*HEADING
 Transfer from Standard to Explicit : Test for C3D8R element 
 - Standard analysis
 - loading in shear
 - with orientation
*NODE,NSET=ALL
 1,
 2, 2., 0.
 3, 0., 2.
 4, 2., 2.
 5, 0.,0., 1.
 6, 2.,0.,1.
 7, 0.,2.,1.
 8, 2.,2.,1.
*NSET,NSET=SIDE
 3,4
*ORIENTATION,NAME=ORIE
1.0,1.0,0,-1.0,1.0,0
*ELEMENT, TYPE=C3D8R, ELSET=SHELL
 10, 1,2,4,3,5,6,8,7
*SOLID SECTION, ELSET=SHELL, MATERIAL=STEEL,ORIENTATION=ORIE
*MATERIAL,NAME=STEEL
*ELASTIC, TYPE=ENGINEERING CONSTANTS
2.0E11, 1.0E11, 1.0E11, 0.3,0.23,0.34, 7.69E10, 7.69E10
9.0E9, 
*DENSITY
7850.0, 
*BOUNDARY
 1, 1,3
 2, 1,3
 3, 2,3
 4, 2,3
 5, 1,2
 6, 1,2
 7, 2,2
 8, 2,2
*RESTART,WRITE
**
**
*ELSET,ELSET=QA_TEST_ALLELEMS
SHELL,
**
*NSET, NSET=QA_TEST_ALLNODES
ALL, SIDE
**
**
*ELSET,ELSET=QA_TEST_ALLELEMS
SHELL,
**
*NSET, NSET=QA_TEST_ALLNODES
ALL, SIDE, QA_TEST_ALLNODES
**
*STEP,NLGEOM,INC=50
*STATIC
 0.1, 1.
**CONTROLS, PARAMETERS=FIELD, FIELD=DISPLACEMENT
** ,,,1000.,
*BOUNDARY, TYPE=VELOCITY
 3, 1, 1, 0.2
 4, 1, 1, 0.2
 7, 1, 1, 0.2
 8, 1, 1, 0.2
*PRINT,FREQ=1
*EL FILE, DIRECTIONS=YES
S, 
E, 
*NODE FILE
 U, 
*EL PRINT,FREQ=100
 S,
 E,
 PEEQ,
*ENERGY PRINT 
 ALLKE, ALLSE,ALLWK,ALLIE,ETOTAL 
*NODE PRINT,FREQ=1
 U,
 COORD,
 RF,
*OUTPUT,FIELD,VARIABLE=PRESELECT,FREQUENCY=9999
*OUTPUT,FIELD
*ELEMENT OUTPUT
S, 
E, 
*OUTPUT,HISTORY
*ELEMENT OUTPUT, ELSET=QA_TEST_ALLELEMS
S, 
E, 
*OUTPUT,FIELD
*NODE OUTPUT
 U, 
*OUTPUT,HISTORY
*NODE OUTPUT, NSET=QA_TEST_ALLNODES
 U, 
*END STEP