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The association of material properties to a part is performed in two stages; the material is defined using the command
PROPERTY MATERIAL GENERAL [matname] 96 reals...
and attached to a geometric part or set of parts via the command
PROPERTY ATTACH partname matname
All elements must have a material property regardless of the destination analysis code.
The material properties are defined by the following list of 96 real numbers which correspond to the PATRAN Neutral file definitions (See PATRAN Plus User Guide 29-17).
Material Types
| 1 | Isotropic | 4 | TIS option | 11 | HAL option | |
| 2 | 2D anisotropic | 5 | TAN option | 12 | LAM option | |
| 3 | 3D orthotropic | 6-7 | 3D anisotropic | 13 | MIX option |
Material Property Constants
1 Reference Temperature (T) 2 Density (RHO) 3-5 Characteristic dimensions (HZ,HY,HX) 6 Structural damping coefficient (GE) 7 Specific heat (CP) 8 Option = material type 9-14 6 Thermal expansion coefficients15-20 6 Thermal conductivities (K11,K12,K13,K22,K23,K33) 21-26 2D thermal stress resultants for 1-degree temperature rise (N1,N2,N12,M1,M2,M12) 27-35 9 engineering material properties
36 0 = n/a 37-57 21 material stiffness matrix terms (C11,C12,C13,C22,C23,C33,C44,C45,C46,C55,C56, C66,C14,C15,C16,C24,C25,C26,C34,C35,C36) 58-63 6 2D membrane stiffness matrix terms (A11,A12,A13,A22,A23,A33) 64-69 6 2D bending stiffness matrix terms (D11,D12,D13,D22,D23,D33) 70-78 9 2D membrane/bending coupling terms (B11,B12,B13,B21,B22,B23,B31,B32,B33) 79-81 Stress limits for tension, compression, and shear (ST,SC,SS) 82 Emissivity 83-96 n/a not applicable at present
There are two methods for entering this material data:
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