*HEADING
 Linear Kinematics Element Test - C3D8I with *ORIENTATION
*NODE
1,0.0,0.0,1.0
2,1.0,0.0,1.0
3,1.0,0.0,0.0
4,0.0,0.0,0.0
5,0.0,1.0,1.0
6,1.0,1.0,1.0
7,1.0,1.0,0.0
8,0.0,1.0,0.0
11,1.25,1.25,2.25
12,2.25,1.25,2.25
13,2.25,1.25,1.25
14,1.25,1.25,1.25
15,1.25,2.25,2.25
16,2.25,2.25,2.25
17,2.25,2.25,1.25
18,1.25,2.25,1.25
*ORIENTATION, NAME=MATAXES
1.0,0.,0.,0.,1.,0.
3,45.0
*NSET,NSET=FRONT1
2,3,7,6
*NSET,NSET=BACK1
1,4,8,5
*NSET,NSET=FRONT2
12,13,17,16
*NSET,NSET=BACK2
11,14,18,15
*NSET,NSET=QA_TEST
FRONT1,BACK1,FRONT2,BACK2
*ELEMENT,TYPE=C3D8I,ELSET=ALL
1,1,2,3,4,5,6,7,8
11,11,12,13,14,15,16,17,18
*SOLID SECTION, ELSET=ALL, MATERIAL=STEEL, ORIENTATION=MATAXES
1.0, 
*MATERIAL, NAME=STEEL
*ELASTIC, TYPE=ENGINEERING CONSTANTS
1.0e05,2.0e05,3.0e05,0.1,0.2,0.3,0.1e05,0.2e05
0.3e05, 
*DENSITY
100.0, 
** history data
*STEP,NLGEOM=NO
*DYNAMIC,EXPLICIT
,1.0
** apply boundary conditions
*BOUNDARY,TYPE=VELOCITY
** loading of element 1 (axial stretch)
**
FRONT1,1,1,1.0
FRONT1,2,3,0.0
BACK1,1,1,-1.0
BACK1,2,3,0.0
** loading of element 2 (shear deformation)
**
FRONT2,1,1,0.0
FRONT2,2,2,1.0
FRONT2,3,3,0.0
BACK2,1,1,0.0
BACK2,2,2,-1.0
BACK2,3,3,0.0
*BULK VISCOSITY
0,0
*RESTART,WRITE,NUMBER=1
********
*FILE OUTPUT,NUMBER=1
*NODE FILE
U,
*EL FILE
ELEN,
S, 
E,
*********
***********************
*OUTPUT, FIELD, NUMBER INTER=1
*NODE OUTPUT,NSET=QA_TEST
U,
*OUTPUT,HISTORY,TIME INTERVAL=1.0
*ENERGY OUTPUT,VAR=PRESELECT
***********************
*END STEP