*HEADING
 Transfer from Standard to Explicit: Test for C3D10M element 
 - Standard analysis
 - loading in shear
*NODE,NSET=ALL
1, 0.0,0.0,0.0
2, 1.0,0.0,0.0
3, 1.0,1.0,0.0
4, 0.0,1.0,0.0
5, 0.0,0.0,1.0
6, 1.0,0.0,1.0
7, 1.0,1.0,1.0
8, 0.0,1.0,1.0
9, 0.5,0.0,0.0
10,1.0,0.5,0.0
11,0.5,1.0,0.0
12,0.0,0.5,0.0
13,0.5,0.0,1.0
14,1.0,0.5,1.0
15,0.5,1.0,1.0
16,0.0,0.5,1.0
17,0.0,0.0,0.5
18,1.0,0.0,0.5
19,1.0,1.0,0.5
20,0.0,1.0,0.5
21,0.5,0.5,0.5
22,0.5,0.5,0.0
23,0.5,0.5,1.0
24,0.5,0.0,0.5
25,1.0,0.5,0.5
26,0.5,1.0,0.5
27,0.0,0.5,0.5
*ELEMENT, TYPE=C3D10M, ELSET=EALL
1,1,2,4,7,9,22,12,21,25,26
2,2,3,4,7,10,11,22,25,19,26
3,1,6,2,7,24,18,9,21,14,25
4,1,5,6,8,17,13,24,27,16,23
5,1,4,8,7,12,20,27,21,26,15
6,1,8,6,7,27,23,24,21,15,14
*SECTION CONTROLS, NAME=EC-1, HOURGLASS=STIFFNESS
*SOLID SECTION, ELSET=EALL, MATERIAL=STEEL, CONTROLS=EC-1
*MATERIAL,NAME=STEEL
*ELASTIC
 200.E9, 0.3
*DENSITY
 1000., 
*BOUNDARY
 1, 1,3
 2, 1,3
 5, 1,2
 6, 1,2
 9, 1,3
13, 1,2
17, 1,2
18, 1,2
24, 1,2
 3, 2,3
 4, 2,3
 7, 2,2
 8, 2,2
11, 2,3
15, 2,2
19, 2,2
20, 2,2
26, 2,2
*RESTART,WRITE
**
**
*STEP,NLGEOM,INC=50
*STATIC
 0.1, 1.
*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 
15, 1, 1, 0.2 
19, 1, 1, 0.2 
20, 1, 1, 0.2 
26, 1, 1, 0.2 
*PRINT,FREQ=1
*EL FILE, DIRECTIONS=YES
 S,E
*NODE FILE
 U,COORD
*EL PRINT,FREQ=1
 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=EALL
 S,E
*OUTPUT,FIELD
*NODE OUTPUT
 U,COORD
*OUTPUT,HISTORY
*NODE OUTPUT, NSET=ALL
 U,COORD
*END STEP