*HEADING THERMAL STRESS IN A CYLINDRICAL SHELL [C3D6T] ** *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 21, 0.1,5.625,0.0 22, 0.1,5.625,0.02 *ELEMENT,TYPE=C3D6T,ELSET=ALLE 1,1,9,11,17,21,22 2,1,11,4,17,22,20 3,17,21,22,5,13,15 4,17,22,20,5,15,8 5,9,2,3,21,18,19 6,9,3,11,21,19,22 7,21,18,19,13,6,7 8,21,19,22,13,7,15 *ELSET,ELSET=QA_TEST ALLE *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 *DENSITY 7800., *CONDUCTIVITY 52., *SPECIFIC HEAT 586., *ELASTIC 200.E9, 0.3 *EXPANSION 1.2E-5, *NSET,NSET=ROTATE 2,3,6,7,9,11,13,15,18,19,21,22 *NSET,NSET=Z1 1,2,5,6,9,13,17,18,21 *NSET,NSET=Z2 3,4,7,8,11,15,19,20,22 *NSET,NSET=RIN 1,2,3,4,9,11 *NSET,NSET=ROUT 5,6,7,8,13,15 *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 2, 21,3,1.0,22,3,1.0 2, 22,3,1.0,20,3,-1.0 ** *BOUNDARY **DISPLACEMENT B.C. ALLN,2 ** *STEP STRESS ANALYSIS USING TEMP DISTRIBUTION *COUPLED TEMPERATURE-DISPLACEMENT,STEADY STATE 1.,1. *BOUNDARY *BOUNDARY ** THERMAL B.C. RIN, 11,11,200.0 ROUT,11,11,100.0 *************************** *OUTPUT,FIELD *ELEMENT OUTPUT Temp,S *NODE OUTPUT NT ************************** ***OUTPUT,HISTORY ***ELEMENT OUTPUT, ELSET=ALLE **Temp,S, *********** *OUTPUT,HISTORY *ENERGY OUTPUT,VAR=ALL ************************ *ENDSTEP