*heading
 ANISOTROPIC HYPERELASTIC, holzapfel-ogden
 Simple shear (plane strain), displacement 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.,
  5,2.,0.,1.
  6,3.,0.,1.
  7,3.,1.,1.
  8,2.,1.,1.
 21,4.,0.,
 22,5.,0.,
 23,5.,1.,
 24,4.,1.,
*nset,nset=nz0
 11,12,13,14, 1,2,3,4
*nset,nset=nz1
 15,16,17,18, 5,6,7,8
*nset,nset=ny0
 11,12,15,16, 1,2,5,6, 21,22
*nset,nset=nx1
 12,13,16,17
*nset,nset=ny1
 13,14,17,18, 3,4,7,8
*nset,nset=ny1ple
 23,24
*nset,nset=nx0
 14,11,18,15
*nset, nset=ndisp
 12, 2, 22
*element,type=c3d8h,elset=e_c3d8h
 1,11,12,13,14,15,16,17,18
*element,type=c3d8rh,elset=e_c3d8rh
 2, 1,2,3,4,5,6,7,8
*element,type=cpe4rh,elset=e_cpe4rh
 3, 21,22,23,24
*elset,elset=eall
1,2,3
*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_c3d8h,material=holzapfel-ogden,orientation=ori-1
 1.0,
*solid section,elset=e_c3d8rh,material=holzapfel-ogden,orientation=ori-1,controls=hgctrl
 1.0,
*solid section,elset=e_cpe4rh,material=holzapfel-ogden,orientation=ori-1,controls=hgctrl
 1.0,
*section control, name=hgctrl, hourglass=stiffness

*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
*step,nlgeom=yes
 simple shear
*static
 0.05,1.0,,0.05
*boundary
 ny0,1,2
 ny1,2,2
 ny1ple,2,2
 nz0,3,3
 nz1,3,3
*cload
 ny1,1,278.0e-3
 ny1ple,1,556.0e-3
***boundary
** ny1,1,1,0.2
** ny1ple,1,1,0.2
*output,field,freq=5
*element output, elset=eall
 s, le
*node out, nset=all
 u, rf
*output, history
*element output, elset=eall
s11,s22,s33,s12,le12
*node out, nset=ndisp
 rf1, rf2, rf3
*end step