*HEADING
 Test for passing abaqus material to UEL: plane strain element
*RESTART,WRITE,NUMBER INTERVAL=10
*PREPRINT,MODEL=YES
*PART,NAME=PART1
  *NODE,NSET=NALLUEL
   1,0,0,0
   2,1,0,0
   3,1,1,0
   4,0,1,0
  *NSET,NSET=NALL
   NALLUEL,
  *NSET,NSET=SOLID_BOTTOM
   1,2
  *NSET,NSET=SOLID_LEFT
   1,4
  *NSET,NSET=SOLID_RIGHT
   2,3
  *NSET,NSET=SOLID_ALL
   1,2,3,4
  *****
  ***** PLANE STRAIN
  *****
  *USER ELEMENT, TYPE=U1, NODES=4, COORDINATES=2, VAR=32, 
   INTEGRATION=4,TENSOR=PSTRAIN
   1,2
  *ELEMENT,TYPE=U1,ELSET=SOLID
   1, 1,2,3,4
  *UEL PROPERTY, ELSET=SOLID, MATERIAL=MAT
  **************************************
  *ELSET,ELSET=EALL
   SOLID,
*END PART
*ASSEMBLY,NAME=ASSEM1
  *INSTANCE,NAME=I1,PART=PART1
  *END INSTANCE
*END ASSEMBLY
*BOUNDARY
 I1.SOLID_BOTTOM,2,2
 I1.SOLID_LEFT,1,1
 I1.SOLID_ALL,3,3
***************************************
*MATERIAL,NAME=MAT
*HYPERFOAM,N=2,TEST DATA INPUT,POISSON=0.0,MODULI=INSTANTANEOUS
*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
*VISCOELASTIC,TIME=RELAXATION TEST DATA
*SHEAR TEST DATA,SHRINF=0.5000
 1.0000, 0.0001
 0.9695, 0.001
 0.9417, 0.002
 0.8722, 0.005
 0.7913, 0.010
 0.7043, 0.020
 0.6233, 0.050
 0.5736, 0.100
 0.5271, 0.200
 0.5013, 0.500
 0.5000, 1.000
*DENSITY
 1.E-11,
*STEP,inc=1000,NLGEOM=YES
*static
 0.001,0.05,,0.001
*BOUNDARY,TYPE=DISPLACEMENT
 I1.SOLID_RIGHT,1,1,1.0
**
*OUTPUT,FIELD,freq=1
*NODE OUTPUT,NSET=I1.NALL
 U,
*OUTPUT,HISTORY
*NODE OUTPUT,NSET=I1.NALL
 U,
 RF,
*END STEP