*HEADING
: NAFEMS TEST LE1, Plane Stress Elements -- Elliptic Membr.  [CPS8R]
*NODE,NSET=EL1
*NSET,NSET=XSYM,GEN
*NSET,NSET=YSYM,GEN
*ELEMENT,TYPE=CPS8R, ELSET=EALL
*ELGEN, ELSET=EALL
*MATERIAL,NAME=MATPROP
*ELASTIC
 210.0E9,0.3
*ELSET,ELSET=LOAD
*SOLID SECTION,MATERIAL=MATPROP, ELSET=EALL
 0.1,
*BOUNDARY
 XSYM,XSYMM
 YSYM,YSYMM
*ELSET,ELSET=OUT
*ELSET,ELSET=PRINT
*STEP
*STATIC
*DLOAD
 LOAD,P3, -10.0E6
*NODE PRINT,FREQ=0
*EL PRINT,ELSET=PRINT, POSITION=AVERAGED AT NODES
 S,
*EL FILE,ELSET=PRINT, POSITION=AVERAGED AT NODES
 S,
*END STEP