*HEADING
**
** Verification of *HYPERELASTIC, MARLOW with *REBAR LAYER
** 
*PREPRINT, MODEL=YES
*NODE,NSET=ALL
 1,
 2,1.
 3,1.,1.,
 4,0.,1.,
*NSET,NSET=FACE1
 1,2
*NSET,NSET=FACE2
 3
*NSET,NSET=FACE3
 3,4
*NSET,NSET=FACE4
 1,4
*ELEMENT,TYPE=S4R,ELSET=ONE
 1,1,2,3,4
*SHELL SECTION, ELSET=ONE, MATERIAL=MAT1
 1.0,
*REBAR LAYER
 XX,1.0,1.0,0.0,CORD,0.0,1
*MATERIAL,NAME=MAT1
*HYPERFOAM
 5.E5,2.5,0.0
*MATERIAL, NAME=CORD
*HYPERELASTIC,MARLOW
*UNIAXIAL TEST DATA
  0.0, 0.0
  1.5506E5,  0.1338
  2.4367E5,  0.2675
  3.1013E5,  0.3567
  4.2089E5,  0.6242
  5.3165E5,  0.8917
  5.9810E5,  1.1592
  6.8671E5,  1.4268
  8.8608E5,  2.0510
 10.6329E5,  2.5860
 12.4051E5,  3.0318
 16.1709E5,  3.7898
 19.9367E5,  4.3694
 23.4810E5,  4.8153
 27.4684E5,  5.1720
 31.0127E5,  5.4395
 34.5570E5,  5.7070
 38.3228E5,  5.9299
 42.0886E5,  6.0637
 45.6329E5,  6.1975
 49.3987E5,  6.3312
 53.1646E5,  6.4650
 56.9304E5,  6.5541
 64.2405E5,  6.6433
*NSET, NSET=NDISP
 2
*EQUATION
 2,
 FACE2,1,1,NDISP,1,-1
*INITIAL CONDITIONS, TYPE=STRESS, REBAR
 ONE, XX, 20.0E4
*STEP, NLGEOM
 SOLVE INITIAL CONDITIONS
*STATIC
 0.1,1.0
*BOUNDARY
 ALL,1,6
*OUTPUT,FIELD, VARIABLE=PRESELECT
*ELEMENT OUTPUT, ELSET=ONE
 S, LE, NE
*ELEMENT OUTPUT, ELSET=ONE, REBAR
 S,LE,NE,RBFOR
*OUTPUT, HISTORY, VARIABLE=PRESELECT
*ELEMENT OUTPUT, ELSET=ONE
 S11, LE11, NE11
*ELEMENT OUTPUT, ELSET=ONE, REBAR
 S11,LE11,NE11,EE11,RBFOR
*NODE OUT, NSET=NDISP
 RF1
*END STEP
*STEP, NLGEOM
 UNIAXIAL LOADING
*STATIC
 0.01,1.0,,0.01
*BOUNDARY, OP=NEW
 ALL,3,6
 FACE1,2
 FACE4,1
*CLOAD
 NDISP,1,10.0E7
*OUTPUT,FIELD, VARIABLE=PRESELECT
*ELEMENT OUTPUT, ELSET=ONE
 S, LE, NE
*ELEMENT OUTPUT, ELSET=ONE, REBAR
 S,LE,NE,RBFOR
*OUTPUT, HISTORY, VARIABLE=PRESELECT
*ELEMENT OUTPUT, ELSET=ONE
 S11, LE11, NE11
*ELEMENT OUTPUT, ELSET=ONE, REBAR
 S11,LE11,NE11,EE11,RBFOR
*NODE OUT, NSET=NDISP
 RF1
*END STEP