*HEADING
  NAFEMS TEST LE3, Hemispherical Shell with Point Loads  [SC8R]
  Using *SHELL GENERAL SECTION
*NODE
*ELEMENT,TYPE=SC8R     ,ELSET=S4_P2
*ELEMENT,TYPE=SC8R     ,ELSET=S4_P4
*ELSET,ELSET=EALL
 S4_P2,S4_P4
*MATERIAL,NAME=A1
*ELASTIC,TYPE=ISO
 6.825E+07,     0.3000,     0.0000
*SHELL GENERAL SECTION,MATERIAL=A1,ELSET=EALL
 4.000E-02,
*NSET,NSET=ZCONSTR
*NSET,NSET=XSYM
*NSET,NSET=YSYM
*NSET,NSET=DISPSET_FINE
*NSET,NSET=DISPSET_COARSE
*NSET,NSET=DISPSET
 DISPSET_FINE,DISPSET_COARSE
*BOUNDARY,OP=NEW
 XSYM,XSYMM
 YSYM,YSYMM
 ZCONSTR,3,3
*RESTART,WRITE
*STEP,PERTURB
*STATIC
*CLOAD,OP=NEW
    8,     1,  1.000E+00
 1008,     1,  1.000E+00
   18,     2, -1.000E+00
 1018,     2, -1.000E+00
   64,     1,  1.000E+00
 1064,     1,  1.000E+00
   92,     2, -1.000E+00
 1092,     2, -1.000E+00
*NODE PRINT,NSET=DISPSET_FINE
 U,
*NODE PRINT,NSET=DISPSET_COARSE
 U,
*NODE FILE,NSET=DISPSET
 U,
*OUTPUT,FIELD
*NODE OUTPUT
 U,
*ELEMENT OUTPUT
 S,
*END STEP