*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
  *NSET,NSET=NALL
   NALLUEL,
  *NSET,NSET=SOLID_BOTTOM
  *NSET,NSET=SOLID_LEFT
  *NSET,NSET=SOLID_RIGHT
  *NSET,NSET=SOLID_ALL
  *****
  ***** PLANE STRAIN
  *****
  *USER ELEMENT, TYPE=U1, NODES=4, COORDINATES=2, VAR=32,
   INTEGRATION=4,TENSOR=PSTRAIN
  *ELEMENT,TYPE=U1,ELSET=SOLID
  *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
*SIMPLE SHEAR TEST DATA
*VISCOELASTIC,TIME=RELAXATION TEST DATA
*SHEAR TEST DATA,SHRINF=0.5000
*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