*HEADING
 DATA DECK TO VERIFY TEMPERATURE DEPENDENT MATERIAL PROPERTY FOR
 PLASTIC MATERIALS
*NODE, INPUT=temp_plastic_ef1.inp
**
**  Mises plastic material
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2D
*ELEMENT, TYPE=T3D2, ELSET=T3D
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2D
*ELEMENT, TYPE=B31, ELSET=B3D
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXI
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3D
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2D
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2D
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAX
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHE
*ELEMENT, TYPE=S4RS, ELSET=SHES
*ELEMENT, TYPE=S4RSW, ELSET=SHESW
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMB
*MATERIAL,NAME=A1
*ELASTIC
 193.1E9, 0.3, 0.0
 160.1E9, 0.3, 100.0
*PLASTIC
 206893., 0.0, 0.0
 413786., 1.0, 0.0
 186893., 0.0, 100.0
 373786., 1.0, 100.0
*DENSITY
 8032.,
*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
*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=SHESW,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, POISSON=MATERIAL
1.0,
*SOLID SECTION,ELSET=T2D,MATERIAL=A1
*SOLID SECTION,ELSET=T3D,MATERIAL=A1
0.1,0.1
**
**  Drucker material
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIDRUCKER
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DDRUCKER
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DDRUCKER
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DDRUCKER
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXDRUCKER
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEDRUCKER
*ELEMENT, TYPE=S4RS, ELSET=SHEDRUCKES
*ELEMENT, TYPE=S4RSW, ELSET=SHEDRUCKEW
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBDRUCKER
*MATERIAL,NAME=A1DRUCKER
*DENSITY
1000.,
*ELASTIC
2.1E7,0.3, 0.0
1.9E7,0.3, 100.0
*DRUCKER PRAGER
*DRUCKER PRAGER HARDENING
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDRUCKER,MATERIAL=A1DRUCKER
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDRUCKES,MATERIAL=A1DRUCKER
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDRUCKEW,MATERIAL=A1DRUCKER
0.1, 3
*MEMBRANE SECTION,ELSET=MEMBDRUCKER,MATERIAL=A1DRUCKER, POISSON=MATERIAL
1.0,
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXIDRUCKER,MATERIAL=A1DRUCKER
0.1, 3
*SOLID SECTION,ELSET=S3DDRUCKER,MATERIAL=A1DRUCKER
*SOLID SECTION,ELSET=PE2DDRUCKER,MATERIAL=A1DRUCKER
*SOLID SECTION,ELSET=PS2DDRUCKER,MATERIAL=A1DRUCKER
*SOLID SECTION,ELSET=CAXDRUCKER,MATERIAL=A1DRUCKER
0.1,0.1
**
** Hill material
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIHILL
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DHILL
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DHILL
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DHILL
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXHILL
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEHILL
*ELEMENT, TYPE=S4RS, ELSET=SHEHILLS
*ELEMENT, TYPE=S4RSW, ELSET=SHEHILLW
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBHILL
*MATERIAL,NAME=A1HILL
*DENSITY
2500.,
*ELASTIC
1.E9,0.3, 0.0
8.E8,0.31, 100.0
*PLASTIC
1.E6,0.0, 0.0
5.E6,10., 0.0
0.9E6,0.0, 100.0
4.6E6,10., 100.0
*POTENTIAL
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEHILL,MATERIAL=A1HILL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEHILLS,MATERIAL=A1HILL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEHILLW,MATERIAL=A1HILL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXIHILL,MATERIAL=A1HILL
0.1, 3
*MEMBRANE SECTION,ELSET=MEMBHILL,MATERIAL=A1HILL
1.0,
**local orientation matching global system
*ORIENTATION,NAME=RECT
*SOLID SECTION,ELSET=S3DHILL,MATERIAL=A1HILL,ORIENT=RECT
*SOLID SECTION,ELSET=PE2DHILL,MATERIAL=A1HILL,ORIENT=RECT
*SOLID SECTION,ELSET=PS2DHILL,MATERIAL=A1HILL,ORIENT=RECT
*SOLID SECTION,ELSET=CAXHILL,MATERIAL=A1HILL,ORIENT=RECT
