*HEADING
 Linear Kinematics Element Test - CAX4R with *ORIENTATION
*NODE,NSET=NOUT
1,0.25,0.25
2,1.25,0.25
3,1.25,1.25
4,0.25,1.25
11,1.50,1.50
12,2.50,1.50
13,2.50,2.50
14,1.50,2.50
*NSET,NSET=QA_TEST
NOUT,
*ELEMENT,TYPE=CAX4R,ELSET=ALL
1,1,2,3,4
11,11,12,13,14
*ORIENTATION, NAME=MATAXES
1.0,0.,0.,0.,1.,0.
3,45.0
*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 deformation)
**
1,1,1,-1.0
1,2,2,0.0
2,1,1,1.0
2,2,2,0.0
3,1,1,1.0
3,2,2,0.0
4,1,1,-1.0
4,2,2,0.0
** loading of element 2 (shearing deformation)
**
11,1,1,0.0
11,2,2,-1.0
12,1,1,0.0
12,2,2,1.0
13,1,1,0.0
13,2,2,1.0
14,1,1,0.0
14,2,2,-1.0
*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
***********************
***OUTPUT,HISTORY,TIME INTERVAL=0.001
***NODE OUTPUT,NSET=NOUT
**U,
**RF,
***ENERGY OUTPUT
**ALLKE,ALLIE,ALLSE,ALLAE,ALLVD,ALLPD,ALLWK,ETOTAL,
**DT,
***ELEMENT OUTPUT,ELSET=ALL
**S,
**LE,
*END STEP