*Heading
 AXISYMMETRIC TIRE PROBLEM
 USED AS BASE STATE FOR am_tireair_acax4_ver.inp
 USED AS BASE STATE FOR am_tire_ac3d8.inp
*preprint,model=yes,HIST=yes
*Node,nset=tire
     51,      136.4036,       11.889
     52,      143.1992,      14.6474
     53,          110.,          20.
     54,          110.,          15.
     55,          141.,           0.
     56,          138.,           0.
     57,          145.,           0.
     58,       139.674,      13.2026
     59,      140.3605,      19.6142
     60,      135.6735,      23.0525
     61,      130.2496,      24.9445
     62,      124.5124,      25.5826
     63,      118.8792,      24.6712
     64,      114.0135,      22.4476
     65,          110.,      18.3503
     66,      114.7767,      17.7824
     67,      119.5534,      19.8569
     68,      124.2259,      20.8643
     69,      128.6882,      20.5012
     70,      132.2826,      18.4378
     71,      134.7612,       15.401
     72,       137.354,      8.03714
     73,      137.8012,      4.04762
     74,      144.8265,      4.65146
     75,      144.3889,      9.49225
     76,      137.5026,       17.175
     77,      134.1037,      20.3423
     78,      129.5284,      22.3786
     79,      124.3888,      22.9216
     80,      119.3783,      22.0249
     81,        114.65,      20.0485
     82,      140.7527,      8.70145
     83,      141.1813,      4.32418
*Element, type=CAX4H,elset=tire
 51, 51, 58, 76, 71
 52, 58, 52, 59, 76
 53, 71, 76, 77, 70
 54, 76, 59, 60, 77
 55, 70, 77, 78, 69
 56, 77, 60, 61, 78
 57, 69, 78, 79, 68
 58, 78, 61, 62, 79
 59, 68, 79, 80, 67
 60, 79, 62, 63, 80
 61, 67, 80, 81, 66
 62, 80, 63, 64, 81
 63, 66, 81, 65, 54
 64, 81, 64, 53, 65
 65, 52, 58, 82, 75
 66, 58, 51, 72, 82
 67, 75, 82, 83, 74
 68, 82, 72, 73, 83
 69, 74, 83, 55, 57
 70, 83, 73, 56, 55
*Solid Section, elset=tire, material=rubber
1.,
*NSET,NSET=nout
 53 , 54, 65, 69, 70
*Nset, nset=SYMS
 55,  56, 57
*Nset, nset=CENT
  53,  54, 65
*Elset, elset=air_S2
 17,  18, 19
*Elset, elset=liner_S4, generate
  51,  63,   2
*Elset, elset=liner_S2, generate
 66,  70,   2
**
*Elset, elset=liner_S4, generate
  51,  63,   2
*Elset, elset=liner_S2, generate
 66,  70,   2
*Surface, type=ELEMENT, name=liner
 liner_S4, S4
 liner_S2, S2
**TRANSFORM,TYPE=C,NSET=AIR
** 0.0, 0.0, 0.0,  0.0, 0.0, 1.0
*Material, name=rubber
*Hyperelastic
 100., 0.
*Density
 1.1e-3,
** 
*Boundary
 SYMS, YSYMM
 CENT, 1, 1
*RESTART,WRITE
** ----------------------------------------------------------------
*Step, name=Step-1, nlgeom
*Static
 1.0, 1.0
** 
*Dsload
 liner, P, -1.5
*Output, field,freq=1
*NODE OUTPUT
 U
*Output, history,fre=1
*NODE OUTPUT,NSET=NOUT
 U,
*El Print, freq=100
 S
*Node Print, freq=100
 U
*End Step