HyperView supports Nastran FEMZIP, OP2 and XDB result file formats.
Data types supported from Nastran OP2 files include:
Data Name |
Result Type |
Data Type |
---|---|---|
1D Element (Forces / Moments)* |
ELEMENT |
VECTOR |
Acceleration (Translation / Rotation) |
NODE |
VECTOR |
Applied (Forces / Moments) |
NODE |
VECTOR |
Contact (Force / Moment / Traction) |
NODE |
VECTOR |
Displacement |
NODE |
VECTOR |
Element (Fluxes / Gradients) |
ELEMENT |
VECTOR |
Grid Point Element (Forces / Moments)** |
ELEMENT |
VECTOR |
MPC (Forces / Moments) |
NODE |
VECTOR |
Rotation |
NODE |
VECTOR |
SPC (Forces / Moment) |
NODE |
VECTOR |
Summed (Forces / Moments) |
NODE |
VECTOR |
Velocity (Translation / Rotation) |
NODE |
VECTOR |
2D Element (Forces / Moments)*** |
ELEMENT |
TENSOR3-D |TENSOR2-D |
Composite (Stress / Strain) |
ELEMENT |
TENSOR3-D |TENSOR2-D |
Grid Point Stresses |
NODE |
TENSOR3-D |TENSOR2-D |
Nonlinear Strain |
ELEMENT |
TENSOR3-D |TENSOR2-D |
C |
ELEMENT |
TENSOR3-D |TENSOR2-D |
PSD Stress |
ELEMENT |
TENSOR3-D |TENSOR2-D |
RMS Stress |
ELEMENT |
TENSOR3-D |TENSOR2-D |
Strain |
ELEMENT |
TENSOR3-D |TENSOR2-D |
Stress |
ELEMENT |
TENSOR3-D |TENSOR2-D |
1D Force:CROD Axial Force CROD Torque CBAR Bending Moment (A1 / A2) CBAR Bending Moment (B1 / B2) CBAR Shear1 CBAR Shear2 CBAR Axial Force CBAR Torque CBEAM Bending Moment (Plane1 A / Plane2 A) CBEAM Bending Moment (Plane1 B / Plane2 B) CBEAM Web Shear (Plane1 A / Plane2 A) CBEAM Web Shear (Plane1 B / Plane2 B) CBEAM Axial Force (A / B) CBEAM Total Torque (A / B) CBEAM Warping Torque (A / B) CBUSH Force (x / y / z) CBUSH Moment (x / y / z) CELAS1 Force CELAS2 Force CGAP Normal x CGAP Shear (v / w / y / z) CGAP Axial u CGAP Slip (v / w) CWELD Bending Moment (Plane1 A / Plane2 A) CWELD Bending Moment (Plane1 B / Plane2 B) CWELD Shear (Plane1 / Plane2) CWELD Axial Force CWELD Torque |
ELEMENT |
SCALAR |
1D Nonlinear StressCBEAM Equivalent Stress at Point (C1 / C2) CBEAM Equivalent Stress at Point (D1 / D2) CBEAM Equivalent Stress at Point (E1 / E2) CBEAM Equivalent Stress at Point (F1 / F2) CBEAM Long Stress at Point (C1 / C2) CBEAM Long Stress at Point (D1 / D2) CBEAM Long Stress at Point (E1 / E2) CBEAM Long Stress at Point (F1 / F2) |
ELEMENT |
SCALAR |
1D Nonlinear StrainCBEAM Effective Creep Strain at Point (C1 / C2) CBEAM Effective Creep Strain at Point (D1 / D2) CBEAM Effective Creep Strain at Point (E1 / E2) CBEAM Effective Creep Strain at Point (F1 / F2) CBEAM Effective Plastic Strain at Point (C1 / C2) CBEAM Effective Plastic Strain at Point (D1 / D2) CBEAM Effective Plastic Strain at Point (E1 / E2) CBEAM Effective Plastic Strain at Point (F1 / F2) CBEAM Total Strain at Point (C1 / C2) CBEAM Total Strain at Point (D1 / D2) CBEAM Total Strain at Point (E1 / E2) CBEAM Total Strain at Point (F1 / F2) |
ELEMENT |
SCALAR |
1D StrainCBAR Axial CBAR (SA1 / SA2 / SA3 / SA4) CBAR SA (Maximum / Minimum) CBAR Safety Margin (Compression / Tension) CBAR (SB1 / SB2 / SB3 / SB4) CBAR SB (Maximum / Minimum) CBEAM Long Strain at Point (C1 / C2) CBEAM Long Strain at Point (D1 / D2) CBEAM Long Strain at Point (E1 / E2) CBEAM Long Strain at Point (F1 / F2) CBEAM Margin of Safety (Compression1 / Compression2) CBEAM Margin of Safety (Tension1 / Tension2) CBEAM Maximum (Strain1 / Strain2) CBEAM Minimum (Strain1 / Strain2) CELAS Strain CROD Axial (Strain / Safety Margin) CROD Torsional (Strain / Safety Margin) CWELD Axial Strain CWELD Max Shear Strain CWELD Max (Strain A / Strain B) CWELD Min (Strain A / Strain B) |
