*HEADING
 ROTATING CYLINDER PROBLEM
**
**  Membrane mesh.
**
*NODE, NSET=QA_TEST_ALLNODES
*NGEN,LINE=C,NSET=M3D
*ELEMENT,TYPE=M3D4R,ELSET=M3D
*ELGEN,ELSET=M3D
*NODAL THICKNESS
M3D,0.1
*MEMBRANE SECTION,ELSET=M3D,MATERIAL=MAT,ORIENTATION=M3D,POISSON=MATERIAL,
NODAL THICKNESS
10.,
*EQUATION
*INITIAL CONDITIONS,TYPE=ROTATING VEL
M3D,4000., 0.,0.,0.
2.,0.,0., 2.,0.,1.
*ORIENTATION,NAME=M3D,SYSTEM=CYLINDRICAL
*BOUNDARY
M3D,3,3
**
**  3D brick mesh.
**
*NODE, NSET=QA_TEST_ALLNODES
*NGEN,LINE=C,NSET=C3D
*ELEMENT,TYPE=C3D8R,ELSET=C3D
*ELGEN,ELSET=C3D
*SOLID SECTION,ELSET=C3D,MATERIAL=MAT
*EQUATION
*MPC
SLIDER, 2001,2101,2099
SLIDER, 2010,2110,2099
SLIDER, 2201,2301,2299
SLIDER, 2210,2310,2299
*BOUNDARY
C3D,3,3
2099,1,3
2299,1,3
*INITIAL CONDITIONS,TYPE=ROTATING VEL
C3D,4000., 0.,0.,0.
0.,1.5,0., 0.,1.5,1.
**
**  Shell mesh.
**
*NODE, NSET=QA_TEST_ALLNODES
*NGEN,LINE=C,NSET=S3D
*ELEMENT,TYPE=S4R,ELSET=S3D
*ELGEN,ELSET=S3D
*NODAL THICKNESS
S3D, 0.1
*SHELL SECTION, SECTION INT=GAUSS,ELSET=S3D,MATERIAL=MAT,
NODAL THICKNESS
1.,
*EQUATION
*INITIAL CONDITIONS,TYPE=ROTATING VEL
S3D,4000., 0.,0.,0.
2.,1.5,0., 2.,1.5,1.
*BOUNDARY
S3D,3,3
**
*MATERIAL,NAME=MAT
*ELASTIC
1.03E7,.33333
*PLASTIC
4.15E4,0.
521.15E4,10.
*DENSITY
2.508E-4,
**
**
*ELSET,ELSET=QA_TEST_ALLELEMS
M3D, C3D, S3D
**
*NSET, NSET=QA_TEST_ALLNODES
QA_TEST_ALLNODES, M3D, C3D, S3D
**
*STEP
*DYNAMIC,EXPLICIT
,.15E-3
*DLOAD
 C3D,P6,9760.
 M3D,P,-9760.
 S3D,P,-9760.
**
*FILE OUTPUT,NUMBER INTERVAL=2,TIME MARKS=YES
*EL FILE
 PEEQ,
 MISES,
 PE,
 SDV
*NODE FILE
 U,
**
*OUTPUT, FIELD, NUMBER INTERVAL=2, TIMEMARKS=YES
*ELEMENT OUTPUT, ELSET=QA_TEST_ALLELEMS
 PEEQ,
 MISES,
 PE,
 SDV
*NODE OUTPUT, NSET=QA_TEST_ALLNODES
 U,
*OUTPUT,FIELD,VARIABLE=PRESELECT
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIMEINT=7.5E-05
***OUTPUT,HISTORY,VARIABLE=PRESELECT
*END STEP