*HEADING
THERMAL STRESS IN A CYLINDRICAL SHELL  [S4RT]
The end temperatures should be: NT11=100;
NT12=125;NT13=150;NT14=175;NT15=200
The Analytical stress value is 171.43 MPa
(the /explicit solution is about 170.3 MPa at SNEG
and 172.5 at SPOS); see the verification Manual
*NODE,NSET=ALLN,SYSTEM=C
 1, 0.1,0.0,0.0
 2, 0.1,0.0,0.02
 3, 0.1,11.25,0.02
 4, 0.1,11.25,0.0
*ELEMENT,TYPE=S4RT,ELSET=ALLE
1, 1,2,3,4
*SHELL SECTION,ELSET=ALLE,MATERIAL=STEEL
0.001,5
*Elset,elset=qa_test
alle
*nset,nset=qa_test
alln
*MATERIAL,NAME=STEEL
*DENSITY
7800., 
*CONDUCTIVITY
52., 
*SPECIFIC HEAT
586., 
*ELASTIC
200.E9, 0.3
*EXPANSION
1.2E-5, 
*NSET,NSET=ROTATE
3,4
*NSET,NSET=SYMM
1,2,3,4
*TRANSFORM,NSET=ROTATE,TYPE=C
0.,0.,0.,0.,0.,1.
*Amplitude,name=ramp
0,0,0.01,1
*STEP
*DYNAMIC TEMPERATURE-DISPLACEMENT, Explicit
,0.06
*BOUNDARY,amp=ramp
ALLN, 11,11, 100.
ALLN, 15,15, 200.
*BOUNDARY
SYMM, 2
SYMM, 4
SYMM, 6
1, 3
4, 3
1, 5
2, 5
3, 5
4, 5  
*****
*OUTPUT,FIELD,NUMBER INTERVAL=4
*ELEMENT OUTPUT
1,2,3,4,5
Temp,S
*NODE OUTPUT
NT, U
****
*OUTPUT,FIELD,NUMBER INTERVAL=1
*ELEMENT OUTPUT, ELSET=QA_TEST
MisesMax
*NODE OUTPUT,NSET=QA_TEST
NT
***
*OUTPUT,HISTORY,TIME INTERVAL=0.003
*node output,nset=alln
NT,
*ENERGY OUTPUT,VAR=ALL
***
*ENDSTEP