*HEADING
: NAFEMS TEST LE1, Plane Stress Elements -- Elliptic Membr.  [CPS4]
*RESTART,WRITE
*NODE, NSET=CF000
*ELEMENT, TYPE=CPS4, ELSET=M001P001
*ELSET,ELSET=LOAD
*ELSET,ELSET=PR
*SOLID SECTION, ELSET=M001P001, MATERIAL=M001P001
0.1000    ,     5
*MATERIAL, NAME=M001P001
*ELASTIC, TYPE=ISO
0.2100E+06, 0.3000    , 0.0000E+00
*STEP, AMP=RAMP
LOAD CASE     1
*STATIC
*DLOAD, OP=NEW
 LOAD,P3,-10.0
*BOUNDARY, OP=NEW
    1,     1,      , 0.0000E+00
    2,     1,      , 0.0000E+00
    3,     1,      , 0.0000E+00
   10,     2,      , 0.0000E+00
   11,     2,      , 0.0000E+00
   12,     2,      , 0.0000E+00
*EL PRINT,POS=AVERAGED AT NODES
*EL FILE, ELSET=PR, POSITION=AVERAGED AT NODES
S,
*NODE FILE, GLOBAL=YES
U,
*OUTPUT,FIELD
*NODE OUTPUT
U,
*END STEP