*HEADING
NAFEMS TEST NLE10, COARSE MESH, C3D10M ELEMENTS  --
**
**RESTART, WRITE, FREQUENCY=1
**
*NODE
**
**
*ELEMENT, TYPE=C3D10M, ELSET=EALL
**
** eall
**
*SOLID SECTION, ELSET=EALL, MATERIAL=STEEL
          1.,
**
** steel
** Date: 23-May-96           Time: 17:30:54
**
*MATERIAL, NAME=STEEL
**
*ELASTIC, TYPE=ISO
     2.1E+11,         0.3
**
** step  1,Default
**
*NSET,NSET=ZFIX
*ELSET,ELSET=EOUT
*STEP, AMPLITUDE=RAMP, PERTURBATION
Linear Static Analysis
**
This load case is the default load case that always appears
**
*STATIC
**
** yfix
**
*BOUNDARY
       8, 2,,          0.
       9, 2,,          0.
      16, 2,,          0.
      17, 2,,          0.
      25, 2,,          0.
      26, 2,,          0.
      33, 2,,          0.
      34, 2,,          0.
**
** xfix
**
*BOUNDARY
     173, 1,,          0.
     174, 1,,          0.
     175, 1,,          0.
     182, 1,,          0.
     183, 1,,          0.
     184, 1,,          0.
     190, 1,,          0.
     191, 1,,          0.
**
** curvefix
**
*BOUNDARY
       1, 1,,          0.
       1, 2,,          0.
       4, 1,,          0.
       4, 2,,          0.
       7, 1,,          0.
       7, 2,,          0.
      10, 1,,          0.
      10, 2,,          0.
*BOUNDARY
ZFIX,3,3,0.
**
** load
**
*DLOAD, OP=NEW
       7, P4,       1.E+6
       9, P4,       1.E+6
      17, P2,       1.E+6
      19, P2,       1.E+6
      27, P2,       1.E+6
      29, P2,       1.E+6
      37, P4,       1.E+6
      39, P4,       1.E+6
      47, P2,       1.E+6
      49, P2,       1.E+6
      57, P4,       1.E+6
      59, P4,       1.E+6
**
*NODE PRINT, FREQ=0
U,
*EL PRINT,FREQ=1,ELSET=EOUT,POSITION=AVERAGED AT NODES
S,
**
*EL FILE, POSITION=AVERAGED AT NODES, FREQ=1,ELSET=EOUT
S,
**
*END STEP