*HEADING
 Transfer from Standard to Explicit : hyperfoam
 - Standard analysis
 [base for sx_x_sax1_hfoam]
*RESTART,WRITE
*NODE,NSET=ALL
1, 3.,0.
2, 3.,1.
*NSET,NSET=FIX
1,
*NSET,NSET=DISP
2,
*ELEMENT,TYPE=SAX1,ELSET=ELALL
1,1,2
*SHELL SECTION,ELSET=ELALL,MATERIAL=MAT1
1.0,
*MATERIAL,NAME=MAT1
*HYPERFOAM,N=2,TEST DATA INPUT,POISSON=0.0
** Stress: MPa = N/mm^2
*UNIAXIAL TEST DATA
 -.0217,   -.05
 -.0317,   -.10
 -.0367,   -.15
 -.0402,   -.20                              
 -.0433,   -.25
 -.0467,   -.30
 -.0504,   -.35
 -.0542,   -.40
 -.0604,   -.45
 -.0668,   -.50
 -.0759,   -.55
 -.0909,   -.60
 -.1083,   -.65
 -.1410,   -.70
 -.1933,   -.75
 -.2896,   -.80
*SIMPLE SHEAR TEST DATA      
  .0140, .08, .0046
  .0334, .16, .0166
  .0533, .24, .0366
  .0853, .32, .0573
  .1280, .40, .0817
  .1653, .48, .1098
  .2080, .56, .1394
  .2560, .64, .1666
  .2987, .72, .1904
*DENSITY
** 10 kg/m^3 = 10 N-sec^2/m^4 = 1.E-11 N-sec^2/mm^4
1.E-11, 
**
** step #1
**
*STEP,NLGEOM
*STATIC
.1,1.
*BOUNDARY
FIX,1,2
FIX,6,6
DISP,1,1
DISP,6,6
DISP, 2,2,-0.2
*ENERGY PRINT
*EL PRINT
S,
E,
*EL FILE
S,
E,
*NODE PRINT
U,
RF,
*NODE FILE
U,
RF,
*END STEP