| UI Name |
Automation (neutral) Name |
Value type |
Range |
Default Value |
| CSYS |
CSYSOption |
integer |
| Valid Options |
| Absolute=0 |
| Cartesian=1 |
| Cylindrical=2 |
| Spherical=3 |
|
0 |
| Local see note (1) |
Plane of Deformation |
coordinate system |
| Valid Entities |
| coordinate system |
|
-- |
| Material |
material |
physical material |
| Excluded Materials |
| Isotropic |
| Orthotropic |
| Anisotropic |
| Formability |
| Fluid |
| Mooney-Rivlin Test Data |
| Polynomial |
| Reduced Polynomial |
| Ogden Test Data |
| Foam Test Data |
| Blatz |
| Arruda-Boyce Test Data |
| Neo Hooke |
| Neo Hooke Test Data |
| Marlow |
| Van Der Waals |
| Yeoh |
| Yeoh Test Data |
| Gent |
| Gasket |
| Gasket Behavior |
| |
|
-- |
| A10 - Distortional Deformation Constant |
A10 |
double |
-FLT_MAX to FLT_MAX |
0.0 |
| A01 - Distortional Deformation Constant |
A01 |
double |
-FLT_MAX to FLT_MAX |
0.0 |
| D1 - Volumetric Deformation Constant |
D1 |
double |
0.000 to FLT_MAX |
-- |
| Mass Density |
RHO |
double |
-FLT_MAX to FLT_MAX |
-- |
| Coefficient of Volumetric Thermal Expansion |
AV |
double |
-FLT_MAX to FLT_MAX |
0.0 |
| Reference Temperature |
TREF |
double |
-FLT_MAX to FLT_MAX |
-- |
| Structural Damping Coefficient |
GE |
double |
-FLT_MAX to FLT_MAX |
0.0 |
| Default Thickness |
Plane Stress Thickness |
double |
0.000 to FLT_MAX |
-- |
| Output Location |
Output Location |
integer |
| Valid Options |
| GRID=0 |
| GAUSS=1 |
|
0 |
