Manufacturing Simulation Using Finite Element - Finite Element Analysis for Satellite Structures - page 310

**
*Material, name = AL2024-T351
*Conductivity
121000.,
*Damage Initiation, criterion = JOHNSON-COOK
0.112, 0.123, 1.5, 0.007, 0., 638., 25., 1.
*Damage Evolution, type = DISPLACEMENT
0.0,
*Density
2.78e-06,
*Elastic
7.31e ? 07, 0.33
*Expansion
2.47e-05,
*Inelastic Heat Fraction
0.9,
*Plastic, hardening = JOHNSON-COOK
369000.,684000., 0.34, 1.7, 638., 25.
*Rate Dependent, type = JOHNSON-COOK
0.0083,1.
*Specific Heat
9.2e ? 08,
*Material, name = ''Tungsten Carbide''
*Density
1.58e-05,
*Elastic
6.9e ? 08, 0.24
**
** INTERACTION PROPERTIES
**
*Surface Interaction, name = IntProp-1
*Friction
0.6,
*Surface Behavior, pressure-overclosure = HARD
**
** BOUNDARY CONDITIONS
**
** Name: BC-3 Type: Displacement/Rotation
*Boundary
_PickedSet24, 1, 1
_PickedSet24, 2, 2
_PickedSet24, 3, 3
_PickedSet24, 4, 4
_PickedSet24, 5, 5
** Name: BC-4 Type: Displacement/Rotation