*HEADING
Plane Stress FeFp
Elements: cps4r, cps3, cps6m, cps8, s4r, s3r, sc8r, m3d4r
Biaxial tension
Marlow model, incompressible, mullins effect
*NODE,NSET=one
**
**
**
*NSET, NSET=SHELL-NODE
*NSET, NSET=SC8R-FRONT
*NSET, NSET=BOT
*NSET, NSET=LEFT
*NSET, NSET=TOP
**63,64,67,68
*NSET, NSET=TOP-1-CPS6M
*NSET, NSET=TOP-1-8NODE
*NSET, NSET=TOP-2-CPS6M
*NSET, NSET=TOP-2-8NODE
*NSET, NSET=TOP-3DEL
*NSET, NSET=RIGHT-3DEL
*NSET, NSET=RIGHT
*NSET, NSET=RIGHT-1-CPS6M
*NSET, NSET=RIGHT-1-8NODE
*NSET, NSET=RIGHT-2-CPS6M
*NSET, NSET=RIGHT-2-8NODE
*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
*SOLID SECTION,ELSET=SOLID,MATERIAL=mat-129
1.
*SHELL SECTION,ELSET=SHELL,MATERIAL=mat-129
1.,5
*MEMBRANE SECTION,ELSET=MEMBRANE,MATERIAL=mat-129
1.,5
*MATERIAL,NAME=mat-129
*HYPERELASTIC,marlow,poisson=0.5
*include, input=heplmu_matprops_bi.inp
*amplitude,name=nominal_stress
0.0,0.0, 10.,2.44444, 20.0,0.0, 40.,3.959985,
60.,0.0, 90.0,6.21102
*STEP,NLGEOM,INC=2000
*STATIC
1.0,90.,,1.0
*BOUNDARY
BOT,2
LEFT,1
SHELL-NODE,3,6
SC8R-FRONT,4,6
*cload, amplitude=nominal_stress
RIGHT,1,0.5
TOP,  2,0.5
TOP-3DEL,2,0.25
RIGHT-3DEL,1,0.25
** for 2nd-order elements
RIGHT-1-CPS6M,1,0.25
RIGHT-2-CPS6M,1,0.50
RIGHT-1-8NODE,1,0.1666666667
RIGHT-2-8NODE,1,0.6666666666
TOP-1-CPS6M,  2,0.25
TOP-2-CPS6M,  2,0.50
TOP-1-8NODE,  2,0.1666666667
TOP-2-8NODE,  2,0.6666666666
*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