Primary Label | Secondary Label | Type | DataBlocks | Description |
Acoustic | Intensity | Scalar | OAIG1 | Acoustic intensity on surface in contact with fluid. |
Acoustic | Radiated Power | Scalar | OARPWR1 | Acoustic power radiated from surface in contact with fluid. |
Acoustic | Field Point Mesh | Vector | OUGFP1 | Acoustic results for Field Point Mesh. |
Acoustic | Velocity @ FPM Grids | Vector | OVGFP1 | Acoustic velocities at the node points of Field Point Mesh. |
Bar Forces | Rotational | Vector | OEF1 | Bar moments |
Translational | Vector | OEF1 | Bar forces | |
Warping Torque | Scalar | OEF1 | Warping torque | |
Bar Strains | Axial Safety Margin | Scalar | OSTR1 | Axial safety margin |
Compression Safety Margin | Scalar | OSTR1 | Safety margin in compression | |
Maximum Axial | Scalar | OSTR1 | Maximum axial strain | |
Minimum Axial | Scalar | OSTR1 | Minimum axial strain | |
Tension Safety Margin | Scalar | OSTR1 | Safety margin in tension | |
Torsional Safety Margin | Scalar | OSTR1 | Safety margin in torsion | |
Bar Stresses | Axial Safety Margin | Scalar | OES1 | Axial safety margin |
Compression Safety Margin | Scalar | OES1 | Safety margin in compression | |
Maximum Axial | Scalar | OES1 | Maximum axial stress | |
Minimum Axial | Scalar | OES1 | Minimum axial stress | |
Tension Safety Margin | Scalar | OES1 | Safety margin in tension | |
Torsional Safety Margin | Scalar | OES1 | Safety margin in torsion | |
Grid Point Stresses | Stress Tensor | Tensor | OGS1 | Stress tensor |
Zero Shear Angle | Scalar | OGS1 | Zero shear angle | |
Major Principal | Scalar | OGS1 | Major principal | |
Minor Principal | Scalar | OGS1 | Minor principal | |
Maximum Shear | Scalar | OGS1 | Maximum shear | |
von Mises | Scalar | OGS1 | von mises | |
Gap Results | Displacement | Vector | OEF1 or OES1 | Gap element displacement |
Force | Vector | OEF1 or OES1 | Gap element force | |
Slip | Vector | OEF1 or OES1 | Gap element slip | |
Nonlinear Strains | Creep Strain | Scalar | OESNL1 | Creep strain |
Plastic Strain | Scalar | OESNL1 | Plastic strain | |
Strain Tensor | Tensor | OESNL1 | Strain tensor | |
Nonlinear Stresses | Equivalent Stress | Scalar | OESNL1 | Equivalent stress |
Stress Tensor | Tensor | OESNL1 | Stress tensor | |
Principal Strain Direction | 1st Principal x cosine | Scalar | OSTR1 | 1st Principal x cosine |
1st Principal y cosine | Scalar | OSTR1 | 1st Principal y cosine | |
1st Principal z cosine | Scalar | OSTR1 | 1st Principal z cosine | |
2nd Principal x cosine | Scalar | OSTR1 | 2nd Principal x cosine | |
2nd Principal y cosine | Scalar | OSTR1 | 2nd Principal y cosine | |
2nd Principal z cosine | Scalar | OSTR1 | 2nd Principal z cosine | |
3rd Principal x cosine | Scalar | OSTR1 | 3rd Principal x cosine | |
3rd Principal y cosine | Scalar | OSTR1 | 3rd Principal y cosine | |
3rd Principal z cosine | Scalar | OSTR1 | 3rd Principal z cosine | |
Zero Shear Angle | Scalar | OSTR1 | Zero shear angle | |
Principal Stress Direction | 1st Principal x cosine | Scalar | OES1 | 1st Principal x cosine |
1st Principal y cosine | Scalar | OES1 | 1st Principal y cosine | |
1st Principal z cosine | Scalar | OES1 | 1st Principal z cosine | |
2nd Principal x cosine | Scalar | OES1 | 2nd Principal x cosine | |
2nd Principal y cosine | Scalar | OES1 | 2nd Principal y cosine | |
2nd Principal z cosine | Scalar | OES1 | 2nd Principal z cosine | |
3rd Principal x cosine | Scalar | OES1 | 3rd Principal x cosine | |
3rd Principal y cosine | Scalar | OES1 | 3rd Principal y cosine | |
3rd Principal z cosine | Scalar | OES1 | 3rd Principal z cosine | |
Zero Shear Angle | Scalar | OES1 | Zero shear angle | |
Shear Panel Forces | Force12 | Scalar | OEF1 | Shear force from nodes 1 to 2 |
Force14 | Scalar | OEF1 | Shear force from nodes 1 to 4 | |
Force21 | Scalar | OEF1 | Shear force from nodes 2 to 1 | |
Force23 | Scalar | OEF1 | Shear force from nodes 2 to 3 | |
Force32 | Scalar | OEF1 | Shear force from nodes 3 to 2 | |
Force34 | Scalar | OEF1 | Shear force from nodes 3 to 4 | |
Force41 | Scalar | OEF1 | Shear force from nodes 4 to 1 | |
