*HEADING
 INPUT FILE TO VERIFY FIELD VARIABLE DEPENDENT MATERIAL PROPERTY 
 FOR PLASTIC MATERIALS
*NODE, INPUT=field_plastic_ef1.inp
**
**  Mises plastic material
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2D
1, 1, 2
*ELEMENT, TYPE=T3D2, ELSET=T3D
2, 3, 4
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2D
 3, 5, 6
*ELEMENT, TYPE=B31, ELSET=B3D
 4, 7, 8
**  PIPE ELEMENT
*ELEMENT, TYPE=PIPE21, ELSET=PIPE2D
 23, 25, 26
*ELEMENT, TYPE=PIPE31, ELSET=PIPE3D
 24, 27, 28
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXI
 5, 9, 10
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3D
 11, 11, 12, 13, 14, 15, 16, 17, 18
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2D
 101, 101, 102, 103, 104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2D
 201, 201, 202, 203, 204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAX
301, 301, 302, 303, 304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHE
 401, 401, 402, 403, 404
*ELEMENT, TYPE=S4RS, ELSET=SHES
 501, 501, 502, 503, 504
*ELEMENT, TYPE=S4RSW, ELSET=SHESW
 601, 601, 602, 603, 604
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMB
 701, 701, 702, 703, 704
*MATERIAL,NAME=A1
*ELASTIC, DEPE=1
193.1E9, 0.3, 0.0, 0.0
193.1E9, 0.3, 10.0, 0.0
160.1E9, 0.3, 0.0, 100.0
160.1E9, 0.3, 10.0, 100.0
*PLASTIC, DEPE=1
206893.0 , 0.0, 0.0, 0.0
413786.0 , 1.0, 0.0, 0.0
206893.0 , 0.0, 10.0, 0.0
413786.0 , 1.0, 10.0, 0.0
186893.0 , 0.0, 0.0, 100.0
373786.0 , 1.0, 0.0, 100.0
186893.0 , 0.0, 10.0, 100.0
373786.0 , 1.0, 10.0, 100.0
*DENSITY
8032, 
*BEAM SECTION,SECTION=PIPE,ELSET=B2D,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=B3D,MATERIAL=A1,TEMPERATURE=VALUE
0.1,0.01
*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
*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
 1005, 1009, 1010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DDRUCKER
 1011, 1011, 1012, 1013, 1014, 1015, 1016, 1017, 1018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DDRUCKER
 1101, 1101, 1102, 1103, 1104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DDRUCKER
 1201, 1201, 1202, 1203, 1204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXDRUCKER
1301, 1301, 1302, 1303, 1304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEDRUCKER
 1401, 1401, 1402, 1403, 1404
*ELEMENT, TYPE=S4RS, ELSET=SHEDRUCKES
 1501, 1501, 1502, 1503, 1504
*ELEMENT, TYPE=S4RSW, ELSET=SHEDRUCKEW
 1601, 1601, 1602, 1603, 1604
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBDRUCKER
 1701, 1701, 1702, 1703, 1704
*MATERIAL,NAME=A1DRUCKER
*DENSITY
1000., 
*ELASTIC, DEPE=1
2.1E7,0.3, 0.0, 0.0
2.1E7,0.3, 10.0, 0.0
1.9E7,0.3, 0.0, 100.0
1.9E7,0.3, 10.0, 100.0
*DRUCKER PRAGER, DEPE=1
40.,1.0,20., 0.0, 0.0
40.,1.0,20., 10.0, 0.0
39.,0.9,19., 0.0, 100.0
39.,0.9,19., 10.0, 100.0
*DRUCKER PRAGER HARDENING, DEPE=1
4.E4,0.0, 0.0, 0.0
8.E4,1.0, 0.0, 0.0
4.E4,0.0, 10.0, 0.0
8.E4,1.0, 10.0, 0.0
3.6E4,0.0, 0.0, 100.0
7.5E4,1.0, 0.0, 100.0
