figure 15-7
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Problem 12: Nonlinear Statics, Post
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CHAPTER 15 Verification and Validat
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Rotational Displacement Tip Transla
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CHAPTER 15 Verification and Validat
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CHAPTER 15 Verification and Validat
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CHAPTER 15 Verification and Validat
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Mode 1, Freq=0.6955 Hz Mode 2, Freq
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CHAPTER 15 Verification and Validat
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Basic Model Figure 15-8 Basic Circu
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Mode i=0, j=1, Freq. =4238.1 Hz Mod
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CHAPTER 15 Verification and Validat
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MODE i=1, j=0, Freq.=2037.8 Hz MODE
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MODE i=0, j=2, Freq.=11178 Hz Figur
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CHAPTER 15 Verification and Validat
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Problem 18: Buckling, Flat Plates S
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First Buckling Mode Figure 15-25 Bu
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CHAPTER 15 Verification and Validat
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Figure 15-28 Displacement Responses
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Engineering Data: Table 15-9 Bar Pr
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Basic Model of Truss with Boundary
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Figure 15-35 Stress Responses at Se
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CHAPTER 15 Verification and Validat
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Figure 15-37 Stress History Plot at
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Problem 22: Direct Nonlinear Transi
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CHAPTER 15 Verification and Validat
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Figure 15-42 Rod End and Mass Displ
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The resonant amplitude is then give
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Figure 15-45 Amplitude Displacement
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Substituting the assumed engineerin
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Figure 15-46 Model of Beam with Sus
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Figure 15-50 Acceleration Responses
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CHAPTER 15 Verification and Validat
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Problem 26: Complex Modes, Direct M
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This gives an estimated damped freq
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Mode 2 Freq = 4.776E-12 Hz Figure 1
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CHAPTER 15 Verification and Validat
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Basic Model with Applied Temperatur
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Problem 28: Transient Heat Transfer
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Basic Model with Convection Conditi
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Problem 29: Steady State Heat Trans
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Basic Model with Convection Conditi
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Basic Model with Loads and BCs Figu
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Freebody Force Bar 4 Figure 15-70 F
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I N D E X MSC.Patran Reference Manu
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numerical forms, 295 O octahedral s