*HEADING
 DATA DECK TO VERIFY TEMPERATURE DEPENDENT MATERIAL PROPERTY FOR ELASTIC
 MATERIALS
*INCLUDE, INPUT=temp_elastic_ef1.inp
**
**  Elasticity
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2DELAS
10001, 10001, 10002
*ELEMENT, TYPE=T3D2, ELSET=T3DELAS
10002, 10003, 10004
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2DELAS
 10003, 10005, 10006
*ELEMENT, TYPE=B31, ELSET=B3DELAS
 10004, 10007, 10008
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIELAS
 10005, 10009, 10010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DELAS
 10011, 10011, 10012, 10013, 10014, 10015, 10016, 10017, 10018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DELAS
 10101, 10101, 10102, 10103, 10104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DELAS
 10201, 10201, 10202, 10203, 10204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXELAS
10301, 10301, 10302, 10303, 10304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEELAS
 10401, 10401, 10402, 10403, 10404
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBELAS
 10501, 10501, 10502, 10503, 10504
*ELEMENT, TYPE=S4RS, ELSET=SHEELSS
 10601, 10601, 10602, 10603, 10604
*ELEMENT, TYPE=S4RSW, ELSET=SHEELSW
 10701, 10701, 10702, 10703, 10704
*MATERIAL,NAME=A1ELAS
*ELASTIC
193.1E9, 0.0, 0.0
97.0E9, 0.0, 100.0
*DENSITY
7850, 
*BEAM SECTION,SECTION=RECT,ELSET=B2DELAS,MATERIAL=A1ELAS,TEMPERATURE=VALUE
0.1,0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3DELAS,MATERIAL=A1ELAS,TEMPERATURE=VALUE
0.1,0.1
*SHELL SECTION, SECTION INT=SIMP,ELSET=SHEELAS,MATERIAL=A1ELAS
0.1, 3
*SHELL SECTION, SECTION INT=SIMP,ELSET=SHEELSS,MATERIAL=A1ELAS
0.1, 3
*SHELL SECTION, SECTION INT=SIMP,ELSET=SHEELSW,MATERIAL=A1ELAS
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SAXIELAS,MATERIAL=A1ELAS
0.1, 3
*SOLID SECTION,ELSET=S3DELAS,MATERIAL=A1ELAS
*SOLID SECTION,ELSET=PE2DELAS,MATERIAL=A1ELAS
*SOLID SECTION,ELSET=PS2DELAS,MATERIAL=A1ELAS
*SOLID SECTION,ELSET=CAXELAS,MATERIAL=A1ELAS
*MEMBRANE SECTION,ELSET=MEMBELAS,MATERIAL=A1ELAS
1.0, 
*SOLID SECTION,ELSET=T2DELAS,MATERIAL=A1ELAS
*SOLID SECTION,ELSET=T3DELAS,MATERIAL=A1ELAS
0.1,0.1
**
**  Orthotropic material (Engineering Constants)
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIEC
 11005, 11009, 11010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DEC
 11011, 11011, 11012, 11013, 11014, 11015, 11016, 11017, 11018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DEC
 11101, 11101, 11102, 11103, 11104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DEC
 11201, 11201, 11202, 11203, 11204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXEC
11301, 11301, 11302, 11303, 11304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEEC
 11401, 11401, 11402, 11403, 11404
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBEC
 11501, 11501, 11502, 11503, 11504
*ELEMENT, TYPE=S4RS, ELSET=SHEECS
 11601, 11601, 11602, 11603, 11604
*ELEMENT, TYPE=S4RSW, ELSET=SHEECW
 11701, 11701, 11702, 11703, 11704
*MATERIAL,NAME=A1EC
*ELASTIC,TYPE=ENGINEERING CONSTANTS
2.E+11,1.E+11,1.E+11,0.0,0.0,0.0,0.7692308E+11,0.7692308E+11
0.9E+10, 0.0
1.E+11,0.5E+11,0.5E+11,0.0,0.0,0.0,0.6692308E+11,0.6692308E+11
0.8E+10, 100.
