*HEADING
: NAFEMS TEST LE2, Cylindrical Shell Bending Patch Test  [S4]
*RESTART,WRITE
*PREPRINT,ECHO=YES,HISTORY=NO,MODEL=NO
*NODE
*NGEN,NSET=EDGECD
*NGEN,NSET=EDGEBC
*NGEN,NSET=EDGEAB
*NGEN,NSET=EDGEAD1
*NSET,NSET=EDGEAD
*NSET,NSET=OUTER
 EDGECD,EDGEBC,EDGEAB,EDGEAD
*NGEN,NSET=INNER
*NSET,NSET=ALL
 INNER,OUTER
*NMAP,NSET=ALL,TYPE=CYLINDRICAL
*ELEMENT,TYPE=S4,ELSET=ALLELS
*MATERIAL,NAME=MAT
*ELASTIC,TYPE=ISOTROPIC
2.1E5,0.3
*SHELL SECTION,MATERIAL=MAT, ELSET=ALLELS
0.01,
*TRANSFORM,TYPE=C,NSET=ALL
*BOUNDARY
EDGEAB,1,6
EDGEAD,ZSYMM
EDGEBC,ZSYMM
*STEP,PERTURB
*STATIC
*CLOAD
 1,6,0.125E3
 3,6,0.25E3
 5,6,0.125E3
*NODE PRINT
*EL FILE,POSITION=AVERAGED AT NODES
 S,
 E,
*EL PRINT,POSITION=AVERAGED AT NODES
 S,
 E,
*END STEP