*HEADING
 TEMPERATURE LOADING COMPOSITE SHELLS, DS3 - INPUT DECK: XTMPCST3.INP
 STRUCTURAL PROBLEM
*NODE
1, 300.,0.,0.
17, 300.,0.,150.
401, 900.,0.,0.
417, 900.,0.,150.
*NGEN,NSET=LOADB
1,17
*NGEN,NSET=BND3
401,417
*NGEN,NSET=BND2
1,401,100
*NGEN,NSET=BND4
17,417,100
*NFILL,NSET=ALL
BND2,BND4,4,4
*ELEMENT,TYPE=S3R, ELSET=EALL
1,1,5,105
2,1,105,101
*ELGEN,ELSET=ALELL
1,4,4,2,4,100,8
2,4,4,2,4,100,8
*ELSET,ELSET=PRINT
1,2,11,12,21,22,31,32
*SHELL SECTION,COMPOSITE,TEMPERATURE=3,ELSET=ALELL
0.9,5,MAT1
1.9,5,MAT2
1.2,5,MAT3
*MATERIAL,NAME=MAT1
*CONDUCTIVITY
5., 
*ELASTIC
3.0E6,0.3
*EXPANSION
1E-5, 
*MATERIAL,NAME=MAT2
*CONDUCTIVITY
15., 
*ELASTIC
3.0E6,0.3
*EXPANSION
1E-5, 
*MATERIAL,NAME=MAT3
*CONDUCTIVITY
7., 
*ELASTIC
3.0E6,0.3
*EXPANSION
1E-5, 
*INITIAL CONDITIONS,TYPE=TEMPERATURE,FILE=xtmpcst3,STEP=1,INC=1
*STEP
*STATIC
*BOUNDARY
ALL,ENCASTRE
*TEMPERATURE,FILE=xtmpcst3,BSTEP=1,BINC=1,ESTEP=1,EINC=1
*NODE PRINT
NT, 
RF, 
*NODE FILE
NT, 
*EL PRINT,POSITION=INTEGRATION POINTS,ELSET=PRINT
1,2,3,4,5,6,7,8,9,10,11,12,13,14,15
TEMP, 
*EL FILE,POSITION=INTEGRATION POINTS,ELSET=PRINT
1,2,3,4,5,6,7,8,9,10,11,12,13,14,15
TEMP, 
*FILE FORMAT,ZERO INCREMENT,ASCII
*END STEP