*DENSITY
 7850., 
*MATERIAL,NAME=A1EC1
*ELASTIC,TYPE=ENGINEERING CONSTANTS
1.E+11,2.E+11,1.E+11,0.0,0.0,0.0,0.7692308E+11,0.9E+10
0.7692308E+11, 0.0
0.5E+11,1.E+11,0.5E+11,0.0,0.0,0.0,0.6692308E+11,0.8E+10
0.6692308E+11, 100.
*DENSITY
 7850., 
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEEC,MATERIAL=A1EC
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEECS,MATERIAL=A1EC
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEECW,MATERIAL=A1EC
0.1, 3
*MEMBRANE SECTION,ELSET=MEMBEC,MATERIAL=A1EC
1.0, 
*SHELL SECTION, SECTION INT=SIMP, ELSET=SAXIEC,MATERIAL=A1EC1
0.1, 3
**local orientation matching global system 
*ORIENTATION,NAME=RECT
 1.0, 0.0, 0.0, 0.0, 1.0, 0.0
 1, 0.0
*SOLID SECTION,ELSET=S3DEC,MATERIAL=A1EC,ORIENT=RECT
*SOLID SECTION,ELSET=PE2DEC,MATERIAL=A1EC,ORIENT=RECT
*SOLID SECTION,ELSET=PS2DEC,MATERIAL=A1EC,ORIENT=RECT
*SOLID SECTION,ELSET=CAXEC,MATERIAL=A1EC,ORIENT=RECT
**
** Orthotropic material(Orthotropic)
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIORTH
 12005, 12009, 12010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DORTH
 12011, 12011, 12012, 12013, 12014, 12015, 12016, 12017, 12018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DORTH
 12101, 12101, 12102, 12103, 12104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DORTH
 12201, 12201, 12202, 12203, 12204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXORTH
12301, 12301, 12302, 12303, 12304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEORTH
 12401, 12401, 12402, 12403, 12404
*ELEMENT, TYPE=S4RS, ELSET=SHEORTS
 12601, 12601, 12602, 12603, 12604
*ELEMENT, TYPE=S4RSW, ELSET=SHEORTW
 12701, 12701, 12702, 12703, 12704
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBORTH
 12501, 12501, 12502, 12503, 12504
*MATERIAL,NAME=A1ORTH
*ELASTIC,TYPE=ORTHOTROPIC
2.24E+11,4.79E+5,1.23E+11,4.21E+5,4.74E+5,1.21E+11,7.69E+10,7.69E+10,
9.00E+9, 0.0
1.E+11,4.59E+5,0.5E+11,4.E+5,4.E+5,0.5E+11,7.E+10,7.E+10,
8.00E+9, 100.
*DENSITY
 7850., 
*MATERIAL,NAME=A1ORTHSAX
*ELASTIC,TYPE=ORTHOTROPIC
1.23E+11,4.79E+5,2.24E+11,4.74E+5,4.21E+5,1.21E+11,7.69E+10,7.69E+10,
9.00E+9, 0.0
0.5E+11,4.59E+5,1.E+11,4.E+5,4.E+5,0.5E+11,7.E+10,7.E+10,
8.00E+9, 100.
