*HEADING
 Linear Kinematics Element Test - B22
*NODE,NSET=NOUT
1,0.0,0.0
2,1.0,0.0
3,0.5,0.0
11,2.0,0.25
12,3.0,0.25
13,2.5,0.25
21,4.0,0.50
22,5.0,0.50
23,4.5,0.50
*NSET,NSET=QA_TEST
NOUT,
*ELEMENT,TYPE=B22,ELSET=BEAM
1,1,3,2
11,11,13,12
21,21,23,22
*BEAM SECTION, SECTION=RECT, ELSET=BEAM, MATERIAL=STEEL, POISSON=0.3
.1, .2
*MATERIAL, NAME=STEEL
*ELASTIC
1.0e05,0.3
*DENSITY
100.0, 
** history data
*STEP,NLGEOM=NO 
*DYNAMIC,EXPLICIT
,1.0
** apply boundary conditions
*BOUNDARY,TYPE=VELOCITY
** first element loading (moment)
1,1,2,0.0
1,6,6,1.0
2,1,2,0.0
2,6,6,-1.0
**
3,1,2,0.0
3,6,6,0.0
** second element loading (axial load)
11,1,1,-1.0
11,2,2,0.0
11,6,6,0.0
12,1,1,1.0
12,2,2,0.0
12,6,6,0.0
**
13,1,1,0.0
13,2,2,0.0
13,6,6,0.0
** third element loading (shear load)
21,1,1,0.0
21,2,2,1.0
21,6,6,0.0
22,1,1,0.0
22,2,2,-1.0
22,6,6,0.0
23,1,1,0.0
23,2,2,0.0
23,6,6,0.0
*BULK VISCOSITY
0,0
*RESTART,WRITE,NUMBER=1
************************
*FILE OUTPUT,NUMBER=1
*NODE FILE
U,
*EL FILE
ELEN,
S, 
SF,
***********************
*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=BEAM
**S,
**LE,
*END STEP