*HEADING
 Transfer from Standard to Explicit : Test for B31 element
 - Standard analysis
 - loading in tension
*NODE, NSET=ALL
*NSET, NSET=LEFT
*NSET, NSET=RIGHT
*ELEMENT, TYPE=B31, ELSET=RECT
*ELEMENT, TYPE=B31, ELSET=BOX
*ELEMENT, TYPE=B31, ELSET=CIRC
*ELEMENT, TYPE=B31, ELSET=HEX
*ELEMENT, TYPE=B31, ELSET=I
*ELEMENT, TYPE=B31, ELSET=L
*ELEMENT, TYPE=B31, ELSET=PIPE
*ELEMENT, TYPE=B31, ELSET=TRAP
*ELSET, ELSET=EALL
*BEAM SECTION,SECTION=RECT,ELSET=RECT,MATERIAL=STEEL
0.1,0.2
*BEAM SECTION,SECTION=BOX,ELSET=BOX,MATERIAL=STEEL
1.0,1.0,0.2,0.2,0.1,0.1
*BEAM SECTION,SECTION=CIRC,ELSET=CIRC,MATERIAL=STEEL
1.0,
0.0, 1.0, 0.0
*BEAM SECTION,SECTION=HEX,ELSET=HEX,MATERIAL=STEEL
1.0,0.1
*BEAM SECTION,SECTION=I,ELSET=I,MATERIAL=STEEL
0.1,1.0,0.5,0.5,0.1,0.1,0.1
*BEAM SECTION,SECTION=L,ELSET=L,MATERIAL=STEEL
0.5,1.0,0.1,0.1
*BEAM SECTION,SECTION=PIPE,ELSET=PIPE,MATERIAL=STEEL
1.0,0.1
*BEAM SECTION,SECTION=TRAPEZOID,ELSET=TRAP,MATERIAL=STEEL
2.0,1.0,1.0,0.25
*MATERIAL,NAME=STEEL
*ELASTIC
 200.E9, 0.3
*DENSITY
 7850.,
*BOUNDARY
 LEFT, 1,6
 RIGHT, 2,6
*RESTART, WRITE
**
**
*ELSET,ELSET=QA_TEST_ALLELEMS
EALL,
**
*NSET, NSET=QA_TEST_ALLNODES
ALL
**
*STEP,NLGEOM,INC=50
*STATIC
 0.1, 1.
*BOUNDARY, TYPE=VELOCITY
 RIGHT, 1, 1, 0.2
*PRINT,FREQ=1
*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=QA_TEST_ALLELEMS
 S,E
*OUTPUT,FIELD
*NODE OUTPUT
 U,COORD
*OUTPUT,HISTORY
*NODE OUTPUT, NSET=QA_TEST_ALLNODES
 U,COORD
*END STEP