*Heading
Composite Cylinder
*Include, input=dsacentrifuge_node_elem.inp
*Elset, elset=_I1,  generate
*Shell Section, elset=_I1, material=Aluminum
3., 3
*Elset, elset=_I2,  generate
*Shell Section, elset=_I2, material=Aluminum
3., 3
*Elset, elset=_I3,  generate
*Shell Section, elset=_I3, Composite, Offset=0.155
    3.00, 3, Aluminum, 0.0
 <TT800>, 3,     T800, 00.0
<THM400>, 3,    HM400, <THETA1>
<THM400>, 3,    HM400, <THETA2>
 <TT800>, 3,     T800, 00.0
<THM400>, 3,    HM400, <THETA2>
<THM400>, 3,    HM400, <THETA1>
 <TT800>, 3,     T800, 00.0
    1.00, 3,     T800, 90.0
*Elset, elset=_I4,  generate
*Shell Section, elset=_I4, Composite
 <TT800>, 3,     T800, 00.0
<THM400>, 3,    HM400, <THETA1>
<THM400>, 3,    HM400, <THETA2>
 <TT800>, 3,     T800, 00.0
<THM400>, 3,    HM400, <THETA2>
<THM400>, 3,    HM400, <THETA1>
 <TT800>, 3,     T800, 00.0
*Elset, elset=_I5,  generate
*Shell Section, elset=_I5, Composite, Offset=0.092
    2.00, 3, Aluminum, 0.0
 <TT800>, 3,     T800, 00.0
<THM400>, 3,    HM400, <THETA1>
<THM400>, 3,    HM400, <THETA2>
 <TT800>, 3,     T800, 00.0
<THM400>, 3,    HM400, <THETA2>
<THM400>, 3,    HM400, <THETA1>
 <TT800>, 3,     T800, 00.0
    1.00, 3,     T800, 90.0
*Elset, elset=_I6,  generate
*Shell Section, elset=_I6, material=Aluminum
2., 3
*Elset, elset=_I7,  generate
*Shell Section, elset=_I7, material=Aluminum
2., 3
*Nset, nset=_G4
*Nset, nset=_G5
*Elset, elset=_G4
*Nset, nset=_G9,  generate
*Elset, elset=_G9,   generate
**
** MATERIALS
**
*Material, name=Aluminum
*Density
 <RHO>,
*Elastic
70000., 0.33
*Material, name=HM400
*Density
 1.63e-09,
*Elastic, type=LAMINA
233967.,14778., 0.032,10191., 5777., 5634.
*Material, name=T800
*Density
 1.63e-09,
*Elastic, type=LAMINA
177000.,14920.,  0.21, 5700., 5700., 5630.
*Parameter
THETA = 45.0
THETA1= THETA
THETA2=-THETA
RHO=2.854e-09
TT800=0.15
THM400=0.50
*Elset, elset=slice, generate
*Nset, nset=cut, generate
*Step
Frequency Analysis
*Frequency, eigensol=subspace,SIM=NO
5,
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_G4, 1, 3
_G5, 2, 3
*El Print, freq=0
*Node Print, freq=0
*Node file
U,
*Output, field, variable=preselect
*Output, history, variable=preselect
*Output, history
*Element output, elset=_G4
mass
*End Step