*HEADING
 Transfer from Standard to Explicit : Test for three 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.
 9, 0.,0., 2.
10, 2.,0.,2.
11, 0.,2.,2.
12, 2.,2.,2.
13, 0.,0., 3.
14, 2.,0.,3.
15, 0.,2.,3.
16, 2.,2.,3.
*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
 11, 5,6,8,7,9,10,12,11
 12, 9,10,12,11,13,14,16,15
*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
 9, 1,2
10, 1,2
11, 2,2
12, 2,2
13, 1,2
14, 1,2
15, 2,2
16, 2,2
*RESTART,WRITE
**
*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
11, 1, 1, 0.2
12, 1, 1, 0.2
15, 1, 1, 0.2
16, 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,
*END STEP