*HEADING
 Transfer from Standard to Standard : elastic
 - Second Standard analysis
*IMPORT,UPDATE=NO,STATE=NO,STEP=1
EALL, 
*RESTART, WRITE
*FILE FORMAT,ZERO INC
*NODE,NSET=ALL1
21,0.0,4.0,0.0
22,1.0,4.0,0.0
23,1.0,5.0,0.0
24,0.0,5.0,0.0
25,0.0,4.0,1.0
26,1.0,4.0,1.0
27,1.0,5.0,1.0
28,0.0,5.0,1.0
*NSET,NSET=DISP2
22,23,26,27
**
*NSET,NSET=YZPLANE3
21,25,24,28
*NSET,NSET=YZPLANE
YZPLANE1,YZPLANE2,YZPLANE3
**
*NSET,NSET=XZPLANE3
21,22,26,25
*NSET,NSET=XZPLANE
XZPLANE1,XZPLANE2,XZPLANE3
**
*NSET,NSET=XYPLANE3
21,22,23,24
*NSET,NSET=XYPLANE
XYPLANE1,XYPLANE2,XYPLANE3
**
*ELEMENT,TYPE=COH3D8,ELSET=EALL1
21,21,22,23,24,25,26,27,28
*COHESIVE SECTION,ELSET=EALL1,MATERIAL=MAT2,RESPONSE=TRACTION SEPARATION,
STACK DIRECTION=1,THICKNESS=GEOMETRY
*MATERIAL,NAME=MAT2
*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
ALL1,2,3
YZPLANE,1
DISP, 1
*ELSET,ELSET=QA_EALL
EALL,EALL1
*NSET,NSET=QA_ALL
ALL,ALL1
*STEP,NLGEOM
*STATIC
0.001, 1.0, 1.0E-5, 0.05
*BOUNDARY, TYPE=VELOCITY
DISP1,1,1,0.005
DISP2,1,1,0.01
*OUTPUT, FIELD
*ELEMENT OUTPUT, ELSET=QA_EALL
S, E, SDEG, DMICRT, STATUS
*NODE OUTPUT, NSET=QA_ALL
U, RF
*OUTPUT, HISTORY
*ELEMENT OUTPUT, ELSET=QA_EALL
S, E, SDEG, DMICRT, STATUS
ENER
ELEN
*ENERGY OUTPUT, ELSET=QA_EALL
ALLSE, ALLKE, ALLDMD, ALLIE
*ENERGY OUTPUT
ETOTAL, ALLWK
*END STEP