**
** Crushable foam
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DCFOAM
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DCFOAM
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXCFOAM
**
*SOLID SECTION,ELSET=S3DCFOAM,MATERIAL=A1CFOAM
*SOLID SECTION,ELSET=PE2DCFOAM,MATERIAL=A1CFOAM
*MATERIAL,NAME=A1CFOAM
*ELASTIC
 3.0E6, 0.0,   0.0
 2.0E6, 0.0, 100.0
*CRUSHABLE FOAM,HARDENING=ISOTROPIC
*CRUSHABLE FOAM HARDENING
*DENSITY
 500.,
**
*SOLID SECTION,ELSET=CAXCFOAM,MATERIAL=A2CFOAM
*MATERIAL,NAME=A2CFOAM
*ELASTIC
 3.0E6, 0.0,   0.0
 2.0E6, 0.0, 100.0
*CRUSHABLE FOAM,HARDENING=VOLUMETRIC
*CRUSHABLE FOAM HARDENING
*DENSITY
 500.,
**
**  Ductile failure plasticity
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2DDUCT
*ELEMENT, TYPE=T3D2, ELSET=T3DDUCT
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2DDUCT
*ELEMENT, TYPE=B31, ELSET=B3DDUCT
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIDUCT
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DDUCT
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DDUCT
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DDUCT
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXDUCT
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEDUCT
*ELEMENT, TYPE=S4RS, ELSET=SHEDUCTS
*ELEMENT, TYPE=S4RSW, ELSET=SHEDUCTW
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBDUCT
*MATERIAL,NAME=A1DUCT
*ELASTIC
 2.0E+8, 0.3, 0.0
 1.8E+8, 0.3, 100.0
*PLASTIC
 2.0E+5, 0.0, 0.0
 4.0E+5, 0.5, 0.0
 1.8E+5, 0.0, 100.0
 3.7E+5, 0.5, 100.0
*SHEAR FAILURE
*DENSITY
 5800.,
*BEAM SECTION,SECTION=RECT,ELSET=B2DDUCT,MATERIAL=A1DUCT,
TEMPERATURE=VALUE
0.1,0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3DDUCT,MATERIAL=A1DUCT,
TEMPERATURE=VALUE
0.1,0.1
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDUCT,MATERIAL=A1DUCT
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDUCTS,MATERIAL=A1DUCT
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDUCTW,MATERIAL=A1DUCT
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXIDUCT,MATERIAL=A1DUCT
0.1, 3
*SOLID SECTION,ELSET=S3DDUCT,MATERIAL=A1DUCT
*SOLID SECTION,ELSET=PE2DDUCT,MATERIAL=A1DUCT
*SOLID SECTION,ELSET=PS2DDUCT,MATERIAL=A1DUCT
*SOLID SECTION,ELSET=CAXDUCT,MATERIAL=A1DUCT
*MEMBRANE SECTION,ELSET=MEMBDUCT,MATERIAL=A1DUCT, POISSON=MATERIAL
1.0,
*SOLID SECTION,ELSET=T2DDUCT,MATERIAL=A1DUCT
*SOLID SECTION,ELSET=T3DDUCT,MATERIAL=A1DUCT
0.1,0.1
**
**  Rate dependent Hill's material
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIRHILL
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DRHILL
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DRHILL
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DRHILL
**
**  AXISYMMETRIC SOLID ELEMENT
**
*ELEMENT, TYPE=CAX4R, ELSET=CAXRHILL
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHERHILL
*ELEMENT, TYPE=S4RS, ELSET=SHERHILLS
*ELEMENT, TYPE=S4RSw, ELSET=SHERHILLW
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBRHILL
*MATERIAL,NAME=A1RHILL
*DENSITY
2500.,
*ELASTIC
1.E9,0.3, 0.0
8.E8,0.31, 100.0
*PLASTIC
1.E6,0.0, 0.0
5.E6,10., 0.0
0.9E6,0.0, 100.0
4.6E6,10., 100.0
*POTENTIAL
*RATE DEPENDENT
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHERHILL,MATERIAL=A1RHILL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHERHILLS,MATERIAL=A1RHILL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHERHILLW,MATERIAL=A1RHILL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXIRHILL,MATERIAL=A1RHILL
0.1, 3
*SOLID SECTION,ELSET=S3DRHILL,MATERIAL=A1RHILL,ORIENT=RECT
*SOLID SECTION,ELSET=PE2DRHILL,MATERIAL=A1RHILL,ORIENT=RECT
*SOLID SECTION,ELSET=PS2DRHILL,MATERIAL=A1RHILL,ORIENT=RECT
*SOLID SECTION,ELSET=CAXRHILL,MATERIAL=A1RHILL,ORIENT=RECT
*MEMBRANE SECTION,ELSET=MEMBRHILL,MATERIAL=A1RHILL
1.0,
**
**  Rate dependent plastic material
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2DRPL
*ELEMENT, TYPE=T3D2, ELSET=T3DRPL
