*HEADING
 Test of triangular and prism elements in a tensile test
 Element types: CPS3, CPE3, CAX3, M3D3, S3R, C3D6, C3D4
*NODE
101,1000.,0.
102,1001.,0.
103,1000.5,.5
104,1001.,1.
105,1000.,1.
**
201,1002.,0.
202,1003.,0.
203,1002.5,.5
204,1003.,1.
205,1002.,1.
**
301,1004.,0.
302,1005.,0.
303,1004.5,.5
304,1005.,1.
305,1004.,1.
**
401,1006.,0.
402,1007.,0.
403,1006.5,.5
404,1007.,1.
405,1006.,1.
**
501,1008.,0.
502,1009.,0.
503,1008.5,.5
504,1009.,1.
505,1008.,1.
**
601,1010.,0.
602,1011.,0.
603,1010.5,.5
604,1010.,0.,-1.
605,1011.,0.,-1.
606,1010.5,.5,-1.
607,1011.,1.
608,1010.,1.
609,1011.,1.,-1.
610,1010.,1.,-1.
**
701,1012.,0.
702,1013.,0.
703,1013.,0.,-1.
704,1012.,0.,-1.
705,1012.,1.
706,1013.,1.
707,1013.,1.,-1.
708,1012.,1.,-1.
**
*NSET,NSET=BOTTOM,GEN
101,501,100
102,502,100
*NSET,NSET=BOTTOM
601,602,604,605
701,702,703,704
*NSET,NSET=SIDE,GEN
101,501,100
105,505,100
*NSET,NSET=SIDE
601,604,608,610
701,704,705,708
*NSET,NSET=NOUT
105,205,305,405
505,608,707
**
*ELEMENT,TYPE=CPS3
101,101,102,103
102,102,104,103
103,103,104,105
104,101,103,105
*ELEMENT,TYPE=CPE3 
201,201,202,203
202,202,204,203
203,203,204,205
204,201,203,205
*ELEMENT,TYPE=CAX3
301,301,302,303
302,302,304,303
303,303,304,305
304,301,303,305
*ELEMENT,TYPE=M3D3 
401,401,402,403
402,402,404,403
403,403,404,405
404,401,403,405
*ELEMENT,TYPE=C3D6
601,601,603,602,604,606,605
602,602,603,607,605,606,609
603,603,608,607,606,610,609
604,601,608,603,604,610,606
*ELEMENT,TYPE=C3D4
701,701,702,703,706
702,701,703,704,708
703,705,708,706,701
704,706,708,707,703
705,701,708,706,703
*ELSET,ELSET=SOLID2D,GEN
101,104,1
201,204,1
*ELSET,ELSET=SOLID3D,GEN
301,304,1
601,604,1
701,705,1
*ELSET,ELSET=SOLID,GEN
101,301,100
102,302,100
103,303,100
104,304,100
601,604,1
701,705,1
*ELSET,ELSET=MEM
401,402,403,404
*SOLID SECTION,ELSET=SOLID2D,MATERIAL=MAT
1., 
*SOLID SECTION,ELSET=SOLID3D,MATERIAL=MAT
1., 
*MEMBRANE SECTION,ELSET=MEM,MATERIAL=MAT
1., 
*ELEMENT,TYPE=S3R,ELSET=SHELL
501,501,502,503
502,502,504,503
503,503,504,505
504,501,503,505
*SHELL SECTION,ELSET=SHELL,MATERIAL=MAT,SECTION INTEGRATION=GAUSS
1.,
*MATERIAL,NAME=MAT
*DENSITY
1., 
*ELASTIC
1.,0.
*BOUNDARY
BOTTOM,2,2
SIDE,1,1
*AMPLITUDE,NAME=RAMP
0.,0.,100.,1.,200.,1.
*RESTART,WRITE,NUMBER INTERVAL=2,TIMEMARKS=NO
*NSET,NSET=LOADS1
104,204,404,504
105,205,405,505
*NSET,NSET=LOADS2,GEN
607,610,1
*ELSET,ELSET=QA_TEST_All_ELSETS_AUTO
SOLID, MEM, SOLID, MEM, SHELL, SHELL,
*NSET,NSET=QA_TEST_All_NSETS_AUTO
BOTTOM, BOTTOM, SIDE, SIDE, NOUT, LOADS1, LOADS2,
*STEP
*DYNAMIC,EXPLICIT
,200.
*CLOAD,AMP=RAMP
LOADS1,2,.004975
LOADS2,2,.002488
705,2,.0016667
706,2,.0033333
707,2,.0016667
708,2,.0033333
** FOR THE AXISYMMETRIC CASE, GIVE THE TOTAL LOAD  
** (.005*2*PI*R) R = 1004,1005
304,2,31.3849
305,2,31.4162
***OUTPUT,HISTORY,TIME INTERVAL=0.2
***ENERGY OUTPUT
**ALLKE,ALLIE,ALLSE,ALLAE,ALLVD,ALLWK,ETOTAL,DT
***NODE OUTPUT,NSET=NOUT
**U,
**RF,
*FILE OUTPUT,NUMBER INTERVAL=1,TIMEMARKS=YES
***EL FILE
**S,LE,
*NODE FILE
U,
***OUTPUT,FIELD,VARIABLE=PRESELECT,NUMBER INTERVAL=4,OP=NEW
***OUTPUT,HISTORY,VARIABLE=PRESELECT,TIME INTERVAL=50,OP=NEW
*OUTPUT, FIELD,NUMBER INTERVAL=1,TIMEMARKS=YES
*ELEMENT OUTPUT,ELSET=QA_TEST_All_ELSETS_AUTO
S
**,LE,
*NODE OUTPUT,NSET=QA_TEST_All_NSETS_AUTO
U,
*END STEP