*DENSITY
 7850., 
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEORTH,MATERIAL=A1ORTH
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEORTS,MATERIAL=A1ORTH
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEORTW,MATERIAL=A1ORTH
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SAXIORTH,MATERIAL=A1ORTHSAX
0.1, 3
*MEMBRANE SECTION,ELSET=MEMBORTH,MATERIAL=A1ORTH
1.0, 
*SOLID SECTION,ELSET=S3DORTH,MATERIAL=A1ORTH,ORIENT=RECT
*SOLID SECTION,ELSET=PE2DORTH,MATERIAL=A1ORTH,ORIENT=RECT
*SOLID SECTION,ELSET=PS2DORTH,MATERIAL=A1ORTH,ORIENT=RECT
*SOLID SECTION,ELSET=CAXORTH,MATERIAL=A1ORTH,ORIENT=RECT
**
** Anisotropic material
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DAN
 13011, 13011, 13012, 13013, 13014, 13015, 13016, 13017, 13018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DAN
 13101, 13101, 13102, 13103, 13104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DAN
 13201, 13201, 13202, 13203, 13204
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEAN
 13401, 13401, 13402, 13403, 13404
*ELEMENT, TYPE=S4RS, ELSET=SHEANS
 13601, 13601, 13602, 13603, 13604
*ELEMENT, TYPE=S4RSW, ELSET=SHEANW
 13701, 13701, 13702, 13703, 13704
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBAN
 13501, 13501, 13502, 13503, 13504
*MATERIAL,NAME=A1AN
*ELASTIC,TYPE=ANISOTROPIC
2.24E+11,4.79E+5,1.23E+11,4.21E+5,4.74E+5,1.21E+11,1.E+6,2.E+6,
3.E+6,7.69E+10,4.E+6,5.E+6,6.E+6,7.E+6,7.69E+10,8.E+6,
9.E+6,10.E+6,11.E+6,12.E+6,9.00E+9, 0.
1.E+11,4.E+5,0.5E+11,4.E+5,4.E+5,0.5E+11,0.9E+6,1.8E+6,
2.6E+6,7.E+10,3.6E+6,4.6E+6,5.6E+6,6.6E+6,7.E+10,7.6E+6,
8.E+6,9.E+6,10.E+6,11.E+6,8.00E+9, 100.
*DENSITY
 7850., 
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEAN,MATERIAL=A1AN
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEANS,MATERIAL=A1AN
0.1, 3
*SHELL SECTION, SECTION INT=SIMP, ELSET=SHEANW,MATERIAL=A1AN
0.1, 3
*MEMBRANE SECTION,ELSET=MEMBAN,MATERIAL=A1AN
1.0, 
*SOLID SECTION,ELSET=S3DAN,MATERIAL=A1AN,ORIENT=RECT
*SOLID SECTION,ELSET=PE2DAN,MATERIAL=A1AN,ORIENT=RECT
*SOLID SECTION,ELSET=PS2DAN,MATERIAL=A1AN,ORIENT=RECT
**
** Lamina
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXILAMINA
 14005, 14009, 14010
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DLAMINA
 14201, 14201, 14202, 14203, 14204
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHELAMINA
 14401, 14401, 14402, 14403, 14404
*ELEMENT, TYPE=S4RS, ELSET=SHELAMINS
 14601, 14601, 14602, 14603, 14604
*ELEMENT, TYPE=S4RSW, ELSET=SHELAMINW
 14701, 14701, 14702, 14703, 14704
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBLAMINA
 14501, 14501, 14502, 14503, 14504
*MATERIAL,NAME=A1LAMINA
*ELASTIC,TYPE=LAMINA
2.E+11,1.5E+11,0.0,2.E+10,9.E+9,8.5E+9, 0.
1.E+11,0.7E+11,0.0,1.8E+10,8.E+9,7.5E+9, 100.
*DENSITY
 7850., 
*MATERIAL,NAME=A1LAMSAX
*ELASTIC,TYPE=LAMINA
1.5E+11,2.E+11,0.0,2.E+10,8.5E+9,9.E+9, 0.
0.7E+11,1.E+11,0.0,1.8E+10,7.5E+9,8.E+9, 100.