3.6E4,0.0, 10.0, 100.0
7.5E4,1.0, 10.0, 100.0
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDRUCKER,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
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDRUCKES,MATERIAL=A1DRUCKER
0.1, 3
*SHELL SECTION, SECTION INT=GAUSS,ELSET=SHEDRUCKEW,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
 2005, 2009, 2010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DHILL
 2011, 2011, 2012, 2013, 2014, 2015, 2016, 2017, 2018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DHILL
 2101, 2101, 2102, 2103, 2104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DHILL
 2201, 2201, 2202, 2203, 2204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXHILL
2301, 2301, 2302, 2303, 2304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEHILL
 2401, 2401, 2402, 2403, 2404
*ELEMENT, TYPE=S4RS, ELSET=SHEHILLS
 2501, 2501, 2502, 2503, 2504
*ELEMENT, TYPE=S4RSW, ELSET=SHEHILLW
 2601, 2601, 2602, 2603, 2604
**  MEMBRANE ELEMENT
*ELEMENT, TYPE=M3D4R, ELSET=MEMBHILL
 2701, 2701, 2702, 2703, 2704
*MATERIAL,NAME=A1HILL
*DENSITY
2500., 
*ELASTIC, DEPE=1
1.E9,0.3, 0.0, 0.0
1.E9,0.3, 10.0, 0.0
8.E8,0.31, 0.0, 100.0
8.E8,0.31, 10.0, 100.0
*PLASTIC, DEPE=1
1.E6,0.0, 0.0, 0.0
5.E6,10., 0.0, 0.0
1.E6,0.0, 10.0, 0.0
5.E6,10., 10.0, 0.0
0.9E6,0.0, 0.0, 100.0
4.6E6,10., 0.0, 100.0
0.9E6,0.0, 10.0, 100.0
4.6E6,10., 10.0, 100.0
*POTENTIAL
1.5,1.,1.,1.,1.,1.
*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, POISSON=MATERIAL
1.0, 
**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=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 with volumetric hardening and isotropic hardening
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DCFOAM
 3011, 3011, 3012, 3013, 3014, 3015, 3016, 3017, 3018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DCFOAM
 3101, 3101, 3102, 3103, 3104
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXCFOAM
3301, 3301, 3302, 3303, 3304
**
*SOLID SECTION,ELSET=S3DCFOAM,MATERIAL=A1CFOAM
*SOLID SECTION,ELSET=PE2DCFOAM,MATERIAL=A1CFOAM
*MATERIAL,NAME=A1CFOAM
*ELASTIC,DEPENDENCIES=1
 5.0E6, 0.3,  0.0,   0.0
 5.0E6, 0.3, 10.0,   0.0
 3.0E6, 0.0,  0.0, 100.0
 3.0E6, 0.0, 10.0, 100.0
*CRUSHABLE FOAM,HARDENING=VOLUMETRIC,DEPENDENCIES=1
 0.9, 0.1,  0.,   0.
 1.1, 0.1,  0.,  50.
 1.3, 0.1,  0., 100.
*CRUSHABLE FOAM HARDENING,DEPENDENCIES=1
 220000.0,  0.0, 0.,   0.
 246512.1,  0.1, 0.,   0.
 272938.0,  0.2, 0.,   0.
 299019.2,  0.3, 0.,   0.
 324549.1,  0.4, 0.,   0.
 349345.3,  0.5, 0.,   0.
 373259.8,  0.6, 0.,   0.
 396170.9,  0.7, 0.,   0.
 418011.1,  0.8, 0.,   0.
 438721.0,  0.9, 0.,   0.
 458268.2,  1.0, 0.,   0.
 493843.0,  1.2, 0.,   0.
 524836.3,  1.4, 0.,   0.
 551528.4,  1.6, 0.,   0.
 574307.3,  1.8, 0.,   0.
 593594.8,  2.0, 0.,   0.
 629359.6,  2.5, 0.,   0.
 651994.7,  3.0, 0.,   0.
 683338.7,  5.0, 0.,   0.
 688332.2, 10.0, 0.,   0.
 220000.0,  0.0, 0.,  50.
 246512.1,  0.1, 0.,  50.
 272938.0,  0.2, 0.,  50.
