# Supported Nastran Results in HyperView

HyperView supports Nastran FEMZIP, OP2, XDB and H5 result file formats.

Data Name | Result Type | Data Type |
---|---|---|

1D Element (Forces / Moments)^{1} |
ELEMENT | VECTOR |

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 Strain CBEAM 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 Nonlinear Stress: CBEAM 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 Strain CBAR 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 Stress CBAR 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 Element (Forces / Moments)^{3} |
ELEMENT | TENSOR3-D |TENSOR2-D |

2D Force Membrane (x / y / xy) Bending (x / y / xy) trans_shear (x / y) |
ELEMENT | SCALAR |

Acceleration (Translation / Rotation) | NODE | VECTOR |

Acoustic Results Sound Pressure RMS Sound Pressure Sound Pressure in dB Sound Pressure in dBa |
NODE | SCALAR |

Applied (Forces / Moments) | NODE | VECTOR |

Axisymmetric Strain Radial Azimuthal Axial Shear Stress Maximum Principal Maximum Shear Octahedral |
ELEMENT | SCALAR |

Axisymmetric Stress Radial Azimuthal Axial Shear Stress Maximum Principal Maximum Shear Octahedral |
ELEMENT | SCALAR |

Bolt Axial Force | ELEMENT | SCALAR |

Bolt Axial Strain | ELEMENT | SCALAR |

Bolt Bending Moment | ELEMENT | SCALAR |

Bolt Shear Force | ELEMENT | SCALAR |

CBEAM Forces^{4}CBEAM Axial Force CBEAM Bending Moment (Plane1 / Plane2) CBEAM Total Torque CBEAM Warping Torque CBEAM Web Shear (Plane1 / Plane2) |
ELEMENT | SCALAR |

CHBDYG Applied Load Forced Convection Free Convection Radiation Total |
ELEMENT | SCALAR |

Composite (Stress / Strain) | ELEMENT | TENSOR3-D |TENSOR2-D |

Contact (Force / Moment / Traction) | NODE | VECTOR |

Contact Incremental Slide | NODE | VECTOR |

Contact Pressure | NODE | SCALAR |

Contact Status | NODE | SCALAR |

Contact Stress Normal Stress Friction Stress 1 Friction Stress 2 |
NODE | SCALAR |

Contact Total Slide | NODE | VECTOR |

CSHEAR Force Force (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^{4}Corner Forces Kick Forces Shear Forces |
ELEMENT | SCALAR |

CSHEAR Strain Average shear Maximum shear Safety margin |
ELEMENT | SCALAR |

CSHEAR Stress Maximum shear Average shear Safety margin |
ELEMENT | SCALAR |

CWELD Force Axial Force Bending Moment (Plane1 A / Plane2 A) Bending Moment (Plane1 B / Plane2 B) Shear (Plane1 / Plane2) Torque |
ELEMENT | SCALAR |

CWELD Strain Axial Strain Max Shear Strain Max Strain (A / B) Min Strain (A / B) |
ELEMENT | SCALAR |

CWELD Stress Axial 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 |

Displacement | NODE | VECTOR |

Element (Fluxes / Gradients | ELEMENT | VECTOR |

Element ERP ERP Value ERP Fraction ERP dB |
ELEMENT | SCALAR |

Failure Index For Direct Stress For Inter Laminar Stress |
ELEMENT | SCALAR |

Grid Point Element (Forces / Moments)^{2} |
ELEMENT | VECTOR |

Grid Point Stresses | NODE | TENSOR3-D |TENSOR2-D |

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 |

MPC (Forces / Moments) | NODE | VECTOR |

Nonlinear Strain | ELEMENT | TENSOR3-D |TENSOR2-D |

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 |

Ply Thickness | ELEMENT | SCALAR |

Rotation | NODE | VECTOR |

Shell Thickness | ELEMENT | SCALAR |

SPC (Forces / Moment)^{6} |
NODE | VECTOR |

Strain | ELEMENT | TENSOR3-D |TENSOR2-D |

Strain Energy Strain Energy % of total energy Energy density |
ELEMENT | SCALAR |

Stress | ELEMENT | TENSOR3-D |TENSOR2-D |

Summed (Forces / Moments) | NODE | VECTOR |

Temperature | NODE | SCALAR |

Velocity (Translation / Rotation) | NODE | VECTOR |

Vibration Intensity | ELEMENT | VECTOR |

Data Name | Result Type | Data Type |
---|---|---|

1D Element Forces | ELEMENT | Scalar |

1D Element Moments | ELEMENT | Scalar |

1D Force | ELEMENT | Scalar |

1D NonLinear Strain | ELEMENT | Scalar |

1D NonLinear Stress | ELEMENT | Scalar |

1D Strain | ELEMENT | Scalar |

1D Stress | ELEMENT | Scalar |

2D Element Force | ELEMENT | Tensor |

2D Element Moment | ELEMENT | Tensor |

2D Force | ELEMENT | Scalar |

Acceleration - Rotation | NODE | Vector |

Acceleration - Translation | NODE | Vector |

Acoustic Results Sound Pressure RMS Sound Pressure Sound Pressure in dB Sound Pressure in dBa |
NODE | Scalar |