*DENSITY
 7850., 
*SHELL SECTION, SECTION INT=SIMP,ELSET=SHELAMINA,MATERIAL=A1LAMINA
0.1, 3
*SHELL SECTION, SECTION INT=SIMP,ELSET=SHELAMINS,MATERIAL=A1LAMINA
0.1, 3
*SHELL SECTION, SECTION INT=SIMP,ELSET=SHELAMINW,MATERIAL=A1LAMINA
0.1, 3
*SHELL SECTION, SECTION INT=SIMP,ELSET=SAXILAMINA,MATERIAL=A1LAMSAX
0.1, 3
*SOLID SECTION,ELSET=PS2DLAMINA,MATERIAL=A1LAMINA,ORIENT=RECT
*MEMBRANE SECTION,ELSET=MEMBLAMINA,MATERIAL=A1LAMINA
1.0, 
*ELSET, ELSET=EALL2
10001,10002,10003,10004,10005,10011,10101,10201,10301,10401,10501
10601,10701
11005,11011,11101,11201,11301,11401,11501,11601,11701
12005,12011,12101,12201,12301,12401,12501,12601,12701
13011,13101,13201,13401,13501,13601,13701
14005,14201,14401,14501,14601,14701
*BOUNDARY
BOTTOM,2,2
SFACE,3,3
*INITIAL CONDITION, TYPE=TEMPERATURE
B2ALL, 0.0, 0.0, 0.0
B3ALL, 0.0, 0.0, 0.0, 0.0
SALL, 0.0
*ELSET, ELSET=EALL
EALL2, 
*RESTART,TIMEMARKS=NO,WRITE,NUMBER=10
*AMPLITUDE, NAME=VAMP
0., 0., 0.01, 0.2
**
*ELSET,ELSET=QA_TEST_All_ELSETS_AUTO
T2DELAS, T3DELAS, B2DELAS, B3DELAS, SAXIELAS, S3DELAS, PE2DELAS, PS2DELAS, CAXELAS, SHEELAS, MEMBELAS, SHEELSS, SHEELSW, B2DELAS, B3DELAS, SHEELAS, SHEELSS, SHEELSW, SAXIELAS, S3DELAS, PE2DELAS, PS2DELAS, CAXELAS, MEMBELAS, T2DELAS, T3DELAS, SAXIEC, S3DEC, PE2DEC, PS2DEC, CAXEC, SHEEC, MEMBEC, SHEECS, SHEECW, SHEEC, SHEECS, SHEECW, MEMBEC, SAXIEC, S3DEC, PE2DEC, PS2DEC, CAXEC, SAXIORTH, S3DORTH, PE2DORTH, PS2DORTH, CAXORTH, SHEORTH, SHEORTS, SHEORTW, MEMBORTH, SHEORTH, SHEORTS, SHEORTW, SAXIORTH, MEMBORTH, S3DORTH, PE2DORTH, PS2DORTH, CAXORTH, S3DAN, PE2DAN, PS2DAN, SHEAN, SHEANS, SHEANW, MEMBAN, SHEAN, SHEANS, SHEANW, MEMBAN, S3DAN, PE2DAN, PS2DAN, SAXILAMINA, PS2DLAMINA, SHELAMINA, SHELAMINS, SHELAMINW, MEMBLAMINA, SHELAMINA, SHELAMINS, SHELAMINW, SAXILAMINA, PS2DLAMINA, MEMBLAMINA, EALL2, EALL,
*NSET,NSET=QA_TEST_All_NSETS_AUTO,ELSET=QA_TEST_All_ELSETS_AUTO
*STEP
*DYNAMIC,EXPLICIT
,0.01
*TEMPERATURE
 B2ALL, 100.0, 100.0, 100.0
 B3ALL, 100.0, 100.0, 100.0, 100.0
 SALL, 100.0
*BOUNDARY, TYPE=VELOCITY, AMPLITUDE=VAMP
 TOP, 2, 2, 1.0
**
*FILE OUTPUT,TIMEMARKS=YES,NUM=1
*EL FILE
 MISES,
 LE,
**
*OUTPUT,FIELD,VARIABLE=PRESELECT,NUMBER INTERVAL=4,OP=NEW
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIME INTERVAL=0.0025,OP=NEW
*OUTPUT, FIELD,TIMEMARKS=YES,NUM=1
*ELEMENT OUTPUT,ELSET=QA_TEST_All_ELSETS_AUTO
 MISES,
 LE,
*END STEP