*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
   1,  1.0, 0.0
   2,  1.0, 1.0
   3,  2.0, 0.0, 0.0
   4,  2.0, 1.0, 0.0
   5,  3.0, 0.0
   6,  3.0, 1.0
   7,  4.0, 0.0
   8,  4.0, 1.0
   9,  5.0, 0.0
  10,  5.0, 1.0
  11,  6.0, 0.0, 1.0
  12,  7.0, 0.0, 1.0
  13,  7.0, 0.0, 0.0
  14,  6.0, 0.0, 0.0
  15,  6.0, 1.0, 1.0
  16,  7.0, 1.0, 1.0
  17,  7.0, 1.0, 0.0
  18,  6.0, 1.0, 0.0
 101,  8.0, 0.0
 102,  9.0, 0.0
 103,  9.0, 1.0
 104,  8.0, 1.0
 201, 10.0, 0.0
 202, 11.0, 0.0
 203, 11.0, 1.0
 204, 10.0, 1.0
 301, 12.0, 0.0
 302, 13.0, 0.0
 303, 13.0, 1.0
 304, 12.0, 1.0
 401, 14.0, 0.0
 402, 15.0, 0.0
 403, 15.0, 1.0
 404, 14.0, 1.0
 501, 16.0, 0.0
 502, 17.0, 0.0
 503, 17.0, 1.0
 504, 16.0, 1.0
 601, 18.0, 0.0
 602, 19.0, 0.0
 603, 19.0, 1.0
 604, 18.0, 1.0
 701, 20.0, 0.0
 702, 21.0, 0.0
 703, 21.0, 1.0
 704, 20.0, 1.0
*NODE,NSET=A2
 1001,  1.0, 2.0
 1002,  1.0, 3.0
 1003,  2.0, 2.0, 0.0
 1004,  2.0, 3.0, 0.0
 1005,  3.0, 2.0
 1006,  3.0, 3.0
 1007,  4.0, 2.0
 1008,  4.0, 3.0
 1009,  5.0, 2.0
 1010,  5.0, 3.0
 1011,  6.0, 2.0, 1.0
 1012,  7.0, 2.0, 1.0
 1013,  7.0, 2.0, 0.0
 1014,  6.0, 2.0, 0.0
 1015,  6.0, 3.0, 1.0
 1016,  7.0, 3.0, 1.0
 1017,  7.0, 3.0, 0.0
 1018,  6.0, 3.0, 0.0
 1101,  8.0, 2.0
 1102,  9.0, 2.0
 1103,  9.0, 3.0
 1104,  8.0, 3.0
 1201, 10.0, 2.0
 1202, 11.0, 2.0
 1203, 11.0, 3.0
 1204, 10.0, 3.0
 1301, 12.0, 2.0
 1302, 13.0, 2.0
 1303, 13.0, 3.0
 1304, 12.0, 3.0
 1401, 14.0, 2.0
 1402, 15.0, 2.0
 1403, 15.0, 3.0
 1404, 14.0, 3.0
 1501, 16.0, 2.0
 1502, 17.0, 2.0
 1503, 17.0, 3.0
 1504, 16.0, 3.0
 1601, 18.0, 2.0
 1602, 19.0, 2.0
 1603, 19.0, 3.0
 1604, 18.0, 3.0
 1701, 20.0, 2.0
 1702, 21.0, 2.0
 1703, 21.0, 3.0
 1704, 20.0, 3.0
**
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2D1
 1, 1, 2
*ELEMENT, TYPE=T2D2, ELSET=T2D2
 1001, 1001, 1002
*ELEMENT, TYPE=T3D2, ELSET=T3D1
 2, 3, 4
*ELEMENT, TYPE=T3D2, ELSET=T3D2
 1002, 1003, 1004
**
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2D1
 3, 5, 6
*ELEMENT, TYPE=B21, ELSET=B2D2
 1003, 1005, 1006
*ELEMENT, TYPE=B31, ELSET=B3D1
 4, 7, 8
*ELEMENT, TYPE=B31, ELSET=B3D2
 1004, 1007, 1008
**
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXI1
 5, 9, 10
*ELEMENT, TYPE=SAX1, ELSET=SAXI2
 1005, 1009, 1010
**
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3D1
 11, 11, 12, 13, 14, 15, 16, 17, 18
*ELEMENT, TYPE=C3D8R, ELSET=S3D2
 1011,1011,1012,1013,1014,1015,1016,1017,1018
**
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2D1
 101, 101, 102, 103, 104
*ELEMENT, TYPE=CPE4R, ELSET=PE2D2
 1101, 1101, 1102, 1103, 1104
**
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2D1
 201, 201, 202, 203, 204
*ELEMENT, TYPE=CPS4R, ELSET=PS2D2
 1201, 1201, 1202, 1203, 1204
