/MAT/LAW1 (ELAST)
Block Format Keyword This keyword defines an isotropic, linear elastic material using Hooke's law. This law represents a linear relationship between stress and strain. It is available for truss, beam (type 3 only), shell and solid elements.
Format
(1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) |
---|---|---|---|---|---|---|---|---|---|
/MAT/LAW1/mat_ID/unit_ID or /MAT/ELAST/mat_ID/unit_ID | |||||||||
mat_title | |||||||||
E |
Definition
Field | Contents | SI Unit Example |
---|---|---|
mat_ID | Material identifier (Integer, maximum 10 digits) |
|
unit_ID | Unit Identifier (Integer, maximum 10 digits) |
|
mat_title | Material title (Character, maximum 100 characters) |
|
Initial density (Real) |
||
E | Young's modulus (Real) |
|
Poisson's ratio (Real) |
Example (Elastic - Steel)
#RADIOSS STARTER
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/UNIT/1
unit for mat
Mg mm s
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#- 2. MATERIALS:
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/MAT/ELAST/1/1
Steel
# RHO_I
7.85E-9 0
# E nu
210000 .3
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#ENDDATA
/END
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
Comments
- This material law is used to model
purely elastic materials. The material stiffness is determined by only two values: the
Young's modulus (E), and Poisson's ratio (
). The shear modulus (G) can be computed using E and
, as:
(1) - The stress-strain relationship can be
represented as shown:
(2) - The value of density is always used in explicit simulations and it may also be used in static implicit simulations to reach a better convergence in quasi-static analysis.
- Global integration approach is applied
to LAW1 and shell elements (/PROP/TYPE1 (SHELL)), when the number of
integration points through the shell thickness is different from NP=1
(membranes).Note: Failure models are not available in the case of global integration. LAW2 and LAW27 with very high yield stress may be used as a substitution to LAW1 in these cases.