*HEADING
: NAFEMS TEST LE3, Hemispherical Shell with Point Loads  [SAXA22]
*NODE
*NGEN,LINE=C
*ELEMENT,TYPE=SAXA22,OFFSET=200
*ELGEN,ELSET=BALL
*NSET,NSET=ZCONSTR
*NSET,NSET=TOP,GENERATE
*NSET,NSET=LOADPTS
*SHELL SECTION,ELSET=BALL,MATERIAL=BALLMT
 .04,3
*MATERIAL,NAME=BALLMT
*ELASTIC
 6.825E7,.3
*EQUATION
*BOUNDARY
 ZCONSTR,2,2
 TOP,1,1
 TOP,6,6
*STEP
*STATIC
*CLOAD
   1,1, 4.
 201,1,-8.
 401,1, 4.
*NODE PRINT,NSET=LOADPTS
 U,
*NODE FILE,NSET=LOADPTS
 U,
 COORD,
*OUTPUT,FIELD
*NODE OUTPUT,NSET=LOADPTS
U,
COORD,
*EL PRINT,FREQUENCY=0
*END STEP