Supported Nastran Results in HyperView

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

Data types supported from Nastran OP2 files include:
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 Forces4

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 Forces4

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 types supported from Nastran H5 files include:
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
The following table provides details about HyperView support for Nastran.
  1. See Element Forces (Vector Plot) for more details.
  2. 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.
  3. See Element Forces (Tensor Plot) for more details.
  4. 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
  5. 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.
  6. 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.

Note:
  • 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