 299019.2,  0.3, 0.,  50.
 324549.1,  0.4, 0.,  50.
 349345.3,  0.5, 0.,  50.
 373259.8,  0.6, 0.,  50.
 396170.9,  0.7, 0.,  50.
 418011.1,  0.8, 0.,  50.
 438721.0,  0.9, 0.,  50.
 458268.2,  1.0, 0.,  50.
 493843.0,  1.2, 0.,  50.
 524836.3,  1.4, 0.,  50.
 551528.4,  1.6, 0.,  50.
 574307.3,  1.8, 0.,  50.
 593594.8,  2.0, 0.,  50.
 629359.6,  2.5, 0.,  50.
 651994.7,  3.0, 0.,  50.
 683338.7,  5.0, 0.,  50.
 688332.2, 10.0, 0.,  50.
 220000.0,  0.0, 0., 100.
 246512.1,  0.1, 0., 100.
 272938.0,  0.2, 0., 100.
 299019.2,  0.3, 0., 100.
 324549.1,  0.4, 0., 100.
 349345.3,  0.5, 0., 100.
 373259.8,  0.6, 0., 100.
 396170.9,  0.7, 0., 100.
 418011.1,  0.8, 0., 100.
 438721.0,  0.9, 0., 100.
 458268.2,  1.0, 0., 100.
 493843.0,  1.2, 0., 100.
 524836.3,  1.4, 0., 100.
 551528.4,  1.6, 0., 100.
 574307.3,  1.8, 0., 100.
 593594.8,  2.0, 0., 100.
 629359.6,  2.5, 0., 100.
 651994.7,  3.0, 0., 100.
 683338.7,  5.0, 0., 100.
 688332.2, 10.0, 0., 100.
*DENSITY
 500., 
**
*SOLID SECTION,ELSET=CAXCFOAM,MATERIAL=A2CFOAM
*MATERIAL,NAME=A2CFOAM
*ELASTIC,DEPENDENCIES=1
 5.0E6, 0.3,  0.0,   0.0
 5.0E6, 0.3, 10.0,   0.0
 3.0E6, 0.0,  0.0, 100.0
 3.0E6, 0.0, 10.0, 100.0
*CRUSHABLE FOAM,HARDENING=ISOTROPIC,DEPENDENCIES=1
 0.9, 0.,  0.,   0.
 1.1, 0.,  0.,  50.
 1.3, 0.,  0., 100.
*CRUSHABLE FOAM HARDENING
 220000.0,  0.0
 246512.1,  0.1
 272938.0,  0.2
 299019.2,  0.3
 324549.1,  0.4
 349345.3,  0.5
 373259.8,  0.6
 396170.9,  0.7
 418011.1,  0.8
 438721.0,  0.9
 458268.2,  1.0
 493843.0,  1.2
 524836.3,  1.4
 551528.4,  1.6
 574307.3,  1.8
 593594.8,  2.0
 629359.6,  2.5
 651994.7,  3.0
 683338.7,  5.0
 688332.2, 10.0
*DENSITY
 500., 
**
**  Ductile failure plasticity
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2DDUCT
4001, 4001, 4002
*ELEMENT, TYPE=T3D2, ELSET=T3DDUCT
4002, 4003, 4004
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2DDUCT
 4003, 4005, 4006
*ELEMENT, TYPE=B31, ELSET=B3DDUCT
 4004, 4007, 4008
**  PIPE ELEMENT
*ELEMENT, TYPE=PIPE21, ELSET=PIPE2DDUCT
 4023, 4025, 4026
*ELEMENT, TYPE=PIPE31, ELSET=PIPE3DDUCT
 4024, 4027, 4028
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIDUCT
 4005, 4009, 4010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DDUCT
 4011, 4011, 4012, 4013, 4014, 4015, 4016, 4017, 4018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DDUCT
