*HEADING
  NONLINEAR POSTBUCKLING ANALYSIS--10% IMPERFECTION
  WITH CONTRIBUTIONS FROM FIRST FOUR MODES
  COMPOSITE CYLINDRICAL PANEL WITH CIRCULAR HOLE
**
**  FROM STUDY IN THESIS OF G.M. STANLEY
**
*NODE,INPUT=laminpanel_s9r5_stri65_node.inp
*NSET,NSET=OUTSIDE,GENERATE
*NSET,NSET=HOLE,GENERATE
*NSET,NSET=XPARB,GENERATE
*NSET,NSET=XPART,GENERATE
*NSET,NSET=YPAR,GENERATE
*NSET,NSET=PROFILE,GENERATE
*EQUATION
*NSET,NSET=MASTER
*ELEMENT,TYPE=STRI65
*ELGEN,ELSET=ALL
*ELEMENT,TYPE=STRI65
*ELGEN,ELSET=ALL
*ELSET,ELSET=PROFILE,GENERATE
*SHELL GENERAL SECTION,ELSET=ALL
7.90239D5,2.51367D5,7.90239D5,-3.08578D-6,-7.94285D-5,2.69436D5,0.,0.
0., 4.92719D+02,0.,0.,0.,1.91513D+02,5.17951D+02,0.
0.,0.,  1.89245D+01 , 1.89245D+01 ,2.03602D+02
*BOUNDARY
XPARB,1,6
XPART,1,2
XPART,4,6
YPAR,1,2
*RESTART,WRITE,FREQUENCY=5
*STEP,NLGEOM,INC=15,EXTRAPOLATION=NO
*STATIC,RIKS
1.,1.,,,,2041,3,-0.08
*CLOAD
2041,3,-10000.
*MONITOR,NODE=2041,DOF=3
*EL PRINT,ELSET=PROFILE,POSITION=AVERAGED AT NODES,FREQUENCY=5
SF,
*NODE PRINT,NSET=XPART,TOTALS=YES,FREQUENCY=5
U,
RF,
*NODE PRINT,NSET=XPARB,TOTALS=YES,FREQUENCY=5
U,
RF,
*NODE FILE,FREQUENCY=1,NSET=MASTER
U,CF
*END STEP