*HEADING
 INPUT FILE TO VERIFY THERMAL STRAIN FOR MISES PLASTIC MATERIAL
 WITH 19 DIFFERENT TYPES OF ELEMENTS
**
**  Mises plastic material
**
**  TRUSS ELEMENT
**
*NODE
*ELEMENT, TYPE=T2D2, ELSET=T2D
*NODE
*ELEMENT, TYPE=T3D2, ELSET=T3D
**
**  BEAM ELEMENT
**
*NODE
*ELEMENT, TYPE=B21, ELSET=B2D
*NODE
*ELEMENT, TYPE=B31, ELSET=B3D
*NODE
*ELEMENT, TYPE=PIPE21, ELSET=PIPE2D
*NODE
*ELEMENT, TYPE=PIPE31, ELSET=PIPE3D
*NODE
*ELEMENT, TYPE=B22, ELSET=B2D_QUAD
*NODE
*ELEMENT, TYPE=B32, ELSET=B3D_QUAD
**
**  AXISYMMETRIC SHELL ELEMENT
**
*NODE
*ELEMENT, TYPE=SAX1, ELSET=SAXI
**
**  AXISYMMETRIC SOLID ELEMENT
**
*NODE
*ELEMENT, TYPE=CAX4R, ELSET=CAX
**
*NODE
*ELEMENT, TYPE=CAX6M, ELSET=CAX
**
**  3D SOLID ELEMENT
**
*NODE
*ELEMENT, TYPE=C3D8R, ELSET=S3D
**
*NODE
*ELEMENT, TYPE=C3D10M, ELSET=S3D
****
**  PLANE STRAIN ELEMENT
**
*NODE
*ELEMENT, TYPE=CPE4R, ELSET=PE2D
**
*NODE
*ELEMENT, TYPE=CPE6M, ELSET=PE2D
**
**  PLANE STRESS ELEMENT
**
*NODE
*ELEMENT, TYPE=CPS4R, ELSET=PS2D
**
*NODE
*ELEMENT, TYPE=CPS6M, ELSET=PS2D
**
**  SHELL ELEMENTS
**
*NODE
*ELEMENT, TYPE=S4R, ELSET=SHE
*NODE
*ELEMENT, TYPE=S4RS, ELSET=SHES
*NODE
*ELEMENT, TYPE=S4RSW, ELSET=SHEW
**
**  Membrane
**
*NODE
*ELEMENT, TYPE=M3D4R, ELSET=MEMB
**
*MATERIAL,NAME=A1
*ELASTIC
193.1E9, 0.3
*PLASTIC
206893.0 , 0.0
413786.0 , 1.0
*DENSITY
80320,
*EXPANSION
0.00005,
*BEAM SECTION,SECTION=RECT,ELSET=B2D,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3D,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.1
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE2D,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE3D,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=RECT,ELSET=B2D_QUAD,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3D_QUAD,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.1
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHE,MATERIAL=A1
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHES,MATERIAL=A1
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEW,MATERIAL=A1
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS, ELSET=SAXI,MATERIAL=A1
0.1, 3
*SOLID SECTION,ELSET=S3D,MATERIAL=A1
*SOLID SECTION,ELSET=PE2D,MATERIAL=A1
*SOLID SECTION,ELSET=PS2D,MATERIAL=A1
*SOLID SECTION,ELSET=CAX,MATERIAL=A1
*MEMBRANE SECTION,ELSET=MEMB,MATERIAL=A1
1.0,
*SOLID SECTION,ELSET=T2D,MATERIAL=A1
*SOLID SECTION,ELSET=T3D,MATERIAL=A1
0.1,0.1
*NSET, NSET=B2ALL
*NSET, NSET=B3ALL
*NSET, NSET=SALL, GENERATE
*NSET, NSET=SFACE, GENERATE
*ELSET, ELSET=EALL1
*NSET, NSET=SALL
SALL, SFACE
*NSET, NSET=ALL
B2ALL, B3ALL, SALL
*BOUNDARY
ALL,2,2
SFACE,3,3
*INITIAL CONDITION, TYPE=TEMPERATURE
ALL, 0.
*ELSET, ELSET=EALL
EALL1,
**
*STEP
*DYNAMIC,EXPLICIT
,0.1
*TEMPERATURE
 B2ALL, 100.0, 100.0, 100.0
 B3ALL, 100.0, 100.0, 100.0, 100.0
 SALL, 100.0
**
*FILE OUTPUT,TIMEMARKS=YES,NUM=1
*EL FILE
 MISES,
 PEEQ,
 ELEN,
**
*OUTPUT, HIST, FREQ=9999, VAR=PRESELECT
*ELEMENT OUTPUT, ELSET=EALL
 PEEQ,
*END STEP