ELEMENT |
SCALAR |
1D StressCBAR Axial CBAR (SA1 / SA2, SA3, SA4) CBAR SA (Maximum / Minimum) CBAR Safety Margin (Compression / Tension) CBAR (SB1 / SB2 / SB3 / SB4) CBAR SB (Maximum / Minimum) CBEAM Long Stress at Point (C1 / C2) CBEAM Long Stress at Point (D1 / D2) CBEAM Long Stress at Point (E1 / E2) CBEAM Long Stress at Point (F1 / F2) CBEAM Maximum (Stress1 / Stress2) CBEAM Margin of Safety (Compression1 / Compression2) CBEAM Margin of Safety (Tension1 / Tension2) CBEAM Minimum (Stress1 / Stress2) CELAS Stress CROD Axial (Stress / Safety Margin) CROD Torsional (Stress / Safety Margin) CWELD Axial Stress CWELD Bearing Stress CWELD Max Shear Stress CWELD Max (Stress A / Stress B) CWELD Min (Stress A / Stress B) |
ELEMENT |
SCALAR |
2D ForceMembrane (x / y / xy) Bending (x / y / xy) trans_shear (x / y) |
ELEMENT |
SCALAR |
CBEAM Forces*****CBEAM Axial Force CBEAM Bending Moment (Plane1 / Plane2) CBEAM Total Torque CBEAM Warping Torque CBEAM Web Shear (Plane1 / Plane2) |
ELEMENT |
SCALAR |
CHBDYGApplied Load Forced Convection Free Convection Radiation Total |
ELEMENT |
SCALAR |
Contact Pressure |
NODE |
SCALAR |
Contact Status |
NODE |
SCALAR |
Contact Stress Normal Stress Friction Stress 1 Friction Stress 2 |
NODE |
SCALAR |
CSHEAR ForceForce (4 to 1 / 2 to 1) Force (1 to 2 / 3 to 2) Force (2 to 3 / 4 to 3) Force (3 to 4 / 1 to 4) Kick Force on (1 / 2 / 3 / 4) Shear (12 / 23 / 34 / 41) |
ELEMENT |
SCALAR |
CSHEAR Forces****Corner Forces Kick Forces Shear Forces |
ELEMENT |
SCALAR |
CSHEAR StrainAverage shear Maximum shear Safety margin |
ELEMENT |
SCALAR |
CSHEAR StressMaximum shear Average shear Safety margin |
ELEMENT |
SCALAR |
CWELD ForceAxial Force Bending Moment (Plane1 A / Plane2 A) Bending Moment (Plane1 B / Plane2 B) Shear (Plane1 / Plane2) Torque |
ELEMENT |
SCALAR |
CWELD StrainAxial Strain Max Shear Strain Max Strain (A / B) Min Strain (A / B) |
ELEMENT |
SCALAR |
CWELD StressAxial Stress Bearing Stress Max Shear Stress Max Stress (A / B) Min Stress (A / B) |
ELEMENT |
SCALAR |
Damping Energy Damping Energy % of Total Energy Energy Density |
ELEMENT |
SCALAR |
Direct Grid Point Stresses Mean Pressure Normal (x / y / z) Shearxy Shearyz Shearzx Vonmises |
NODE |
SCALAR |
Direct Strain Firstprincipal Normal (x / y /z) Secondprincipal Shearangle Shearxy Shearyz Shearzx Thirdprincipal Vonmises |
ELEMENT |
SCALAR |
Direct Stress Firstprincipal Normal (x / y / z) Secondprincipal Shearangle Shearxy Shearyz Shearzx Thirdprincipal Vonmises |
ELEMENT |
SCALAR |
Failure Index For Direct Stress For Inter Laminar Stress |
ELEMENT |
SCALAR |
Grid Temperatures |
NODE |
SCALAR |
Heat Flow Applied Load Convection Convection Coefficient Radiation Total |
ELEMENT |
SCALAR |
Inter Laminar Strain Shear XZ Shear YZ |
ELEMENT |
SCALAR |
Inter Laminar Stress Shear XZ Shear YZ |
ELEMENT |
SCALAR |
Kinetic Energy Kinetic Energy % of Total Energy Energy Density |
ELEMENT |
SCALAR |
Nonlinear Strain Creep Normal (x / y / z) Plastic Shearxy Shearyz Shearzx |
ELEMENT |
SCALAR |
Nonlinear Stress Equivalent Normal (x / y / z) Shearxy Shearyz Shearzx |
ELEMENT |
SCALAR |
Axisymmetric StrainRadial Azimuthal Axial Shear Stress Maximum Principal Maximum Shear Octahedral |
