MSC Nastran > Read Results > 4.2 Supported OUTPUT2 Result and Model Quantities
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4.2 Supported OUTPUT2 Result and Model Quantities
The following table indicates all the possible results quantities that can be loaded into the Patran database during results translation from MD Nastran. The Primary and Secondary Labels are items selected from the postprocessing menus. The Type indicates whether the results are Scalar, Vector, or Tensor, and determines which postprocessing techniques are available to view the results quantity. Data Block indicates which MD Nastran OUTPUT2 data block the data comes from. The Description gives a brief discussion about the results quantity, such as if it is only for certain element types, and what Output Request selection will generate this data block. For design optimization, all of the listed results can be loaded as a function of design cycle.
Results
 
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
Global Variables
In addition to standard results quantities, a number of Global Variables can be created. This table outlines Global Variables that may be created. Global Variables are results quantities where one value is representative of the entire model.
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.
Coordinate Systems
In some cases, the elemental stresses and strains are transformed from one coordinate frame to another when imported into the Patran database. The following describes the coordinate systems for these element results after they are imported into the Patran database. The coordinate system names referred to are described in the Patran or the MD Nastran documentation.
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.
Projected Global System
The projected system is defined as follows. First, the normal to the shell surface is calculated. This varies for curved elements and is constant for flat elements. If the angle between the normal and the global x-axis is greater than .01 radians, the global x-axis is projected onto the shell surface as the local x-axis. If the angle is less than .01 radians, either the global y-axis or the z-axis (whichever makes the largest angle with the normal) is defined to be the local x-axis. The local y-axis is perpendicular to the plane defined by the normal and the local x-axis.
XY Plots
For results from MD Nastran design optimization solution 200 runs, three XY Plots are generated, but not posted, when the Read OUTPUT2 option is selected:
1. Objective Function vs. Design Cycle.
1. Maximum Constraint Value vs. Design Cycle.
1. Design Variable vs. Design Cycle.
These plots can be viewed under the XY Plot option in (p. 1) in the Patran User’s Guide. When they are initially posted, you will have to expand their windows to view them properly.
Model Data
The following table outlines all the data that will be created in the Patran database when reading model data from an MD Nastran OUTPUT2 file and the location in the OUTPUT2 file from where it is derived. This is the only data extracted from the OUTPUT2 file. This data should be sufficient for evaluating results values.
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