 4101, 4101, 4102, 4103, 4104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DDUCT
 4201, 4201, 4202, 4203, 4204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXDUCT
4301, 4301, 4302, 4303, 4304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEDUCT
 4401, 4401, 4402, 4403, 4404
*ELEMENT, TYPE=S4RS, ELSET=SHEDUCTS
 4501, 4501, 4502, 4503, 4504
*ELEMENT, TYPE=S4RSW, ELSET=SHEDUCTW
 4601, 4601, 4602, 4603, 4604
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBDUCT
 4701, 4701, 4702, 4703, 4704
*MATERIAL,NAME=A1DUCT
*ELASTIC, DEPE=1
 2.E+8,0.3, 0.0, 0.0
 2.E+8,0.3, 10.0, 0.0
 1.8E+8,0.3, 0.0, 100.0
 1.8E+8,0.3, 10.0, 100.0
*PLASTIC,DEPE=1
 2.E+5, 0.0, 0.0,  0.0
 4.E+5, 0.5, 0.0,  0.0
 2.E+5, 0.0, 10.0, 0.0
 4.E+5, 0.5, 10.0, 0.0
 1.8E+5,0.0, 0.0,  100.0
 3.7E+5,0.5, 0.0,  100.0
 1.8E+5,0.0, 10.0, 100.0
 3.7E+5,0.5, 10.0, 100.0
*SHEAR FAILURE
 0.5,
*DENSITY
 5800., 
**
*BEAM SECTION,SECTION=PIPE,ELSET=B2DDUCT,MATERIAL=A1DUCT, TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=B3DDUCT,MATERIAL=A1DUCT, TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE2DDUCT,MATERIAL=A1DUCT, TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE3DDUCT,MATERIAL=A1DUCT, TEMPERATURE=VALUE
0.1,0.01
*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
 5005, 5009, 5010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DRHILL
 5011, 5011, 5012, 5013, 5014, 5015, 5016, 5017, 5018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DRHILL
 5101, 5101, 5102, 5103, 5104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DRHILL
 5201, 5201, 5202, 5203, 5204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXRHILL
5301, 5301, 5302, 5303, 5304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHERHILL
 5401, 5401, 5402, 5403, 5404
*ELEMENT, TYPE=S4RS, ELSET=SHERHILLS
 5501, 5501, 5502, 5503, 5504
*ELEMENT, TYPE=S4RSw, ELSET=SHERHILLW
 5601, 5601, 5602, 5603, 5604
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBRHILL
 5701, 5701, 5702, 5703, 5704
*MATERIAL,NAME=A1RHILL
*DENSITY
2500., 
*ELASTIC, DEPE=1
1.E9,0.3, 0.0, 0.0
1.E9,0.3, 10.0, 0.0
8.E8,0.31, 0.0, 100.0
8.E8,0.31, 10.0, 100.0
*PLASTIC, DEPE=1
1.E6,0.0, 0.0, 0.0
5.E6,10., 0.0, 0.0
1.E6,0.0, 10.0, 0.0
5.E6,10., 10.0, 0.0
0.9E6,0.0, 0.0, 100.0
4.6E6,10., 0.0, 100.0
0.9E6,0.0, 10.0, 100.0
4.6E6,10., 10.0, 100.0
*POTENTIAL
1.5,1.,1.,1.,1.,1.
*RATE DEPENDENT
4000.,6.
