*HEADING
 fld criterion with hill plasticity
*RESTART,WRITE,NUMBER INTERVAL=10
*PREPRINT,MODEL=YES
*NODE,NSET=NALL
1,0,0,0
2,1,0,0
3,1,1,0
4,0,1,0
5,0,0,0.1
6,1,0,0.1
7,1,1,0.1
8,0,1,0.1
9,2,0,0
10,3,0,0
11,3,1,0
12,2,1,0
13,4,0,0
14,5,0,0
15,5,1,0
16,4,1,0
17,6,0,0
18,7,0,0
19,7,1,0
20,6,1,0
21,8,0,0
22,9,0,0
23,9,1,0
24,8,1,0
25,10,0,0
26,12,0,0
27,12,2,0
28,10,2,0
*******CONTINUUM SHELL**********
*ELEMENT,TYPE=SC8R,ELSET=SHELL
1,1,2,3,4,5,6,7,8
*NSET,NSET=CONTINUUM_BOTTOM
1,2,5,6
*NSET,NSET=CONTINUUM_TOP
3,4,8,7
*NSET,NSET=CONTINUUM_LEFT
1,4,5,8
*NSET,NSET=CONTINUUM_RIGHT
2,3,6,7
*NSET,NSET=CONTINUUM_BACK
1,2,3,4
*NSET,NSET=CONTINUUM_FRONT
5,6,7,8
*NSET,NSET=CONTINUUM_ALL
CONTINUUM_BOTTOM,CONTINUUM_TOP,CONTINUUM_LEFT,CONTINUUM_RIGHT
CONTINUUM_BACK,CONTINUUM_FRONT
*******SHELL*****************
*ELEMENT,TYPE=S4R,ELSET=SHELL
2,9,10,11,12
*ELEMENT,TYPE=S4R,ELSET=SHELL
3,13,14,15,16
*NSET,NSET=SHELL_BOTTOM
9,10,13,14
*NSET,NSET=SHELL_TOP
12,11,16,15
*NSET,NSET=SHELL_LEFT
9,12,13,16
*NSET,NSET=SHELL_RIGHT
10,11,14,15
*NSET,NSET=SHELL_ALL
SHELL_BOTTOM,SHELL_TOP,SHELL_LEFT,SHELL_RIGHT
************CPS4R AND MEMBRANE***************
*ELEMENT,TYPE=CPS4R,ELSET=SOLID
4,17,18,19,20
*ELEMENT,TYPE=M3D4R,ELSET=MEMBRANE
5,21,22,23,24
*ELEMENT,TYPE=M3D4,ELSET=MEMBRANE
6,25,26,27,28
*NSET,NSET=PLANE_BOTTOM
17,18,21,22,25,26
*NSET,NSET=PLANE_LEFT
17,20,21,24,25,28
*NSET,NSET=PLANE_TOP
19,20,23,24
*NSET,NSET=MEMBRANE_TOP
27,28
*NSET,NSET=PLANE_RIGHT
18,19,22,23
*NSET,NSET=MEMBRANE_RIGHT
26,27
*NSET,NSET=PLANE_ALL
PLANE_BOTTOM,PLANE_TOP,PLANE_LEFT,PLANE_RIGHT,
MEMBRANE_RIGHT,MEMBRANE_TOP
***************BOUNDARY************************
*BOUNDARY
CONTINUUM_BOTTOM,2,2
CONTINUUM_LEFT,1,1
CONTINUUM_ALL,3,3
SHELL_BOTTOM,2,2
SHELL_LEFT,1,1
SHELL_ALL,3,6
PLANE_BOTTOM,2,2
PLANE_LEFT,1,1
PLANE_ALL,3,3
***************************************
*ORIENTATION,NAME=RECT
 1.0, 0.0, 0.0, 0.0, 1.0, 0.0
 3, 0.0
*SHELL SECTION,MATERIAL=MAT_HILL,ELSET=SHELL,CONTROLS=CONT,ORIENT=RECT
0.1
*SOLID SECTION,MATERIAL=MAT_HILL,ELSET=SOLID,CONTROLS=CONT,ORIENT=RECT
1.0
*MEMBRANE SECTION,MATERIAL=MAT_HILL,ELSET=MEMBRANE,CONTROLS=CONT,ORIENT=RECT
0.1
*SECTION CONTROLS,ELEMENT DELETION=YES,MAX DEGRADATION=0.75,NAME=CONT
*ELSET,ELSET=EALL
SOLID,SHELL,MEMBRANE
*ELSET,ELSET=QA_TEST_ALLELEMENTS
EALL
***************************************
*MATERIAL,NAME=MAT_HILL
*DENSITY
8.96E3
*ELASTIC
124.E9,0.34
*PLASTIC,HARDENING=ISOTROPIC
  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
*POTENTIAL
1.5,1.2,1.0,1.0,1.0,1.0
*DAMAGE INITIATION,CRITERION=FLD
3E-2
*DAMAGE EVOLUTION,TYPE=ENERGY,SOFTENING=LINEAR
 1E6
*AMPLITUDE,NAME=AMP1,DEFINITION=DECAY
-1,1,0,-5
*STEP,nlgeom=yes,inc=1000
*static
 0.01,0.5,,0.01
*BOUNDARY,TYPE=DISPLACEMENT,AMP=AMP1
CONTINUUM_TOP,2,2,1
CONTINUUM_RIGHT,1,1,1
SHELL_TOP,2,2,1
SHELL_RIGHT,1,1,1
PLANE_TOP,2,2,1
PLANE_RIGHT,1,1,1
MEMBRANE_TOP,2,2,2
MEMBRANE_RIGHT,1,1,2
**
**
*OUTPUT,FIELD,freq=10
*ELEMENT OUTPUT,ELSET=QA_TEST_ALLELEMENTS
STATUS,SDEG,DMICRT
PEEQ,S
*NODE OUTPUT,NSET=NALL
U,
*OUTPUT,HISTORY
*ELEMENT OUTPUT,ELSET=EALL
STATUS,SDEG,DMICRT
PEEQ,LEP,SP,MISES,PRESS
*END STEP