*HEADING
  - HYPERELASTICITY (POLYNOMIAL), FRQ DOMAIN VISCOELASTICITY
*PREPRINT,MODEL=YES
*NODE,NSET=ALL
**
*NSET,NSET=FACE1
*NSET,NSET=FACE2
*NSET,NSET=FACE3
*NSET,NSET=FACE4
*NSET,NSET=FACE5
*NSET,NSET=FACE6
*ELEMENT,TYPE=C3D8R,ELSET=REF
*ELEMENT,TYPE=C3D8R,ELSET=TEST
*SOLID SECTION,ELSET=REF,MATERIAL=POLY1
*MATERIAL,NAME=POLY1
*DENSITY
8.E-7,
*HYPERFOAM,N=2
0.167099, 9.00665, 2.153721E-05, -4.86940, 0.1, 0.2
*VISCOELASTIC,FREQUENCY=TABULAR
1.161E-2,-3.21E-2,,,1.
1.775E-3,-5.116E-3,,,100.0
*SOLID SECTION,ELSET=TEST,MATERIAL=POLY2
*MATERIAL,NAME=POLY2
*DENSITY
8.E-7,
*HYPERFOAM,N=2
0.167099, 9.00665, 2.153721E-05, -4.86940, 0.1, 0.2
*VISCOELASTIC,FREQUENCY=TABULAR,PRELOAD=UNIAXIAL
3.077460322e-03,0.3762620237,1.,0.
4.772892248e-04,0.369048695,100.,0.
0.010413423,1.273184789,1.,0.25
1.615037773e-03,1.248776531,100.,0.25
0.082257708,10.05714085,1.,0.75
0.012757505,9.864335142,100.,0.75
2.332535727,285.1847048,1.,2.
0.36175744,279.7174215,100.,2.
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
1.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
100.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,NLGEOM,INC=20
UNIAXIAL TENSION
*STATIC,DIRECT
1.,20.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.25
*EL PRINT,F=10
S,
NE,
*NODE PRINT,F=10
U,RF
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
1.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
100.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,NLGEOM,INC=20
UNIAXIAL TENSION
*STATIC,DIRECT
1.,20.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.75
*EL PRINT,F=10
S,
NE,
*NODE PRINT,F=10
U,RF
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
1.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
100.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,NLGEOM,INC=20
UNIAXIAL TENSION
*STATIC,DIRECT
1.,20.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,2.0
*EL PRINT,F=10
S,
NE,
*NODE PRINT,F=10
U,RF
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
1.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP
*STEP,PERTURBATION
*STEADY STATE DYNAMICS,DIRECT
100.
*BOUNDARY,OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,0.1
*EL PRINT
S,
E,
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,NE
*END STEP