*HEADING
Plane Stress FeFp
Elements: cps4r, cps3, cps6m, cps8, s4r, s3r, sc8r, m3d4
Biaxial tension with orientation
Ogden model, incompressible, mullins effect
*NODE,NSET=one
**
**
**
*NSET, NSET=SHELL-NODE
*NSET, NSET=BOT
*NSET, NSET=LEFT
*NSET, NSET=TOP
*NSET, NSET=RIGHT
*ELEMENT,TYPE=CPS4R,ELSET=SOLID
*ELEMENT,TYPE=CPS3,ELSET=SOLID
*ELEMENT,TYPE=CPS6M,ELSET=SOLID
*ELEMENT,TYPE=CPS8,ELSET=SOLID
*ELEMENT,TYPE=S4R,ELSET=SHELL
*ELEMENT,TYPE=S3R,ELSET=SHELL
*ELEMENT,TYPE=SC8R,ELSET=SHELL
*ELEMENT,TYPE=M3D4R,ELSET=MEMBRANE
*ELSET, ELSET=ALLE
 SOLID
 SHELL
*orientation,name=ori1
*SOLID SECTION,ELSET=SOLID,MATERIAL=mat-129,ori=ori1
1.
*SHELL SECTION,ELSET=SHELL,MATERIAL=mat-129,ori=ori1
1.,5
*MEMBRANE SECTION,ELSET=MEMBRANE,MATERIAL=mat-129,ori=ori1
1.,5
*MATERIAL,NAME=mat-129
*HYPERELASTIC,ogden, n=3,test
*include, input=heplmu_matprops.inp
*amplitude,name=nominal_strain
0.0,0.0, 10.,0.186595, 20.,0.006786, 40.,0.388704,
50.,0.013413, 80.,1.0
*STEP,NLGEOM,INC=2000
*STATIC
0.5,80.,,0.5
*BOUNDARY
BOT,2
LEFT,1
SHELL-NODE,3,6
*BOUNDARY, AMPLITUDE=nominal_strain
RIGHT,1,1,1
TOP,  2,2,0.5
*output,history,freq=2
*element output, elset=ALLE
 S22
*output,field,freq=1000
*node output
 u,rf
*element output
 S,LE,PE
 PEEQ
*END STEP