Applied Force | NODE | Vector |

Applied Moment | NODE | Vector |

CBEAM Forces | ELEMENT | Scalar |

CBUSH Forces | ELEMENT | Scalar |

CBUSH Stress | ELEMENT | Scalar |

CFAST Forces | ELEMENT | Scalar |

Composite Strain | ELEMENT | Tensor |

Composite Stress | ELEMENT | Tensor |

Contact Forces | NODE | Vector |

Contact Status | NODE | Scalar |

Contact Status:Friction Stress 1 | NODE | Scalar |

Contact Status:Friction Stress 2 | NODE | Scalar |

Contact Status:Normal Stress | NODE | Scalar |

CSHEAR Forces | ELEMENT | Scalar |

CWELD Forces | ELEMENT | Scalar |

CWELD Strain | ELEMENT | Scalar |

CWELD Stress | ELEMENT | Scalar |

Direct Nonlinear Strain | ELEMENT | Scalar |

Direct Nonlinear Stress | ELEMENT | Scalar |

Direct Stress: normal-x,y,z, shear-xy,yz,zx | ELEMENT | Scalar |

Direct Strain: normal-x,y,z, shear-xy,yz,zx | ELEMENT | Scalar |

Displacement | NODE | Vector |

Element ERP ERP Value ERP Fraction ERP dB |
ELEMENT | Scalar |

Failure Index:for direct Stress | ELEMENT | Scalar |

Failure Index:for inter laminar Stress | ELEMENT | Scalar |

Friction Forces | NODE | Vector |

Grid Point Applied Forces | NODE | Vector |

Grid Point Applied Moments | NODE | Vector |

Grid Point Element Forces | ELEMENT | Vector |

Grid Point Element Moments | ELEMENT | Vector |

Grid Point MPC Forces | NODE | Vector |

Grid Point MPC Moments | NODE | Vector |

Grid Point SPC Forces | NODE | Vector |

Grid Point SPC Moments | NODE | Vector |

Grid Point Summed Forces | NODE | Vector |

Grid Point Summed Moments | NODE | Vector |

InterLaminar Strain | ELEMENT | Scalar |

InterLaminar Stress | ELEMENT | Scalar |

Kinetic Energy | ELEMENT | Scalar |

MPC Force | NODE | Vector |

MPC Moment | NODE | Vector |

NonlinearStrain | ELEMENT | Tensor |

NonlinearStress | ELEMENT | Tensor |

Ply thickness | ELEMENT | Scalar |

Rotation | NODE | Vector |

Shell Thickness | ELEMENT | Scalar |

SPC Force | NODE | Vector |

SPC Moment | NODE | Vector |

Strain | ELEMENT | Tensor |

Strain Energy:% of Total Energy | ELEMENT | Scalar |

Strain Energy:Energy Density | ELEMENT | Scalar |

Strain Energy:Strain Energy | ELEMENT | Scalar |

Stress | ELEMENT | Tensor |

TotalPly thickness | ELEMENT | Scalar |

Velocity - Rotation | NODE | Vector |

Velocity - Translation | NODE | Vector |

Vibration Intensity | ELEMENT | Vector |

- See Element Forces (Vector Plot) for more details.
- 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.
- See Element Forces (Tensor Plot) for more details.
- CSHEAR Forces are read into
HV as element results with Corner Data. Corner data values represent the following:
- Corner Forces: N1: Force 4 to 1
- Corner Forces: N2: Force 1 to 2
- Corner Forces: N3: Force 2 to 3
- Corner Forces: N4: Force 3 to 4
- Shear Forces: N1: Shear 41
- Shear Forces: N2: Shear 12
- Shear Forces: N3: Shear 23
- Shear Forces: N4: Shear 34
- Kick Forces: N1: Kick 1
- Kick Forces: N2: Kick 2
- Kick Forces: N3: Kick 3
- Kick Forces: N4: Kick 4

- 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.
- Result from
`OGPFB1 (Grid point force)`

block: Reader creates data type as “SPC Forces”. And this block will have results like SPC,MPC,Applied forces/moments.Results from

`OQG1 (SPC force)`

block: Reader creates data type as “SPC Force”. And this block will have only SPC force/moment data’s.

- 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.
- Random Response Results will create PSD, RMS, CRMS, N0 and AUTO Function Load Cases, that can have any Data Type listed above.

## Reading Nastran Model and Result Files

Functionality | HyperView – Animation Window |
---|---|

Reads model file directly | DAT, NAS, BDF, OP2, XDB, H5 |

Reads results file directly | OP2, XDB, H5 |

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 |