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2DRPL
*ELEMENT, TYPE=B31, ELSET=B3DRPL
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIRPL
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DRPL
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DRPL
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DRPL
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXRPL
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHERPL
*ELEMENT, TYPE=S4RS, ELSET=SHERPLS
*ELEMENT, TYPE=S4RSW, ELSET=SHERPLW
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBRPL
*MATERIAL,NAME=A1RPL
*DENSITY
8032.0,
*ELASTIC
193.1E9, 0.3, 0.0
160.1E9, 0.3, 100.0
*PLASTIC
206893.0 , 0.0, 0.0
413786.0 , 1.0, 0.0
186893.0 , 0.0, 100.0
373786.0 , 1.0, 100.0
*RATE DEPENDENT
*BEAM SECTION,SECTION=RECT,ELSET=B2DRPL,MATERIAL=A1RPL,
TEMPERATURE=VALUE
0.1,0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3DRPL,MATERIAL=A1RPL,
TEMPERATURE=VALUE
0.1,0.1
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHERPL,MATERIAL=A1RPL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHERPLS,MATERIAL=A1RPL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHERPLW,MATERIAL=A1RPL
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXIRPL,MATERIAL=A1RPL
0.1, 3
*SOLID SECTION,ELSET=S3DRPL,MATERIAL=A1RPL
*SOLID SECTION,ELSET=PE2DRPL,MATERIAL=A1RPL
*SOLID SECTION,ELSET=PS2DRPL,MATERIAL=A1RPL
*SOLID SECTION,ELSET=CAXRPL,MATERIAL=A1RPL
*MEMBRANE SECTION,ELSET=MEMBRPL,MATERIAL=A1RPL
1.0,
*SOLID SECTION,ELSET=T2DRPL,MATERIAL=A1RPL
*SOLID SECTION,ELSET=T3DRPL,MATERIAL=A1RPL
0.1,0.1
**
**  Cap plastic material
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DCAP
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DCAP
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXCAP
*MATERIAL,NAME=A1CAP
*DENSITY
 2.4E-3,
*ELASTIC
30000.,0.3, 0.0
29000.,0.29, 100.0
*CAP PLASTICITY
*CAP HARDENING
*SOLID SECTION,ELSET=S3DCAP,MATERIAL=A1CAP
*SOLID SECTION,ELSET=PE2DCAP,MATERIAL=A1CAP
*SOLID SECTION,ELSET=CAXCAP,MATERIAL=A1CAP
**
** Porous material
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIPORO
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DPORO
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DPORO
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DPORO
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXPORO
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEPORO
*ELEMENT, TYPE=S4RS, ELSET=SHEPOROS
*ELEMENT, TYPE=S4RSW, ELSET=SHEPOROW
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBPORO
*MATERIAL,NAME=A1PORO
*DENSITY
 7700.E4,
*ELASTIC
 200.E9, 0.33, 0.0
 180.E9, 0.33, 100.0
*PLASTIC
 750.E6,
*POROUS METAL PLASTICITY, RELATIVE DENSITY=0.98
*VOID NUCLEATION
*POROUS FAILURE CRITERIA
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEPORO,MATERIAL=A1PORO
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEPOROS,MATERIAL=A1PORO
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEPOROW,MATERIAL=A1PORO
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXIPORO,MATERIAL=A1PORO
0.1, 3
*SOLID SECTION,ELSET=S3DPORO,MATERIAL=A1PORO
*SOLID SECTION,ELSET=PE2DPORO,MATERIAL=A1PORO
*SOLID SECTION,ELSET=PS2DPORO,MATERIAL=A1PORO
*SOLID SECTION,ELSET=CAXPORO,MATERIAL=A1PORO
*MEMBRANE SECTION,ELSET=MEMBPORO,MATERIAL=A1PORO, POISSON=MATERIAL
1.0,
*NSET, NSET=B2ALL
*NSET, NSET=B3ALL
*NSET, NSET=SALL, GENERATE
*NSET, NSET=SFACE, GENERATE
*NSET, NSET=BOTTOM
*NSET, NSET=TOP
*ELSET, ELSET=EALL1
*NSET, NSET=ALL
B2ALL, B3ALL, SALL
*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
EALL1,
*RESTART,TIMEMARKS=NO,WRITE,NUMBER=10
**
*STEP
*DYNAMIC,EXPLICIT
,0.001
*TEMPERATURE
 B2ALL, 100.0, 100.0, 100.0
 B3ALL, 100.0, 100.0, 100.0, 100.0
 SALL,  100.0
*BOUNDARY,TYPE=VELOCITY
 TOP, 2, 2, 10.0
**
*FILE OUTPUT,TIMEMARKS=YES,NUM=1
*EL FILE
 PEEQ,
 MISES,
 PE,
**
*OUTPUT,FIELD,NUM=0
*END STEP