**
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAX1
 301, 301, 302, 303, 304
*ELEMENT, TYPE=CAX4R, ELSET=CAX2
 1301, 1301, 1302, 1303, 1304
**
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHE1
 401, 401, 402, 403, 404
*ELEMENT, TYPE=S4R, ELSET=SHE2
 1401, 1401, 1402, 1403, 1404
*ELEMENT, TYPE=S4RS, ELSET=SHES1
 601, 601, 602, 603, 604
*ELEMENT, TYPE=S4RS, ELSET=SHES2
 1601, 1601, 1602, 1603, 1604
*ELEMENT, TYPE=S4RSW, ELSET=SHESW1
 701, 701, 702, 703, 704
*ELEMENT, TYPE=S4RSW, ELSET=SHESW2
 1701, 1701, 1702, 1703, 1704
**
**  MEMBRANE
*ELEMENT, TYPE=M3D4R, ELSET=MEMB1
 501, 501, 502, 503, 504
*ELEMENT, TYPE=M3D4R, ELSET=MEMB2
 1501, 1501, 1502, 1503, 1504
**
*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
 203.1705E6,   0.0470
 209.4871E6,   0.0560
 215.1371E6,   0.0650
 220.2701E6,   0.0740
 224.9886E6,   0.0830
 229.3661E6,   0.0920
 233.4572E6,   0.1010
 237.3040E6,   0.1100
 240.9393E6,   0.1190
 244.3896E6,   0.1280
 247.6762E6,   0.1370
 250.8171E6,   0.1460
 253.8271E6,   0.1550
 256.7187E6,   0.1640
 259.5029E6,   0.1730
 262.1888E6,   0.1820
 264.7846E6,   0.1910
 267.2973E6,   0.2000
** 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
 1,3,5,7,9,11,12,13,14,101,102
 201,202,301,302,401,402,501,502,
 601,602,701,702
 1001,1003,1005,1007,1009,
 1011,1012,1013,1014,1101,1102
 1201,1202,1301,1302,1401,1402,1501,1502,
 1601,1602,1701,1702
*NSET, NSET=TOP
 2,4,6,8,10,15,16,17,18,103,104
 203,204,303,304,403,404,503,504
 603,604,703,704
 1002,1004,1006,1008,1010,
 1015,1016,1017,1018,1103,1104
 1203,1204,1303,1304,1403,1404,1503,1504
 1603,1604,1703,1704
*NSET,NSET=LEFT
 1,2,3,4,5,6,7,8,
 11,14,15,18,
 101,104,201,204,
 301,304,401,404,
 501,504,601,604,701,704
 1001,1002,1003,1004,1005,1006,1007,1008,
 1011,1014,1015,1018,
 1101,1104,1201,1204,
 1301,1304,1401,1404,
 1501,1504,1601,1604,1701,1704
*NSET,NSET=FACE
 11,12,15,16
 1011,1012,1015,1016
*NSET,NSET=SHELL3D
 401, 402, 403, 404, 1401, 1402, 1403, 1404
 601, 602, 603, 604, 1601, 1602, 1603, 1604
 701, 702, 703, 704, 1701, 1702, 1703, 1704 
   7,   8,1007,1008
*NSET,NSET=SHELL2D
   5,   6,   9,  10, 1005, 1006, 1009, 1010
*ELSET,ELSET=EALL
 1,2,3,4,5,11,101,201,301,401,501,601,701
 1001,1002,1003,1004,1005,
 1011,1101,1201,1301,1401,1501,1601,1701
*ELSET,ELSET=QA_TEST_ELSET
EALL,
*NSET,NSET=QA_TEST_NSET
A1, A2
*ELSET, ELSET=PLOT
 101, 1101	
**
*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.
**
*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,NUM=10
*NODE OUTPUT
U,
*ELEMENT OUTPUT
S, PEEQ
*************************************
*OUTPUT,FIELD,NUM=1
*NODE OUTPUT,NSET=QA_TEST_NSET
U,
*ELEMENT OUTPUT,ELSET=QA_TEST_ELSET
LE,
*OUTPUT, HISTORY, FREQ=1
*ELEMENT OUTPUT, ELSET=PLOT
 MISES, LE22	
**
*END STEP