*HEADING
 Transfer from Standard to Standard: elastic+plastic
 - First Standard analysis
*RESTART,WRITE
*NODE,NSET=ALL
1,0.0,0.0,0.0
2,1.0,0.0,0.0
3,1.0,1.0,0.0
4,0.0,1.0,0.0
5,0.0,0.0,1.0
6,1.0,0.0,1.0
7,1.0,1.0,1.0
8,0.0,1.0,1.0
11,0.0,2.0,0.0
12,1.0,2.0,0.0
13,1.0,3.0,0.0
14,0.0,3.0,0.0
15,0.0,2.0,1.0
16,1.0,2.0,1.0
17,1.0,3.0,1.0
18,0.0,3.0,1.0
*NSET,NSET=DISP
2,3,6,7
*NSET,NSET=DISP1
12,13,16,17
**
*NSET,NSET=YZPLANE1
1,5,4,8
*NSET,NSET=YZPLANE2
11,15,14,18
*NSET,NSET=YZPLANE
YZPLANE1,YZPLANE2
**
*NSET,NSET=XZPLANE1
1,2,6,5
*NSET,NSET=XZPLANE2
11,12,16,15
*NSET,NSET=XZPLANE
XZPLANE1,XZPLANE2
**
*NSET,NSET=XYPLANE1
1,2,3,4
*NSET,NSET=XYPLANE2
11,12,13,14
*NSET,NSET=XYPLANE
XYPLANE1,XYPLANE2
**
*ELEMENT,TYPE=COH3D8,ELSET=EALL
1,1,2,3,4,5,6,7,8
11,11,12,13,14,15,16,17,18
*COHESIVE SECTION,ELSET=EALL,MATERIAL=MAT1,RESPONSE=TRACTION SEPARATION,
STACK DIRECTION=1,THICKNESS=GEOMETRY
*MATERIAL,NAME=MAT1
*ELASTIC,TYPE=TRACTION
4.0E6,2.0E6,2.0E6
*DAMAGE INITIATION, CRITERION=QUADS
8000., 2000., 2000.
*DAMAGE EVOLUTION, TYPE=DISPLACEMENT, MODE MIX RATIO=TRACTION, MIXED MODE BEHAVIOR=TABULAR, SOFTENING=EXPONENTIAL
0.006, 2.0, 0.0
0.007, 2.0, 1.0
*BOUNDARY
ALL,2,3
YZPLANE,1
*STEP,NLGEOM, INC=1000
*STATIC
0.001, 1.0, 1.0E-5, 0.05
*BOUNDARY
DISP ,1,1,0.01
DISP1,1,1,0.005
*OUTPUT, FIELD
*ELEMENT OUTPUT, ELSET=EALL
S, E, SDEG, DMICRT, STATUS
*NODE OUTPUT, NSET=ALL
U, RF
*OUTPUT, HISTORY
*ELEMENT OUTPUT, ELSET=EALL
S, E, SDEG, DMICRT, STATUS
ENER
ELEN
MMIXDMI,MMIXDME
*ENERGY OUTPUT, ELSET=EALL
ALLSE, ALLKE, ALLDMD, ALLIE
*ENERGY OUTPUT
ETOTAL, ALLWK
*END STEP
*STEP,NLGEOM, INC=1000
*STATIC
0.001, 1.0, 1.0E-5, 0.05
*BOUNDARY
DISP1,1,1,0.01
*END STEP