*HEADING
: ASYMMETRIC INTERAL AND EXTERNAL PRESSURE LOADS  [CAXA43]
** 6-IN LONG CYLINDER OF 2-IN & 6-IN INNER AND OUTER RADII (20X1 MESH)
*NODE
1,2.,0.
21,6.,0.
201,2.,6.
221,6.,6.
*NGEN,NSET=BOT0
1,21
*NGEN,NSET=TOP0
201,221
*NFILL,NSET=P000
BOT0,TOP0,2,100
*ELEMENT,TYPE=CAXA43,OFFSET=1000,ELSET=ALL
1,1,2,202,201
*ELGEN,ELSET=ALL
1,20,1,1
*SOLID SECTION,ELSET=ALL,MATERIAL=STEEL
*MATERIAL,NAME=STEEL
*ELASTIC
30.E6,.33
*EXPANSION
0.0001, 
*NSET,NSET=BOTTOM,GEN
1,21
1001,1021
2001,2021
3001,3021
*NSET,NSET=TOP,GEN
201,221
1201,1221
2201,2221
3201,3221
*NSET,NSET=L1-000,GEN
1,201,100
*NSET,NSET=L1-060,GEN
1001,1201,100
*NSET,NSET=L1-120,GEN
2001,2201,100
*NSET,NSET=L1-180,GEN
3001,3201,100
*NSET,NSET=L1
L1-000,L1-060,L1-120,L1-180
*NSET,NSET=L2,GEN
11,211,100
1011,1211,100
2011,2211,100
3011,3211,100
*NSET,NSET=L3,GEN
21,221,100
1021,1221,100
2021,2221,100
3021,3221,100
*ELSET,ELSET=INWALL
1, 
*ELSET,ELSET=OUTWALL
20, 
*NSET,NSET=NFILE
1,21, 1001,1021, 2001,2021, 3001,3021
201,221, 1201,1221, 2201,2221, 3201,3221
*ELSET,ELSET=EFILE
1,2,19,20
*STEP
*STATIC
*BOUNDARY
L1-000,1,,-9.9853946E-4
TOP,2,2
BOTTOM,2,2
*DLOAD
INWALL,P4NU
OUTWALL,P2NU
*EL FILE,ELSET=EFILE,POSITION=AVERAGED AT NODES
S, 
*NODE FILE,NSET=NFILE
U,RF
*ENERGY PRINT
*EL PRINT,ELSET=EFILE,POSITION=AVERAGED AT NODES
S, 
E, 
*NODE PRINT,NSET=NFILE,TOTAL=NO
COORD,U1,U2,RF1,RF2
** *NODE PRINT,NSET=L1,TOTAL=NO
** COORD,U1,U2,RF1,RF2
** *NODE PRINT,NSET=L2,TOTAL=NO
** COORD,U1,U2,RF1,RF2
** *NODE PRINT,NSET=L3,TOTAL=NO
** COORD,U1,U2,RF1,RF2
*END STEP