*heading
 ANISOTROPIC HYPERELASTIC, holzapfel-ogden
 Plane stress, tension, load control
*preprint, model=yes
*node,nset=all
 11,
 12,1.
 13,1.,1.,
 14,0.,1.,
 15,0.,0.,1.
 16,1.,0.,1.
 17,1.,1.,1.
 18,0.,1.,1.
  1,2.,0.,
  2,3.,0.,
  3,3.,1.,
  4,2.,1.,
 21,4.,0.,
 22,5.,0.,
 23,5.,1.,
 24,4.,1.,
 31,6.,0.,
 32,7.,0.,
 33,7.,1.,
 34,6.,1.,
*nset,nset=nz0
 11,12,13,14, 21,22,23,24, 31,32,33,34
*nset,nset=ny0
 11,12,15,16, 1,2, 21,22, 31,32
*nset,nset=nx1
 12,13,16,17
*nset,nset=nx1ps
 2,3, 22,23, 32,33
*nset,nset=nx0
 11,14,15,18, 1,4, 21,24, 31,34
*nset,nset=nrot
21,22,23,24
*nset, nset=nout_u
3, 23, 33
*nset, nset=nout_rf
2, 22, 32
*element,type=c3d8rh,elset=e_c3d8rh
 1,11,12,13,14,15,16,17,18
*element,type=cps4,elset=e_cps4
 2, 1,2,3,4
*element,type=s4r,elset=e_s4r
 3, 21,22,23,24
*element,type=m3d4r,elset=e_m3d4r
 4, 31,32,33,34
*elset,elset=eall
1,2,3,4
*orientation,name=ori-1,local directions=2
 1.0,0.0,0.0,0.0,1.0,0.0
 3,0.0
 0.643055,0.76582,0.0
 0.643055,-0.76582,0.0
*solid section,elset=e_c3d8rh,material=holzapfel-ogden,orientation=ori-1
 1.0,
*solid section,elset=e_cps4,material=holzapfel-ogden,orientation=ori-1
 1.0,
*shell section,elset=e_s4r,material=holzapfel-ogden,orientation=ori-1
 1.0,
*membrane section,elset=e_m3d4r,material=holzapfel-ogden,orientation=ori-1
 1.0,
*material,name=holzapfel-ogden
*Damping, alpha=320.
*density
 1.06e-09,
*anisotropic hyperelastic,definition=holzapfel-ogden, local directions=2
**   a,       b,      af,      bf,      as,      bs,     afs,     bfs
 0.00099993,  3.143938, 0.004696677,  12.33052484,   0.002673816,  9.057685378,      9.0234e-7,  0.000670602
**   D
  0.0
*amplitude, name=amp1, def=smooth
0.0,0.0, 1.0,1.0
*step,nlgeom=yes
 tension
*static
 0.05,1.0,,0.05
*boundary
 nx0,1,1
 ny0,2,2
 nz0,3,3
nrot,4,6
*cload, amp=amp1
 nx1,1,55.6e-3
 nx1ps,1,111.2
*output,field,freq=5
*element output, elset=eall
 s, le
*node out, nset=all
 u, rf
*output, history
*element output, elset=eall
s11,le11
*node out, nset=nout_rf
rf1
*node out, nset=nout_u
u1
*end step