*HEADING
Plane Stress FeFp
Elements: cps4r, cps3, cps6m, cps8, s4r, s3r
Simple shear, with orientation
Ogden model, incompressible, mullins effect
**
**We should not compare the results between shells
**and CPS elements when the orientation rotates; they
**have different element bases.
**
*NODE,NSET=one
1,
2,1.
3,1.,1.,
4,0.,1.,
**
11,2.
12,3.
13,3.,1.
14,2.,1.
**
21,4.0,0.0
22,5.0,0.0
23,5.0,1.0
24,4.0,1.0
25,4.5,0.0
26,5.0,0.5
27,4.5,1.0
28,4.0,0.5
29,4.5,0.5
**
31,6.0,0.0
32,7.0,0.0
33,7.0,1.0
34,6.0,1.0
35,6.5,0.0
36,7.0,0.5
37,6.5,1.0
38,6.0,0.5
**
41,0.0,3.0
42,1.0,3.0
43,1.0,4.0
44,0.0,4.0
**
51,2.0,3.0
52,3.0,3.0
53,3.0,4.0
54,2.0,4.0
**
*NSET, NSET=SHELL-NODE
41,42,43,44
51,52,53,54
*NSET, NSET=BOT
1,2
11,12
21,22,25
31,32,35
41,42
51,52
*NSET, NSET=LEFT
1,4
11,14
21,24,28
31,34,38
41,44
51,54
*NSET, NSET=TOP
3,4
13,14
43,44
53,54
23,24,27
33,34,37
*NSET, NSET=RIGHT
2,3
12,13
42,43
52,53
22,23,26
32,33,36
*ELEMENT,TYPE=CPS4,ELSET=SOLID
1,1,2,3,4
*ELEMENT,TYPE=CPS3,ELSET=SOLID
2,11,12,13
3,11,13,14
*ELEMENT,TYPE=CPS6M,ELSET=SOLID
21,21,22,23,25,26,29
22,21,23,24,29,27,28
*ELEMENT,TYPE=CPS8,ELSET=SOLID
31,31,32,33,34,35,36,37,38
*ELEMENT,TYPE=S4R,ELSET=SHELL
41,41,42,43,44
*ELEMENT,TYPE=S3R,ELSET=SHELL
51,51,52,53
52,51,53,54
*ELSET, ELSET=ALLE
 SOLID
 SHELL
*orientation,name=ori1
5.,1.,0., -1.,5.,0.,
3,0
*SOLID SECTION,ELSET=SOLID,MATERIAL=mat-129,ori=ori1
1.
*SHELL SECTION,ELSET=SHELL,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.,0.4, 20.,0.0, 40.,0.8,
50.,0.0, 70.,1.6
**---------
*equation
2
36,2,1.0,38,2,-1.0
2
36,1,1.0,38,1,-1.0
2
26,2,1.0,28,2,-1.0
2
26,1,1.0,28,1,-1.0
**---------
*STEP,NLGEOM,INC=2000
*STATIC
0.5,70.,,0.5
*BOUNDARY
BOT,1,2
TOP,2,2
SHELL-NODE,3,6
*BOUNDARY, AMPLITUDE=nominal_strain
TOP, 1,1,1.0
*output,history,freq=1
*element output, elset=ALLE
 S22
*output,field,freq=1000
*node output
 u,rf
*element output
 S,LE,PE
 PEEQ
*END STEP