Force43 | Scalar | OEF1 | Shear force from nodes 4 to 3 | |
Kick | Scalar | OEF1 | Kick forces | |
Rotational | Vector | OEF1 | Moments at nodes | |
Shear | Scalar | OEF1 | Shear force in panel | |
Translational | Vector | OEF1 | Forces at nodes | |
Shear Panel Strains | Average Shear | Scalar | OSTR1 | Average shear strain in panel |
Maximum Shear | Scalar | OSTR1 | Maximum shear strain in panel | |
Safety Margin | Scalar | OSTR1 | Shear safety margin of panel | |
Shear Panel Stresses | Average Shear | Scalar | OES1 | Average shear stress in panel |
Maximum Shear | Scalar | OES1 | Maximum shear stress in panel | |
Safety Margin | Scalar | OES1 | Shear safety margin of panel | |
Shell Forces | Force Resultant | Tensor | OEF1 | Force resultants and moment resultants |
Moment Resultant | Tensor | OEF1 | Moment stress resultants | |
Strain Curvatures | Strain Tensor | Tensor | OSTR1 | Strain curvatures of a plate |
1st Principal | Scalar | OSTR1 | Curvature of strain 1st principal | |
2nd Principal | Scalar | OSTR1 | Curvature of strain 2nd principal | |
Maximum Shear | Scalar | OSTR1 | Curvature of maximum shear strain | |
von Mises | Scalar | OSTR1 | Curvature of von Mises strain | |
Zero Shear Angle | Scalar | OSTR1 | Curvature of zero shear angle | |
Strain Energy | Energy | Scalar | ONRGY1 | Element’s total strain energy |
Energy Density | Scalar | ONRGY1 | Element’s strain energy density | |
Percent of Total | Scalar | ONRGY1 | Element’s percentage of total strain density | |
Strain Invariants | 1st Principal | Scalar | OSTR1 | Strain 1st principal |
2nd Principal | Scalar | OSTR1 | Strain 2nd principal | |
3rd Principal | Scalar | OSTR1 | Strain 3rd principal | |
Maximum Shear | Scalar | OSTR1 | Maximum shear strain | |
Mean Pressure | Scalar | OSTR1 | Mean strain pressure | |
Octahedral Shear | Scalar | OSTR1 | Octahedral shear strain | |
von Mises | Scalar | OSTR1 | von Mises equivalent strain | |
Strain Tensor | NONE | Tensor | OSTR1 | Strain tensor |
Stress Invariants | 1st Principal | Scalar | OES1 | Stress 1st Principal |
2nd Principal | Scalar | OES1 | Stress 2nd Principal | |
3rd Principal | Scalar | OES1 | Strain 3rd Principal | |
Maximum Shear | Scalar | OES1 | Maximum shear stress | |
Mean Pressure | Scalar | OES1 | Mean stress principal | |
Octahedral Shear | Scalar | OES1 | Octahedral shear stress | |
von Mises | Scalar | OES1 | von Mises equivalent stress | |
Stress Tensor | NONE | Tensor | OES1 | Stress tensor |
Accelerations | Rotational | Vector | OUGV1 | Nodal angular accelerations |
Translational | Vector | OUGV1 | Nodal translational accelerations | |
Applied Loads | Rotational | Vector | OPG1 | Nodal equivalent applied moments |
Translational | Vector | OPG1 | Nodal equivalent applied forces | |
Constraint Forces | Rotational | Vector | OQG1 | Nodal moments of single-point constraints |
Translational | Vector | OQG1 | Nodal forces of single-point constraint | |
Displacements | Rotational | Vector | OUGV1 | Nodal rotational displacements |
Translational | Vector | OUGV1 | Nodal translational displacements | |
Eigenvectors | Rotational | Vector | OPHIG | Nodal rotational eigenvectors |
Translational | Vector | OPHIG | Nodal translational eigenvectors | |
Nonlinear Applied Loads | Rotational | Vector | OPNL1 | Nodal nonlinear applied moments |
Translational | Vector | OPNL1 | Nodal nonlinear applied forces | |
Velocities | Rotational | Vector | OUGV1 | Nodal angular velocity |
Translational | Vector | OUGV1 | Nodal translational velocity | |
Error | Estimate | Scalar | ERROR | Elemental error in adaptive analysis |
Grid Point Forces | Elements | Vector | OGPFB1* | Internal nodal force contribution by element |
Applied Loads | Vector | OGPFB1* | Nodal equivalent applied forces | |
Constraint Forces | Vector | OGPFB1* | Nodal equivalent constraint forces | |
Total | Vector | OGPFB1* | Total nodal equivalent forces due to internal loads, applied loads and constraint forces. | |
Grid Point Moments | Elements | Vector | OGPFB1* | Internal nodal moment contribution by element |
Applied Loads | Vector | OGPFB1* | Nodal equivalent applied moments | |