*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, POISSON=MATERIAL
1.0, 
**
**  Rate dependent plastic material
**  TRUSS ELEMENT
*ELEMENT, TYPE=T2D2, ELSET=T2DRPL
6001, 6001, 6002
*ELEMENT, TYPE=T3D2, ELSET=T3DRPL
6002, 6003, 6004
**  BEAM ELEMENT
*ELEMENT, TYPE=B21, ELSET=B2DRPL
 6003, 6005, 6006
*ELEMENT, TYPE=B31, ELSET=B3DRPL
 6004, 6007, 6008
**  PIPE ELEMENT
*ELEMENT, TYPE=PIPE21, ELSET=PIPE2DRPL
 6023, 6025, 6026
*ELEMENT, TYPE=PIPE31, ELSET=PIPE3DRPL
 6024, 6027, 6028
**  AXISYMMETRIC SHELL ELEMENT
*ELEMENT, TYPE=SAX1, ELSET=SAXIRPL
 6005, 6009, 6010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DRPL
 6011, 6011, 6012, 6013, 6014, 6015, 6016, 6017, 6018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DRPL
 6101, 6101, 6102, 6103, 6104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DRPL
 6201, 6201, 6202, 6203, 6204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXRPL
6301, 6301, 6302, 6303, 6304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHERPL
 6401, 6401, 6402, 6403, 6404
*ELEMENT, TYPE=S4RS, ELSET=SHERPLS
 6501, 6501, 6502, 6503, 6504
*ELEMENT, TYPE=S4RSW, ELSET=SHERPLW
 6601, 6601, 6602, 6603, 6604
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBRPL
 6701, 6701, 6702, 6703, 6704
*MATERIAL,NAME=A1RPL
*DENSITY
8032.0, 
*ELASTIC, DEPE=1
193.1E9, 0.3, 0.0, 0.0
193.1E9, 0.3, 10.0, 0.0
160.1E9, 0.3, 0.0, 100.0
160.1E9, 0.3, 10.0, 100.0
*PLASTIC, DEPE=1
206893.0 , 0.0, 0.0, 0.0
413786.0 , 1.0, 0.0, 0.0
206893.0 , 0.0, 10.0, 0.0
413786.0 , 1.0, 10.0, 0.0
186893.0 , 0.0, 0.0, 100.0
373786.0 , 1.0, 0.0, 100.0
186893.0 , 0.0, 10.0, 100.0
373786.0 , 1.0, 10.0, 100.0
*RATE DEPENDENT
1000.,2.
*BEAM SECTION,SECTION=PIPE,ELSET=B2DRPL,MATERIAL=A1RPL, TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=B3DRPL,MATERIAL=A1RPL, TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE2DRPL,MATERIAL=A1RPL, TEMPERATURE=VALUE
0.1,0.01
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE3DRPL,MATERIAL=A1RPL, TEMPERATURE=VALUE
0.1,0.01
*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, POISSON=MATERIAL
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
 7011, 7011, 7012, 7013, 7014, 7015, 7016, 7017, 7018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DCAP
 7101, 7101, 7102, 7103, 7104
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXCAP
7301, 7301, 7302, 7303, 7304
*MATERIAL,NAME=A1CAP
*DENSITY
 2.4E-3, 
*ELASTIC, DEPE=1
30000.,0.3, 0.0, 0.0
30000.,0.3, 10.0, 0.0
29000.,0.29, 0.0, 100.0
29000.,0.29, 10.0, 100.0
*CAP PLASTICITY, DEPE=1
100.0,37.67,0.1,.0 ,.01, 1.0, 0.0, 0.0
100.0,37.67,0.1,.0 ,.01, 1.0, 10.0, 0.0
99.0,36.67,0.11,.0 ,.011, 1.0, 0.0, 100.
99.0,36.67,0.11,.0 ,.011, 1.0, 10.0, 100.
