*HEADING
EC3KSRSJ: THERMAL STRESS IN A CYLINDRICAL SHELL  [C3D20R]
*NODE,NSET=ALLN,SYSTEM=C
 1, 0.0995,0.0,0.0
 2, 0.0995,11.25,0.0
 3, 0.0995,11.25,0.02
 4, 0.0995,0.0,0.02
 5, 0.1005,0.0,0.0
 6, 0.1005,11.25,0.0
 7, 0.1005,11.25,0.02
 8, 0.1005,0.0,0.02
 9, 0.0995,5.625,0.0
10, 0.0995,11.25,0.01
11, 0.0995,5.625,0.02
12, 0.0995,0.0,0.01
13, 0.1005,5.625,0.0
14, 0.1005,11.25,0.01
15, 0.1005,5.625,0.02
16, 0.1005,0.0,0.01
17, 0.1,0.0,0.0
18, 0.1,11.25,0.0
19, 0.1,11.25,0.02
20, 0.1,0.0,0.02
*ELEMENT,TYPE=C3D20R,ELSET=ALLE
1, 1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,
16,17,18,19,20
*SOLID SECTION,ELSET=ALLE,MATERIAL=STEEL,ORIE=OR1
*ORIENTATION,SYS=CYL,NAME=OR1
 0.0,0.0,0.0, 0.0, 0.0, 1.0
 1, 0.0
*MATERIAL,NAME=STEEL
*ELASTIC
200.E9, 0.3                          
*EXPANSION
1.2E-5, 
*NSET,NSET=ROTATE
2,3,6,7,9,10,11,13,14,15,18,19
*NSET,NSET=Z1
1,2,5,6,9,13,17,18
*NSET,NSET=Z2
3,4,7,8,11,15,19,20
*NSET,NSET=SYMM,GENERATE
1,8,1
10,16,2
17,20,1            
*NSET,NSET=RIN
 1,2,3,4,9,10,11,12
*NSET,NSET=ROUT
 5,6,7,8,13,14,15,16
*TRANSFORM,NSET=ROTATE,TYPE=C
0.,0.,0.,0.,0.,1.
*EQUATION
** RADIAL
2, 
RIN,1,1.0,ROUT,1,-1.0
**AXIAL
2    ,      ,         
RIN,3,1.0,ROUT,3,-1.0
**RADIAL mid nodes
2    ,      
17,1,1.0,5,1,-1.0
2    ,      
18,1,1.0,6,1,-1.0
2    ,      
19,1,1.0,7,1,-1.0
2    ,      
20,1,1.0,8,1,-1.0
**AXIAL mid nodes
2    ,      
17,3,1.0,20,3,1.0
2    ,      
18,3,1.0,19,3,1.0
2    ,      
19,3,1.0,20,3,-1.0
*STEP
STRESS ANALYSIS USING TEMP DISTRIBUTION
*STATIC
*TEMPERATURE,FILE=ec3kdfsj
*BOUNDARY
ALLN, 2
*EL PRINT,ELSET=ALLE
S, 
*OUTPUT,FIELD
*ELEMENT OUTPUT,ELSET=ALLE
S, 
*NODE PRINT
U, 
*ENDSTEP