Constraint Forces | Vector | OGPFB1* | Nodal equivalent constraint moments | |
Total | Vector | OGPFB1* | Total nodal equivalent moments due to internal loads, applied loads and constraint forces. | |
Shape Change | None | Vector | GEOMIN | In a shape optimization run, this is the new shape displayed as a deformation of the original shape. |
Active Constraints | Element Stress | Scalar | R1TABRG | Element stress |
Element Strain | Scalar | R1TABRG | Element strain | |
Element Force | Scalar | R1TABRG | Element force | |
Element Ply Failure | Scalar | R1TABRG | Element ply failure | |
Translational Displacement | Vector | R1TABRG | Nodal translational displacement | |
Rotational Displacement | Vector | R1TABRG | Nodal rotational displacement | |
Translational Velocity | Vector | R1TABRG | Nodal translational velocity | |
Rotational Velocity | Vector | R1TABRG | Nodal rotational velocity | |
Translational Acceleration | Vector | R1TABRG | Nodal translational acceleration | |
Rotational Acceleration | Vector | R1TABRG | Nodal rotational acceleration | |
Translational SPC | Vector | R1TABRG | Nodal translational SPC force | |
Rotational SPC | Vector | R1TABRG | Nodal rotational SPC force |
Labels | Type | DataBlocks | Description |
Critical Load Factor | S | Oxxx | Value of buckling load for the given buckling mode. |
Time | S | Oxxx | Time value of the time step. |
Frequency | S | Oxxx | Frequency value of the frequency step or for the normal mode. |
Damping Ratio | S | Oxxx | Damping ratio value of a complex eigenvalue analysis. |
Eigenvalue | S | Oxxx | Eigenvalue for normal modes or complex eigenvalue analysis. |
Percent of Load | S | Oxxx | Percent of load value for a nonlinear static analysis. |
Adaptive Cycle | S | Oxxx | Cycle number in p-adaptive analysis. |
Design Cycle | S | Oxxx | Cycle number in an optimization run (SOL 200). |
Design Variable | S | DESTAB HISADD | Design Variable for optimization (Label from DESTAB, value from HISADD). |
Maximum Constraint Value | S | HISADD | Maximum constraint value for optimization. |
Objective Function | S | HISADD | Objective function for optimization. |
CTRIA3 | Table 4-1 Results are in the MD Nastran system which coincides with the Patran IJK system. At the user’s request during postprocessing, these results can be transformed by Patran to alternate coordinate systems. If the user selects a component of a stress or strain tensor to be displayed, by default, the Results application transforms the tensor to a projected global system (Projected Global System). |
CQUAD4 | Table 4-2 Results are in the MD Nastran “bisector” coordinate system but may be transformed by Patran to alternate coordinate systems (e.g., global) during postprocessing. If the user selects a component of a stress or strain tensor to be displayed, by default, the Results application transforms the tensor to a projected global system (Projected Global System). Import of results when this element is used in a hyperelastic analysis is not currently supported. |
CHEXA, CPENTA, CTETRA | Table 4-3 The user can request that MD Nastran compute element results in either a local element or alternate coordinate system via the PSOLID entry. If the element results are in the local element system, these are converted to the Patran IJK system on import. If the results are in a system other than local element, they are imported in this system. These results may be transformed to alternate systems during postprocessing. |
CQUAD8, CTRI6 | Table 4-4 The elemental coordinate system, used by MD Nastran for results, is described in the MD Nastran documentation. These results are imported into the Patran database “as-is”. These results can be postprocessed in Patran using the “As Is” options, but they cannot be transformed to alternate coordinate systems. |
Item | Block | Description |
Nodes | GEOM1 | Node ID Nodal Coordinates Reference Coordinate Frame Analysis Coordinate Frame |
Coordinate Frames | GEOM1 | Coordinate Frame ID Transformation Matrix Origin Can be Rectangular, Cylindrical, or Spherical |
Elements | GEOM2 | Element ID Topology (e.g., Quad/4 or Hex20) Nodal Connectivity |