*HEADING
 DATA DECK TO VERIFY JOHNSON COOK PLASTICITY MODEL
 ELEMENTS TESTED: T2D2, T3D2, B21, B31, SAX1,
                  C3D8R, CPE4R, CPS4R, CAX4R
                  S4R, S4RS, S4RSW, M3D4R
 LOADING: UNIAXIAL COMPRESSION
*NODE,NSET=A1
*NODE,NSET=A2
**
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2D1
*ELEMENT, TYPE=T2D2, ELSET=T2D2
*ELEMENT, TYPE=T3D2, ELSET=T3D1
*ELEMENT, TYPE=T3D2, ELSET=T3D2
**
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2D1
*ELEMENT, TYPE=B21, ELSET=B2D2
*ELEMENT, TYPE=B31, ELSET=B3D1
*ELEMENT, TYPE=B31, ELSET=B3D2
**
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXI1
*ELEMENT, TYPE=SAX1, ELSET=SAXI2
**
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3D1
*ELEMENT, TYPE=C3D8R, ELSET=S3D2
**
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2D1
*ELEMENT, TYPE=CPE4R, ELSET=PE2D2
**
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2D1
*ELEMENT, TYPE=CPS4R, ELSET=PS2D2
**
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAX1
*ELEMENT, TYPE=CAX4R, ELSET=CAX2
**
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHE1
*ELEMENT, TYPE=S4R, ELSET=SHE2
*ELEMENT, TYPE=S4RS, ELSET=SHES1
*ELEMENT, TYPE=S4RS, ELSET=SHES2
*ELEMENT, TYPE=S4RSW, ELSET=SHESW1
*ELEMENT, TYPE=S4RSW, ELSET=SHESW2
**
**  MEMBRANE
*ELEMENT, TYPE=M3D4R, ELSET=MEMB1
*ELEMENT, TYPE=M3D4R, ELSET=MEMB2
**
*BEAM SECTION,SECTION=RECT,ELSET=B2D1,MATERIAL=A1,
TEMPERATURE=VALUE
 0.1, 0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3D1,MATERIAL=A1,
TEMPERATURE=VALUE
 0.1, 0.1
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHE1,MATERIAL=A1
 0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHES1,MATERIAL=A1
 0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHESW1,MATERIAL=A1
 0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXI1,MATERIAL=A1
 0.1, 3
*SOLID SECTION,ELSET=S3D1,MATERIAL=A1
*SOLID SECTION,ELSET=PE2D1,MATERIAL=A1
*SOLID SECTION,ELSET=PS2D1,MATERIAL=A1
*SOLID SECTION,ELSET=CAX1,MATERIAL=A1
*MEMBRANE SECTION,ELSET=MEMB1,MATERIAL=A1
 1.0,
*SOLID SECTION,ELSET=T2D1,MATERIAL=A1
*SOLID SECTION,ELSET=T3D1,MATERIAL=A1
 0.1, 0.1
**
*BEAM SECTION,SECTION=RECT,ELSET=B2D2,MATERIAL=A2,
TEMPERATURE=VALUE
 0.1, 0.1
*BEAM SECTION,SECTION=RECT,ELSET=B3D2,MATERIAL=A2,
TEMPERATURE=VALUE
 0.1, 0.1
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHE2,MATERIAL=A2
 0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHES2,MATERIAL=A2
 0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHESW2,MATERIAL=A2
 0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SAXI2,MATERIAL=A2
 0.1, 3
*SOLID SECTION,ELSET=S3D2,MATERIAL=A2
*SOLID SECTION,ELSET=PE2D2,MATERIAL=A2
*SOLID SECTION,ELSET=PS2D2,MATERIAL=A2
*SOLID SECTION,ELSET=CAX2,MATERIAL=A2
*MEMBRANE SECTION,ELSET=MEMB2,MATERIAL=A2
 1.0,
*SOLID SECTION,ELSET=T2D2,MATERIAL=A2
*SOLID SECTION,ELSET=T3D2,MATERIAL=A2
 0.1, 0.1
**
** Mises Material Properties (OFHC copper)
*MATERIAL,NAME=A1
*ELASTIC
 124.E9, 0.34
** Young's modulus unit: Pa
*PLASTIC
  90.0000E6,   0.0000
 142.7256E6,   0.0040
 155.3643E6,   0.0080
 164.1189E6,   0.0120
 171.0327E6,   0.0160
 176.8365E6,   0.0200
 187.4375E6,   0.0290
 195.9536E6,   0.0380
** Yield stress unit: Pa
*DENSITY
 8.96E3,
** unit: kg/m^3
**
** JOHNSON-COOK PLASTICITY (OFHC copper)
*MATERIAL,NAME=A2
*ELASTIC
 124.E9, 0.34
** Young's modulus unit: Pa
*PLASTIC,HARDENING=JOHNSON COOK
 90.E6, 292.E6, 0.31, 1.09, 1083., 25.
** A & B unit: Pa
*DENSITY
 8.96E3,
** unit: kg/m^3
**
*NSET, NSET=BOTTOM
*NSET, NSET=TOP
*NSET,NSET=LEFT
*NSET,NSET=FACE
*NSET,NSET=SHELL3D
*NSET,NSET=SHELL2D
*ELSET,ELSET=EALL
**
*BOUNDARY
 LEFT, 1, 1
 BOTTOM, 2, 2
 FACE, 3, 3
 SHELL2D, 6
 SHELL3D, 3, 6
*AMPLITUDE,NAME=LOAD,DEFINITION=SMOOTH STEP
 0., 0., 1., 1.
**
*INITIAL CONDITIONS, TYPE=HARDENING
 EALL, 0.02
**
*ELSET,ELSET=QA_TEST_All_ELSETS_AUTO
T2D1, T2D2, T3D1, T3D2, B2D1, B2D2, B3D1, B3D2, SAXI1, SAXI2, S3D1, S3D2, PE2D1, PE2D2, PS2D1, PS2D2, CAX1, CAX2, SHE1, SHE2, SHES1, SHES2, SHESW1, SHESW2, MEMB1, MEMB2, B2D1, B3D1, SHE1, SHES1, SHESW1, SAXI1, S3D1, PE2D1, PS2D1, CAX1, MEMB1, T2D1, T3D1, B2D2, B3D2, SHE2, SHES2, SHESW2, SAXI2, S3D2, PE2D2, PS2D2, CAX2, MEMB2, T2D2, T3D2, EALL,
*NSET,NSET=QA_TEST_All_NSETS_AUTO
A1, A2, BOTTOM, TOP, LEFT, FACE, SHELL3D, SHELL2D,
*STEP
*DYNAMIC,EXPLICIT,ELEMENT BY ELEMENT
 ,1.
**
** Uniaxial compression
*BOUNDARY,AMPLITUDE=LOAD
 TOP, 2, 2, -0.1
**
*FILE OUTPUT,NUMBER=2,TIME MARKS=YES
*EL FILE
 PEEQ,
 MISES,
 PRESS,
*OUTPUT,FIELD,VARIABLE=PRESELECT,NUMBER INTERVAL=4,OP=NEW
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIME INTERVAL=0.25,OP=NEW
*OUTPUT, FIELD,NUMBER=2,TIME MARKS=YES
*ELEMENT OUTPUT,ELSET=QA_TEST_All_ELSETS_AUTO
 PEEQ,
 MISES,
 PRESS,
*END STEP