*HEADING
 Linear Kinematics Element Test - SAX1 with *SHELL SECTION
*NODE,NSET=NOUT
1,0.25,0.0
2,1.25,0.0
11,0.50,0.25
12,1.50,0.25
21,0.75,0.50
22,1.75,0.50
31,2.0,0.75
32,3.0,0.75
*NSET,NSET=QA_TEST
NOUT,
*ELEMENT,TYPE=SAX1,ELSET=ALL
1,1,2
11,11,12
21,21,22
31,31,32
*SHELL SECTION, ELSET=ALL, MATERIAL=STEEL
0.1, 
*MATERIAL, NAME=STEEL
*ELASTIC
1.0e05,0.0
*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
1,6,6,0.0
2,1,1,1.0
2,2,2,0.0
2,6,6,0.0
**loading of element 2 (bending deformation)
11,1,2,0.0
11,6,6,-1.0
12,1,2,0.0
12,6,6,1.0
**loading of element 3 (hoop deformation)
21,1,1,1.0
21,2,2,0.0
21,6,6,0.0
22,1,1,1.0
22,2,2,0.0
22,6,6,0.0
**loading of element 4 (tranverse shear deformation)
31,1,1,0.0
31,2,2,1.0
31,6,6,0.0
32,1,1,0.0
32,2,2,-1.0
32,6,6,0.0
*BULK VISCOSITY
0,0
*RESTART,WRITE,NUMBER=1
*FILE OUTPUT,NUMBER=1
*NODE FILE
U,
*EL FILE
ELEN, 
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=ALL
**S,
**LE,
*END STEP