ELEMENT |
SCALAR |
Axisymmetric StressRadial Azimuthal Axial Shear Stress Maximum Principal Maximum Shear Octahedral |
ELEMENT |
SCALAR |
Ply Thickness |
ELEMENT |
SCALAR |
Shell Thickness |
ELEMENT |
SCALAR |
Strain Energy Strain Energy % of total energy Energy density |
ELEMENT |
SCALAR |
Temperature |
NODE |
SCALAR |
The following table provides details about HyperView’s support for Nastran.
* |
See Element Forces (Vector Plot) for more details. |
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** |
Grid Point Element Forces/Moments are read into HV as element results with Corner Data. Corner data values represent the individual nodal grid point forces/moments for the given element. |
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*** |
See Element Forces (Tensor Plot) for more details. |
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**** |
CSHEAR Forces are read into HV as element results with Corner Data. Corner data values represent the following:
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***** |
CBEAM Forces are read into HV as element results with Corner Data. Corner data values represent the individual nodal grid point forces for the given element. |
• | HyperView supports composite stress in OP2 result files generated from Nastran 2012. |
• | HyperView supports GPFORCE results in OP2 result files for frequency response. |
• | HyperView supports OP2 result files generated with the option PARAM, POST, 1. |
• | HyperView supports the following data block names for PARAM, POST, -1: |
OQG1, OUGV1, OES1, OEF1, OSTR1, ONRGY1, OES1X .
• | HyperView supports the following data block names for PARAM, POST, -2: |
OQG1, BOUGV1, OUGV1, OES1, OEF1, OSTR1, ONRGY1, OES1X.
• | HyperView supports the following element types for stress and strain data types: |
CQUAD (33), CQUADR (82), CTETRA (39), CTRIAR(70) CQUAD8 (64), CHEXA (67), CPENTA (68), CTRIA3 (74)
CTRIA6 (75), CQUAD4(144), CTRIAX6 (53)
For corner stress and strain, following element types are supported:
CQUAD8 (64), CTRIA6 (75), CQUAD4(144), CTETRA (39), CHEXA (67), CPENTA (68)
• | HyperView supports the following element types for force data type: |
CROD(1), CONROD(10), CBEAM(2), CELAS1(11), CELAS2(12), CGAP(38), CBAR(34), CQUAD4(33), CTRIA3(74),
CQUAD(64), CQUADR(82), CTRIA6(75), CTRIAR(70), CQUAD4(144)
• | For modal frequency response problems (sol 103), the simulation name is Mode # f #Hz. |
• | HyperView supports the following data block names for geometry: |
GEOM1, GEOM1S, GEOM2, GEOM2S
HEX8(208), HEX20(220), PENTA6(206), PENTA15(215), TETRA4(204),
TETRA10(210), QUAD4(104), TRIA3(103), QUAD8(108), TRIA6(106),BAR(60),
ROD(61)
• | All tensor results (2D and 3D) should be viewed in the Element Result System |
• | To extract only a selected set of results, use the external translator HvTrans to create an h3d file. |
Functionality |
HyperView – Animation Window |
---|---|
Reads model file directly |
DAT, NAS, BDF, OP2, XDB |
Reads results file directly |
OP2, XDB |
Reads translated results |
PCH (hmnast: HMRES and H3D) OP2 (hmnast02:HMRES and H3D) |
Nastran Results Form for OP2 and XDB |
|
Nastran centroidal results |
Yes |
Nastran corner results |
Yes |
Thickness contour |
Yes |
Coordinate Systems |
|
Transforms results to other system type in application |
Yes |
Transform any tensor to vector results |
Yes |