*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
*ELASTIC
200.E3,.3
*PLASTIC, HARDENING=COMBINED, DATA TYPE=PARAMETERS,NUMBERBACKSTRESS=3
200., 1.111E4,34.65, 5.555E3,34.65, 5.555E3,0.0
*CYCLIC HARDENING, PARAMETERS
200., 0., 0.
*Density
 2700
*STEP,inc=1000
*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