*HEADING
  - HYPERFOAM, FRQ DOMAIN VISCOELASTICITY
*PREPRINT,MODEL=YES
*NODE,NSET=ALL
1,
2,1.
3,1.,1.,
4,0.,1.,
5,0.,0.,1.
6,1.,0.,1.
7,1.,1.,1.
8,0.,1.,1.
**
11,10.,0.,0.
12,11.,0.,0.
13,11.,1.,0.
14,10.,1.,0.
15,10.,0.,1.
16,11.,0.,1.
17,11.,1.,1.
18,10.,1.,1.
*NSET,NSET=FACE1
1,2,3,4,11,12,13,14
*NSET,NSET=FACE2
5,6,7,8,15,16,17,18
*NSET,NSET=FACE3
1,2,5,6,11,12,15,16
*NSET,NSET=FACE4
2,3,6,7,12,13,16,17
*NSET,NSET=FACE5
3,4,7,8,13,14,17,18
*NSET,NSET=FACE6
4,1,8,5,14,11,18,15
*ELEMENT,TYPE=C3D8R,ELSET=REF
1,1,2,3,4,5,6,7,8
*ELEMENT,TYPE=C3D8R,ELSET=TEST
10,11,12,13,14,15,16,17,18
*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-2,1.161E-2,-3.21E-2,1.
1.775E-3,-5.116E-3,1.775E-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
2.722676325e-03,0.242039143,1.,-0.25
4.162576126e-04,0.235711089,100.,-0.25
2.921712435e-03,0.259732963,1.,-0.1
4.466873478e-04,1.252942308,100.,-0.1
4.26865942971e-03,0.379473159878,1.,0.
6.52615890373e-04,0.36955192718,100.,0.
*VISCOELASTIC,FREQUENCY=TABULAR,PRELOAD=VOLUMETRIC
1.778684496e-03,0.158120608,1.,1.
2.719349682e-04,0.153986584,100.,1.
1.984962025e-03,0.176458165,1.,0.919168874
3.034717997e-04,0.171844710,100.,0.919168874
2.565853073e-03,0.228097929,1.,0.794422580
3.922815853e-04,0.222134365,100.,0.794422580
*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,-0.1
*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,-0.25
*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