*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
*DENSITY
 0.01, 
*ELASTIC
 30000., 0.3
*CAP PLASTICITY
15.0, 30.0, 0.1, 0.0005, 0.01
*CAP HARDENING
  2.150, .0
 20.960, .0005
 46.600, .001
 79.670, .0015
126.280, .002
205.950, .0025
311.270, .0028
655.600, .00299
10000., 0.004
*STEP,inc=1000
*static
 0.001,0.05,,0.001
*BOUNDARY,TYPE=DISPLACEMENT
 I1.SOLID_RIGHT,1,1,1.0
**
*OUTPUT,FIELD,freq=1
*ELEMENT OUTPUT
 SDV,
*NODE OUTPUT,NSET=I1.NALL
 U,
*OUTPUT,HISTORY
*NODE OUTPUT,NSET=I1.NALL
 U,RF
*END STEP