*CAP HARDENING, DEPE=1
 20.960, .000, 0.0, 0.0
 46.600, .0005, 0.0, 0.0
 79.670, .0010, 0.0, 0.0
126.280, .0015, 0.0, 0.0
205.950, .0020, 0.0, 0.0
311.270, .0023, 0.0, 0.0
655.600, .00249, 0.0, 0.0
 20.960, .000, 10.0, 0.0
 46.600, .0005, 10.0, 0.0
 79.670, .0010, 10.0, 0.0
126.280, .0015, 10.0, 0.0
205.950, .0020, 10.0, 0.0
311.270, .0023, 10.0, 0.0
655.600, .00249, 10.0, 0.0
 19.960, .000, 0.0, 100.0
 44.600, .0005, 0.0, 100.0
 70.670, .0010, 0.0, 100.0
120.280, .0015, 0.0, 100.0
200.950, .0020, 0.0, 100.0
300.270, .0023, 0.0, 100.0
600.600, .00249, 0.0, 100.0
 19.960, .000, 10.0, 100.0
 44.600, .0005, 10.0, 100.0
 70.670, .0010, 10.0, 100.0
120.280, .0015, 10.0, 100.0
200.950, .0020, 10.0, 100.0
300.270, .0023, 10.0, 100.0
600.600, .00249, 10.0, 100.0
*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
 8005, 8009, 8010
**  3D SOLID ELEMENT
*ELEMENT, TYPE=C3D8R, ELSET=S3DPORO
 8011, 8011, 8012, 8013, 8014, 8015, 8016, 8017, 8018
**  PLANE STRAIN ELEMENT
*ELEMENT, TYPE=CPE4R, ELSET=PE2DPORO
 8101, 8101, 8102, 8103, 8104
**  PLANE STRESS ELEMENT
*ELEMENT, TYPE=CPS4R, ELSET=PS2DPORO
 8201, 8201, 8202, 8203, 8204
**  AXISYMMETRIC SOLID ELEMENT
*ELEMENT, TYPE=CAX4R, ELSET=CAXPORO
8301, 8301, 8302, 8303, 8304
**  SHELL ELEMENT
*ELEMENT, TYPE=S4R, ELSET=SHEPORO
 8401, 8401, 8402, 8403, 8404
*ELEMENT, TYPE=S4RS, ELSET=SHEPOROS
 8501, 8501, 8502, 8503, 8504
*ELEMENT, TYPE=S4RSW, ELSET=SHEPOROW
 8601, 8601, 8602, 8603, 8604
**  Membrane
*ELEMENT, TYPE=M3D4R, ELSET=MEMBPORO
 8701, 8701, 8702, 8703, 8704
*MATERIAL,NAME=A1PORO
*DENSITY
7700.E4, 
*ELASTIC, DEPE=1
200.E9, .33, 0.0, 0.0
200.E9, .33, 10.0, 0.0
180.E9, .33, 0.0, 100.0
180.E9, .33, 10.0, 100.0
*PLASTIC
750.E6, 
*POROUS METAL PLASTICITY, RELATIVE DENSITY=0.98
1.,1.25,1.
*VOID NUCLEATION
0.1,0.06,0.04
*POROUS FAILURE CRITERIA
0.8,0.5
*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
5,6,4005,4006,6005,6006
25,26,4025,4026,6025,6026
*NSET, NSET=B3ALL
7,8,4007,4008,6007,6008
27,28,4027,4028,6027,6028
*NSET, NSET=SALL, GENERATE
1, 4, 1
9, 18, 1
101, 104, 1
201, 204, 1
301, 304, 1
401, 404, 1
501, 504, 1
601, 604, 1
701, 704, 1
1009, 1018, 1
1101, 1104, 1
1201, 1204, 1
1301, 1304, 1
1401, 1404, 1
1501, 1504, 1
1601, 1604, 1
1701, 1704, 1
2009, 2018, 1
2101, 2104, 1
2201, 2204, 1
2301, 2304, 1
2401, 2404, 1
2501, 2504, 1
2601, 2604, 1
2701, 2704, 1
3011, 3018, 1
3101, 3104, 1
3301, 3304, 1
4001, 4004, 1
4009, 4018, 1
4101, 4104, 1
4201, 4204, 1
4301, 4304, 1
4401, 4404, 1
4501, 4504, 1
4601, 4604, 1
4701, 4704, 1
5009, 5018, 1
5101, 5104, 1
5201, 5204, 1
5301, 5304, 1
5401, 5404, 1
5501, 5504, 1
5601, 5604, 1
5701, 5704, 1
6001, 6004, 1
6009, 6018, 1
6101, 6104, 1
6201, 6204, 1
6301, 6304, 1
6401, 6404, 1
6501, 6504, 1
6601, 6604, 1
6701, 6704, 1
7011, 7018, 1
7101, 7104, 1
7301, 7304, 1
8009, 8018, 1
