**
** test import of ductile damage initiation
** Standard to Explicit
** base deck for: sx_x_ductile.inp
**
*HEADING
 ductile failure with Mises plasticity
*NODE,NSET=NALL-1
1,0,0
2,1,0
3,1,1
4,0,1
*NODE,NSET=NALL-2
11,2,0
12,3,0
13,3,1
14,2,1
*node,nset=nall-3
21,4,0
22,5,0
23,5,1
24,4,1
25,4,0,1
26,5,0,1
27,5,1,1
28,4,1,1
*nset,nset=x0
 1,4
 11,14
 21,24,25,28
*nset,nset=x1
 2,3
 12,13
 22,23,26,27
*nset,nset=y0
 1,2
 11,12
 21,22,25,26
*nset,nset=y1
 3,4
 13,14
 23,24,27,28
*nset,nset=z0
 21,22,23,24
*ELEMENT,TYPE=CPS4R,ELSET=SOLID-1
1,1,2,3,4
*element,type=c3d8r,elset=solid-2
3,21,22,23,24,25,26,27,28
*ELEMENT,TYPE=S4R,ELSET=Shell
2,11,12,13,14
*elset,elset=alle
1,2,3
*elset,elset=solid
1,3
***************************************
*SOLID SECTION,MATERIAL=MAT_MISES,ELSET=SOLID-1
1.0
*SOLID SECTION,MATERIAL=MAT_MISES,ELSET=SOLID-2
1.0
*Shell SECTION,MATERIAL=MAT_MISES,ELSET=Shell
1.0,5
***************************************
*MATERIAL,NAME=MAT_MISES
*Density
2000
*Elastic
20.E+010,	0.33
*plastic
2.e8,0.0
6.e8,2.0
*Damage Initiation, Criterion = Ductile 
 1.8,   -0.5,
 1.5,   -0.1,
 1.0, 	 0.0,
0.90,    0.1,
0.80,    0.3,
0.50,    0.6,
0.30,    1.0,
*damage evolution, type=energy, softening=linear
1.e9
**--------------------------------
*STEP,nlgeom=yes,inc=1000
*static
 0.004,0.04,,0.004
*BOUNDARY,TYPE=DISPLACEMENT
 nall-2,3,6
 y0,2,2
 x0,1,1
 z0,3,3
*boundary, type=velocity
 y1,2,2,20
 x1,1,1,1.
**
*restart,write
*OUTPUT,FIELD,freq=10
*ELEMENT OUTPUT
DMICRT
PEEQ
S
PE
*NODE OUTPUT
U,
*OUTPUT,HISTORY
*ELEMENT OUTPUT,ELSET=alle
DMICRT
PEEQ,
MISES
PRESS
TRIAX
*END STEP