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/FAIL/EMC - Extended Mohr Coulomb Failure Model

Description

Describes failure dependent on effective plastic strain.

Format

(1)

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/FAIL/EMC/mat_ID/unit_ID

a

n

b0

c

 

 

 

Card 2

(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

symbol_y

 

 

 

 

 

Optional Line:

(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

fail_ID

 

 

 

 

 

 

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)

 

a

Hosford exponent

Default = 1.0  (Real)

 

n

Stress state sensitivity exponent

(Real)

 

b0

Strain to fracture for uni-axial tension (Comment 2)

Default = 1.0 (Real)

 

c

Friction parameter for triaxiality

Default = 0.0  (Real)

 

symbol_y

Strain rate sensitivity parameter

(Real)

 

Reference strain rate

Default = 1030  (Real)

fail_ID

(Optional) Failure criteria identifier (Comment 3)

(Integer, maximum 10 digits)

 

hmtoggle_plus1Example (Metal)

Fracture parameters could be identified with tests like uniaxial tension (), pure shear (), and axisymmetric compression ().

 

#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/LAW84/1/1

Swift-voce (metal)

#              RHO_I

                8E-9

#                  E                  NU

             206000.                0.30

#                P12                 P22                 P33               QVOCE               BVOCE

                -0.5                  1.                  3.            524.0000                 25.

#                G11                 G22                 G33                  K0               ALPHA

                -0.5                  1.                  3.                100.                 0.5

#                 AN                EPS0                  NN               CEPSP               DEPS0

               1000.             0.00128               0.200               0.014              0.0011

#                ETA                  CP                TINI                TREF               TMELT

                 0.9              420e+8                 293                293.               1700.

#              MTEMP              DEPSAD

               0.921               1.379

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

/FAIL/EMC/1/1

#         exponent_a          exponent_n              coef_b              coef_c

                 1.9                 0.2                0.20                 0.0

#               GAMA               DEPS0

                 0.0                 1.0

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

#ENDDATA

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

hmtoggle_plus1Comments
1.The failure criteria is calculated as follows:

Where,

Where,

f1, f2 and f3 are functions of the Lode angle

With

Where, is the traixiality .

2.The coefficient, b is computed as follows:

if  else

3.The fail_ID is used with /STATE/BRICK/FAIL and /INIBRI/FAIL for brick. There is no default value. If the line is blank, no value will be output for failure model variables in the /INIBRI/FAIL (written in .sta file with /STATE/BRICK/FAIL for brick).

See Also:

Stress triaxiality and Lode Angle