*HEADING
1 X 4 mesh for cantilever bending problem with CPS6M elements.
**
*NODE
       1,          0.,          0.
       2,        0.75,          0.
       3,         1.5,          0.
       4,        2.25,          0.
       5,          3.,          0.
       6,        3.75,          0.
       7,         4.5,          0.
       8,        5.25,          0.
       9,          6.,          0.
      10,          0.,         0.1
      11,        0.75,         0.1
      12,         1.5,         0.1
      13,        2.25,         0.1
      14,          3.,         0.1
      15,        3.75,         0.1
      16,         4.5,         0.1
      17,        5.25,         0.1
      18,          6.,         0.1
      19,          0.,         0.2
      20,        0.75,         0.2
      21,         1.5,         0.2
      22,        2.25,         0.2
      23,          3.,         0.2
      24,        3.75,         0.2
      25,         4.5,         0.2
      26,        5.25,         0.2
      27,          6.,         0.2
**
**
*ELEMENT, TYPE=CPS6M, ELSET=EALL
       1,      21,      19,       1,      20,      10,      11
       2,       1,       3,      21,       2,      12,      11
       3,       3,       5,      21,       4,      13,      12
       4,      23,      21,       5,      22,      13,      14
       5,      25,      23,       5,      24,      14,      15
       6,       5,       7,      25,       6,      16,      15
       7,       7,       9,      25,       8,      17,      16
       8,      27,      25,       9,      26,      17,      18
**
** eall
**
*SOLID SECTION, ELSET=EALL, MATERIAL=A1,controls=ctr
         0.1,
*section controls,name=ctr,hourglass=stiffness
**
** A1
** Date: 05-Apr-96           Time: 11:38:19
**
*MATERIAL, NAME=A1
**
*ELASTIC, TYPE=ISO
       1.E+7,       1.E-5
**
** step  1,Default
**
*STEP, AMPLITUDE=RAMP, PERTURBATION
Linear Static Analysis
**
This load case is the default load case that always appears
**
*STATIC
**
** fix
**
*BOUNDARY, OP=NEW
       1, 1,,          0.
       1, 2,,          0.
      10, 1,,          0.
      10, 2,,          0.
      19, 1,,          0.
      19, 2,,          0.
**
** load
**
*CLOAD, OP=NEW
       9, 2,        -0.5
      27, 2,        -0.5
**
*NODE FILE
U, 
*OUTPUT,FIELD
*NODE OUTPUT
U,
*EL PRINT
S, 
E, 
*END STEP