*HEADING
   BENDING PROBLEM
*NODE,NSET=NALL
   1101,0. ,0.2
   1111, .4,0.2
   1201,0. ,0.2,.02
   1211, .4,0.2,.02
**
   11101,0.5,0.1
   11111, .9,0.1
   11201,0.5,0.1,.02
   11211, .9,0.1,.02
**
   1601,0. ,0.55
   1611, .4,0.55
   1701,0. ,0.55,.02
   1711, .4,0.55,.02
**
   11601,0.5,0.4
   11611, .9,0.4
   11701,0.5,0.4,.02
   11711, .9,0.4,.02
**
   2101,0. ,0.9
   2111, .4,0.9
   2201,0. ,0.9,.02
   2211, .4,0.9,.02
**
   3101,0. ,1.25
   3111, .4,1.25
   3201,0. ,1.25,.02
   3211, .4,1.25,.02
*NGEN,NSET=NALL
   1101,1111
   1201,1211
   1601,1611
   1701,1711
   11101,11111
   11201,11211
   11601,11611
   11701,11711
   2101,2111
   2201,2211
   3101,3111
   3201,3211
*NSET,NSET=SYM
1101,1201,11101,11201,
1601,1701,11601,11701
2101,2201,3101,3201
*NSET,NSET=END
1111,1211,11111,11211,
1611,1711,11611,11711
2111,2211,3111,3211
*ELEMENT,TYPE=S4R,ELSET=SHELL2
   1101,1101,1201,1202,1102
*ELEMENT,TYPE=S4R,ELSET=SHELL2O
   1601,1601,1701,1702,1602
*ELEMENT,TYPE=S4R,ELSET=SHELL3
   11101,11101,11201,11202,11102
*ELEMENT,TYPE=S4R,ELSET=SHELL3O
   11601,11601,11701,11702,11602
*ELEMENT,TYPE=S4R,ELSET=SHELL2A
   2101,2101,2201,2202,2102
*ELEMENT,TYPE=S4R,ELSET=SHELL2B
   3101,3101,3201,3202,3102
*ELGEN,ELSET=SHELL2
   1101,10,1,1
*ELGEN,ELSET=SHELL3
  11101,10,1,1
*ELGEN,ELSET=SHELL2O
   1601,10,1,1
*ELGEN,ELSET=SHELL3O
  11601,10,1,1
*ELGEN,ELSET=SHELL2A
   2101,10,1,1
*ELGEN,ELSET=SHELL2B
   3101,10,1,1
*ELSET,ELSET=ESYM
1101,11101,1601,11601,2101,3101
*ORIENTATION,NAME=ORI3,SYSTEM=RECT,DEFINITION=OFFSET TO NODES
2,4
3,0.0
*SHELL GENERAL SECTION,ELSET=SHELL2,COMPOSITE, POISSON=0.
0.006,3,STEEL
0.008,3,ALUMI
0.006,3,STEEL
*SHELL GENERAL SECTION,ELSET=SHELL2O,COMPOSITE, POISSON=0.0
0.006,3,STEEL,90.
0.008,3,ALUMI,90.
0.006,3,STEEL,90.
*SHELL GENERAL SECTION,ELSET=SHELL3,DENSITY=115.8, POISSON=0.
2.952E+09, 0., 2.952E+09,0.,0.,1.476E+09,0.,0.,
0.,1.27744E+05,0.,0.,0.,0.,1.27744E+05,0.,
0.,0.,0.,0.,63872.,
*SHELL GENERAL SECTION,ELSET=SHELL3O,DENSITY=115.8,ORIENTATION=ORI3, POISSON=0.,DEPENDENCIES=1
2.952E+09, 0., 2.952E+09,0.,0.,1.476E+09,0.,0.,
0.,1.27744E+05,0.,0.,0.,0.,1.27744E+05,0.,
0.,0.,0.,0.,63872.,

.5, .5,, 0.
1., 1.,, 1.
*SHELL GENERAL SECTION,ELSET=SHELL2A,COMPOSITE,CONTROLS=CONT1, POISSON=0.
0.006,3,STEEL
0.008,3,ALUMI
0.006,3,STEEL
*SHELL GENERAL SECTION,ELSET=SHELL2B,DENSITY=115.8,CONTROLS=CONT1, POISSON=0.0
2.952E+09, 0., 2.952E+09,0.,0.,1.476E+09,0.,0.,
0.,1.27744E+05,0.,0.,0.,0.,1.27744E+05,0.,
0.,0.,0.,0.,63872.,
*MATERIAL,NAME=STEEL
*ELASTIC
   200.E9,0.
*DENSITY
   7850., 
*MATERIAL,NAME=ALUMI
*ELASTIC
   69.E9,0.
*DENSITY
   2700., 
*BOUNDARY
 END,1,5
 NALL,3,5
 SYM,1,1
 SYM,6,6
*SECTION CONTROLS,HOURGLASS=RELAX STIFFNESS,NAME=CONT1
1.,1.,1.
*AMPLITUDE,NAME=FUNC
   0.,0.,.02,1.
*RESTART,WRITE,NUMBER INTERVAL=2,TIMEMARKS=NO
**
*ELSET,ELSET=QA_TEST_ALLELEMS
SHELL2, SHELL2O, SHELL3, SHELL3O
SHELL2A, SHELL2B
**
*NSET, NSET=QA_TEST_ALLNODES
NALL, NALL, SYM, END
**
*INITIAL CONDITIONS,TYPE=FIELD
NALL,1.0
*STEP
*DYNAMIC,EXPLICIT
,.012
*DLOAD,AMPLITUDE=FUNC
SHELL2,P,-1.E8
SHELL3,P,-1.E8
SHELL2O,P,-1.E8
SHELL3O,P,-1.E8
SHELL2A,P,-1.E8
SHELL2B,P,-1.E8
***OUTPUT,HISTORY,TIME INTERVAL=1.2E-5
***NODE OUTPUT,NSET=SYM
**U,
***ELEMENT OUTPUT,ELSET=ESYM
**SF,SM1
***ENERGY OUTPUT
**ALLKE,ALLIE,ALLSE,ALLAE,ALLVD,ALLCD,ALLPD,ALLFD,ALLWK,ETOTAL,DT
*FILE OUTPUT,TIMEMARKS=YES,NUMBER INTERVAL=1
*EL FILE
 ELEN,
*NODE FILE
U, 
*OUTPUT, FIELD, TIMEMARKS=YES, NUMBER INTERVAL=1
*ELEMENT OUTPUT, ELSET=QA_TEST_ALLELEMS
 ELEN,
*NODE OUTPUT, NSET=QA_TEST_ALLNODES
U, 
*OUTPUT,FIELD,VARIABLE=PRESELECT
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIMEINT=0.012
*END STEP