HyperWorks Solvers

/MAT/LAW23 (PLAS_DAMA)

/MAT/LAW23 (PLAS_DAMA)

Previous topic Next topic Expand/collapse all hidden text  

/MAT/LAW23 (PLAS_DAMA)

Previous topic Next topic JavaScript is required for expanding text JavaScript is required for the print function  

Block Format Keyword

/MAT/LAW23 - Elastic Plastic with Damage Material

Description

This law models an isotropic elastic plastic material and combines Johnson-Cook material model with a generalized damage model. The law is applicable only for solid elements.

Format

(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

/MAT/LAW23/mat_ID/unit_ID or /MAT/PLAS_DAMA/mat_ID/unit_ID

mat_title

 

 

 

 

 

 

 

 

E

 

 

 

 

 

 

a

b

n

c

ICC

 

 

 

 

 

Et

 

 

 

 

 

 

hmtoggle_plus1Flag Definition

Field

Contents

SI Unit Example

mat_ID

Material identifier

(Integer, maximum 10 digits)

 

unit_ID

Optional 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)

 

a

Plasticity yield stress - should be strictly positive.

(Real)

b

Plasticity hardening parameter

(Real)

 

n

Plasticity hardening exponent (Comment 3)

(Real)

 

Failure plastic strain

Default = 1030  (Real)

 

Plasticity maximum stress

Default = 1030  (Real)

c

Strain rate coefficient

Default = 0.00  (Real)

= 0: no strain rate effect

 

Reference strain rate

If , no strain rate effect

(Real)

ICC

Strain rate computation flag (Comment 5)

(Integer)

= 0: default set to 1

= 1: strain rate effect on

= 2: no strain rate effect on

 

Damage model starts at

Default = 0.15  (Real)

 

Et

Softening damage slope ()

Default = 0.00  (Real)

hmtoggle_plus1Example (Aluminum)

#RADIOSS STARTER

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

/UNIT/1

unit for mat

                  g                  mm                  ms

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

#-  2. MATERIALS:

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

/MAT/LAW23/1/1

Aluminum

#              RHO_I

               .0027

#                  E                  NU

               70000                  .3

#                  a                   b                   n             EPS_max          SIGMA_max0

                 100                   0                   1                  .2                 100

#                  c               EPS_0       ICC

                   0                   0         0

#            EPS_dam                 E_t

                  .1               -2000

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

#ENDDATA

/END

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

hmtoggle_plus1Comments
1.The damage law is applied to the stress tensor and damage occurs in tension, compression and shear.
2.The input is the same as material law /MAT/DAMA (LAW22).
3.The plasticity hardening exponent n must be less than one.
4.When reaches , in one integration point, then the solid element is deleted.
5.ICC is a flag of the strain rate effect on material maximum stress .

mat_law27

See Also:

Material Compatibility

Law Compatibility with Failure Model

/MAT/LAW2 in Theory Manual

Ductile damage model in Theory Manual

More Options in FAQ