*HEADING
: NAFEMS TEST LE2, Cylindrical Shell Bending Patch Test  [S3R]
*NODE
 1, 1.0, 0.0, 0.0, 1.0, 0.0, 0.0
 5, 1.0, 30.0, 0.0, 1.0, 0.0, 0.0
 21,1.0, 0.0, 0.5, 1.0, 0.0, 0.0
 25,1.0, 30.0, 0.5, 1.0, 0.0, 0.0
 13,1.0, 20.0, 0.3, 1.0, 0.0, 0.0
*NGEN,NSET=EDGEAB
 1,21,5
*NGEN,NSET=EDGECD
 5,25,5
*NGEN,NSET=EDGEAD
 1,5
*NGEN,NSET=EDGEBC
 21,25,
*NGEN
 11,13
 13,15
 3,13,5
 13,23,5
 6,8
 8,10
 16,18
 18,20
*NSET,NSET=NALL,GEN
 1,25
*NMAP,NSET=NALL,TYPE=CYLINDRICAL
0.,0.,0.,0.,0.,1.
1.,0.,0.
*ELEMENT,TYPE=S3R,ELSET=ALLELS
 1,1,3,11
 2,11,3,13
*ELGEN,ELSET=ALLELS
 1,2,2,2,2,10,10
 2,2,2,2,2,10,10
*MATERIAL,NAME=MAT
*ELASTIC,TYPE=ISOTROPIC
2.1E5,0.3
*orientation, name=ori, system=cylindrical
 0.,0.,0., 0.,0.,1.
 1,0.
*SHELL SECTION,MATERIAL=MAT,ELSET=ALLELS, orientation=ori
0.01, 
*TRANSFORM,TYPE=C,NSET=NALL
0.,0.,0.,0.,0.,1.
*BOUNDARY
 EDGEAD,ZSYMM
 EDGEBC,ZSYMM
 EDGEAB,1,6
*RESTART,WRITE
*STEP
*STATIC
*CLOAD
5,6,125.0
15,6,250.0,
25,6,125.0
*EL PRINT,POS=AVERAGED AT NODES
S, 
*EL FILE,POS=AVERAGED AT NODES
S, 
*END STEP