*HEADING
: NAFEMS TEST LE2, Cylindrical Shell Bending Patch Test  [SC8R]
*PREPRINT,ECHO=YES,HISTORY=NO,MODEL=NO
*NODE
 1,    0.995,      10.,  0.0,   1.,  0.,  0.
 5,    0.995,      10.,  0.5,   1.,  0.,  0.
 9,    0.995,       0.,  0.5,   1.,  0.,  0.
 13,   0.995,       0.,  0.0,   1.,  0.,  0.
 17,   0.995,      10.,  0.0,   1.,  0.,  0.
 101,  0.995,  6.66667,  0.3,   1.,  0.,  0.
 1001, 1.005,      10.,  0.0,   1.,  0.,  0.
 1005, 1.005,      10.,  0.5,   1.,  0.,  0.
 1009, 1.005,       0.,  0.5,   1.,  0.,  0.
 1013, 1.005,       0.,  0.0,   1.,  0.,  0.
 1017, 1.005,      10.,  0.0,   1.,  0.,  0.
 1101, 1.005,  6.66667,  0.3,   1.,  0.,  0.
*NGEN,NSET=EDGECD
 1,5
 1001,1005
*NGEN,NSET=EDGEBC
 5,9
 1005,1009
*NGEN,NSET=EDGEAB
 9,13
 1009,1013
*NGEN,NSET=EDGEAD1
 13,17
 1013,1017
*NSET,NSET=EDGEAD
 1,13,14,15,16
 1001,1013,1014,1015,1016
*NSET,NSET=OUTER
 EDGECD,EDGEBC,EDGEAB,EDGEAD
*NGEN,NSET=INNER
 1,101,50
 3,101,49
 5,101,48
 7,101,47
 9,101,46
 11,101,45
 13,101,44
 15,101,43
 1001,1101,50
 1003,1101,49
 1005,1101,48
 1007,1101,47
 1009,1101,46
 1011,1101,45
 1013,1101,44
 1015,1101,43
*NSET,NSET=ALL
 INNER,OUTER
*NMAP,NSET=ALL,TYPE=CYLINDRICAL
0.,0.,0.,0.,0.,1.
1.,0.,0.
*ELEMENT,TYPE=SC8R,ELSET=ALLELS
1,  1,3,101,15, 1001, 1003, 1101, 1015
2,  3,5,7,101, 1003, 1005, 1007, 1101
3,  101,7,9,11, 1101, 1007, 1009, 1011
4,  15,101,11,13, 1015, 1101, 1011, 1013
*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,CONTROLS=HGC, orientation=ori
0.01, 
*SECTION CONTROLS,NAME=HGC,HOURGLASS=ENHANCED
*TRANSFORM,TYPE=C,NSET=ALL
0.,0.,0.,0.,0.,1.
*BOUNDARY
EDGEAB,1,3
EDGEAD,ZSYMM
EDGEBC,ZSYMM
*STEP,PERTURB
*STATIC
*CLOAD
 1,2,-0.125E5
 3,2,-0.25E5
 5,2,-0.125E5
 1001,2,+0.125E5
 1003,2,+0.25E5
 1005,2,+0.125E5
*OUTPUT, FIELD
*ELEMENT OUTPUT
 S,
*OUTPUT, FIELD
*ELEMENT OUTPUT, POSITION=NODES
 S,
*END STEP