*HEADING
 Linear Kinematics Element Test - COH3D6
*NODE, NSET=NALL
11,0.0,0.0,1.0
12,1.0,0.0,1.0
13,1.0,0.0,0.0
14,0.0,0.0,0.0
15,0.0,1.0,1.0
16,1.0,1.0,1.0
17,1.0,1.0,0.0
18,0.0,1.0,0.0
*SYSTEM
2, 0, 0
*NODE, NSET=NALL
21,0.0,0.0,1.0
22,1.0,0.0,1.0
23,1.0,0.0,0.0
24,0.0,0.0,0.0
25,0.0,1.0,1.0
26,1.0,1.0,1.0
27,1.0,1.0,0.0
28,0.0,1.0,0.0
*ELEMENT,TYPE=COH3D6,ELSET=EL1
11, 11, 12, 14, 15, 16, 18 
12, 13, 14, 12, 17, 18, 16
*ELEMENT,TYPE=COH3D6,ELSET=EL2
21, 21, 22, 24, 25, 26, 28 
22, 23, 24, 22, 27, 28, 26
*ELSET, ELSET=ELALL
EL1, EL2
*ELSET, ELSET=QA_TEST_ELALL
ELALL
*NSET, NSET=QA_TEST_NALL
NALL
*NSET,NSET=TOP1
15, 16, 17, 18
*NSET, NSET=TOP2
25, 26, 27, 28
*NSET,NSET=BOT1
11, 12, 13, 14
*NSET, NSET=BOT2
21, 22, 23, 24
**
** Thickness direction for each element is +2
**
*COHESIVE SECTION, ELSET=ELALL, MATERIAL=MAT, THICKNESS=GEOMETRY, RESPONSE=CONTINUUM
*MATERIAL, NAME=MAT
*ELASTIC
1.0E05,0.3
*DENSITY
100.0, 
*BOUNDARY
TOP1, 1, 1
TOP1, 3, 3
BOT1, 1, 1
BOT1, 3, 3
TOP2, 2, 3
BOT2, 2, 3
**
*STEP,NLGEOM=NO
*DYNAMIC,EXPLICIT
,1.0
*BOUNDARY, TYPE=VELOCITY
**
** Loading of elements 11 and 12 (axial stretch)
**
TOP1, 2, 2, 1.0
BOT1, 2, 2, -1.0
**
**Loading of element 21 and 22 (shear deformation) 
**
TOP2, 1, 1, 1.0
BOT2, 1, 1, -1.0
**
**Output requests
**
*OUTPUT, FIELD, NUMBER INTERVAL=20, TIME MARKS=YES
*NODE OUTPUT,NSET=QA_TEST_NALL
U, RF
*ELEMENT OUTPUT, ELSET=QA_TEST_ELALL
E, S
*OUTPUT, HISTORY, TIME INTERVAL=0.01
*ENERGY OUTPUT, ELSET=EL1
ALLIE, ALLSE, ALLKE
*ENERGY OUTPUT, ELSET=EL2
ALLIE, ALLSE, ALLKE
*ENERGY OUTPUT
ALLWK, ETOTAL
*END STEP