*HEADING
: NAFEMS TEST LE3, Hemispherical Shell with Point Loads  [S8R]
*ELEMENT,TYPE=S8R     ,ELSET=S8_P2
*ELEMENT,TYPE=S8R     ,ELSET=S8_P4
*NODE,NSET=DISPSET
*NODE,NSET=GENSET
*ELSET,ELSET=EALL
S8_P2,S8_P4
*MATERIAL,NAME=A1
*ELASTIC,TYPE=ISO
 6.825E+07,     0.3000,     0.0000
**GENERAL RIGID ELEMENTS
*SHELL SECTION,MATERIAL=A1,ELSET=EALL
 4.000E-02,
*NSET,NSET=XSYM,GEN
*NSET,NSET=YSYM,GEN
*BOUNDARY,OP=NEW
 XSYM,XSYMM
 YSYM,YSYMM
 20801,3,3
 41601,3,3
*STEP
*STATIC
*CLOAD,OP=NEW
20001,     1,  2.000E+00
20009,     2, -2.000E+00
40001,     1,  2.000E+00
40017,     2, -2.000E+00
*NODE PRINT,NSET=DISPSET
 U,
 COORD,
*NODE FILE,NSET=DISPSET
 U,
 COORD,
*OUTPUT,FIELD
*NODE OUTPUT,NSET=DISPSET
U,
COORD,
*EL PRINT,FREQUENCY=0
*END STEP