8101, 8104, 1
8201, 8204, 1
8301, 8304, 1
8401, 8404, 1
8501, 8504, 1
8601, 8604, 1
8701, 8704, 1
*NSET, NSET=SFACE, GENERATE
11, 18, 1
1011, 1018, 1
2011, 2018, 1
3011, 3018, 1
4011, 4018, 1
5011, 5018, 1
6011, 6018, 1
7011, 7018, 1
8011, 8018, 1
*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
1009,1011,1012,1013,1014,1101,1102
1201,1202,1301,1302,1401,1402,1501,1502
1601,1602,1701,1702
2009,2011,2012,2013,2014,2101,2102
2201,2202,2301,2302,2401,2402,2501,2502
2601,2602,2701,2702
3011,3012,3013,3014,3101,3102,3301,3302
4001,4003,4005,4007,4009,4011,4012,4013,4014,4101,4102
4201,4202,4301,4302,4401,4402,4501,4502
4601,4602,4701,4702
5009,5011,5012,5013,5014,5101,5102
5201,5202,5301,5302,5401,5402,5501,5502
5601,5602,5701,5702
6001,6003,6005,6007,6009,6011,6012,6013,6014,6101,6102
6201,6202,6301,6302,6401,6402,6501,6502
6601,6602,6701,6702
7011,7012,7013,7014,7101,7102,7301,7302
8009,8011,8012,8013,8014,8101,8102
8201,8202,8301,8302,8401,8402,8501,8502
8601,8602,8701,8702
25,27,4025,4027,6025,6027
*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
1010,1015,1016,1017,1018,1103,1104
1203,1204,1303,1304,1403,1404,1503,1504
1603,1604,1703,1704
2010,2015,2016,2017,2018,2103,2104
2203,2204,2303,2304,2403,2404,2503,2504
2603,2604,2703,2704
3015,3016,3017,3018,3103,3104,3303,3304
4002,4004,4006,4008,4010,4015,4016,4017,4018,4103,4104
4203,4204,4303,4304,4403,4404,4503,4504
4603,4604,4703,4704
5010,5015,5016,5017,5018,5103,5104
5203,5204,5303,5304,5403,5404,5503,5504
5603,5604,5703,5704
6002,6004,6006,6008,6010,6015,6016,6017,6018,6103,6104
6203,6204,6303,6304,6403,6404,6503,6504
6603,6604,6703,6704
7015,7016,7017,7018,7103,7104,7303,7304
8010,8015,8016,8017,8018,8103,8104
8203,8204,8303,8304,8403,8404,8503,8504
8603,8604,8703,8704
26,28,4026,4028,6026,6028
*ELSET, ELSET=EALL1
1,2,3,4,5,11,101,201,301,401,501,601,701
1005,1011,1101,1201,1301,1401,1501,1601,1701
2005,2011,2101,2201,2301,2401,2501,2601,2701
3011,3101,3301
4001,4002,4003,4004,4005,4011,4101,4201,4301,4401,4501
4601,4701
5005,5011,5101,5201,5301,5401,5501,5601,5701
6001,6002,6003,6004,6005,6011,6101,6201,6301,6401,6501
6601,6701
7011,7101,7301
8005,8011,8101,8201,8301,8401,8501,8601,8701
23, 24, 4023, 4024, 6023, 6024
*NSET, NSET=ALL
B2ALL, B3ALL, SALL
*BOUNDARY
BOTTOM,2,2
SFACE,3,3
*INITIAL CONDITION, TYPE=FIELD, VARIABLE=1, section specification=uniform
 ALL, 0.
*ELSET, ELSET=EALL
EALL1, 
*ELSET, ELSET=QA_TEST
EALL,
**
*STEP
*DYNAMIC,EXPLICIT
,0.001
*FIELD,VARIABLE=1, section specification=uniform
 B2ALL, 100.0
 B3ALL, 100.0
 SALL,  100.0
*BOUNDARY,TYPE=VELOCITY
 TOP, 2, 2, 10.
**
*FILE OUTPUT,TIMEMARKS=YES,NUM=1
*EL FILE
 MISES,
 PEEQ,
 PE,
**
********************
*OUTPUT,FIELD,NUM=1
*ELEMENT OUTPUT,ELSET=QA_TEST
FV,PEEQ
***OUTPUT,HISTORY,TIME INTERV=1E-3
***ELEMENT OUTPUT,ELSET=EALL
**FV,
*END STEP