*HEADING
QUENCHING OF AN INFINITE PLATE                
** converted deck to parts & assembly
*** Heat transfer run quenchplate_dc2d4 uses DC2D4 (first-order) elements.
*** Thermal stress analysis uses CAX8R (second-order) elements.
*** Temperature interpolated to the midside nodes.
**  requires quenchplate_dc2d4.fil results file.
**
** PARTS
**
*Part, name=DUMMY
*NODE
1,
81,,18
101,.5
181,.5,18
201,1.
281,1.,18
*NGEN,NSET=ALL
1,81,4
101,181,4
201,281,4
*NSET,NSET=RAXIS
1,101,201
*NSET,NSET=ZAXIS,GENERATE
1,81,4
*NSET,NSET=TOP
81,181,281
*NSET,NSET=SIDE,GENERATE
201,281,4
*NSET,NSET=SIDE1,GENERATE
205,281,4
*ELEMENT,TYPE=CAX8R
1,1,201,209,9,101,205,109,5
*ELGEN,ELSET=ALL
1,10,8,10
*ELSET,ELSET=PR
1,91
*SOLID SECTION,MATERIAL=MAT,ELSET=ALL
*End Part
**  
**
** ASSEMBLY
**
*Assembly, name=BIG
**  
*Instance, name=DUMMY-1, part=DUMMY
*EQUATION
2, 
SIDE1,1,1., 201,1,-1.
*end instance
*end assembly
*MATERIAL,NAME=MAT
*ELASTIC
3.E7,.3
*PLASTIC
3.6E4,.0
3.6E4,.0,250.
4.5E3,.0,2000.
*EXPANSION,ZERO=70.
7.5E-6, 
*INITIAL CONDITIONS,TYPE=TEMPERATURE
DUMMY-1.ALL,1900.
*STEP,INC=100
*STATIC
10.,9.616E4
*BOUNDARY
DUMMY-1.RAXIS,2
DUMMY-1.ZAXIS,1
*TEMPERATURE,FILE=quenchplate_dc2d4,MIDSIDE
*EL PRINT,FREQUENCY=5
COORD,S
E, 
PE, 
TEMP, 
*EL FILE,ELSET=DUMMY-1.PR
S,PE
*OUTPUT,FIELD
*ELEMENT OUTPUT,ELSET=DUMMY-1.PR
S,PE
*NODE PRINT,FREQUENCY=5
nt, 
*END STEP