*HEADING
 SHALLOW CYLINDRICAL SHELL VIA S4R5 / USE STABILIZE          
USING GAUSS INTEGRATION WITH 5 SECTION POINTS
*RESTART, WRITE
*NODE
1,2.54,0.,0.,1.
7,2.5273106,.2535769,0.,.9950042,.0998334
61,2.54,0.,.254,1.
67,2.5273106,.2535769,.254,.9950042,.0998334
*NGEN,LINE=C ,NSET=EDGE
1,7,1,0,0.,0.,0.
*NGEN,LINE=C,NSET=ZSYMM
61,67,1,0,0.,0.,.254
*NFILL
EDGE,ZSYMM,6,10
*NGEN,NSET=YSYMM
1,61,10
*NGEN,NSET=HINGE
7,67,10
*NSET,NSET=N61
61, 
*ELEMENT,TYPE=S4R5
1,1,2,12,11
*ELGEN,ELSET=EALL
1,6,1,1,6,10,10
*MATERIAL,NAME=ROOF
*ELASTIC
3.103E9,.3
*SHELL SECTION ,MATERIAL=ROOF,ELSET=EALL, SECTION INTEGRATION=GAUSS
6.35E-3,5
*BOUNDARY
ZSYMM,ZSYMM
YSYMM,YSYMM
HINGE,1,5
*STEP,NLGEOM,INC=50
*STATIC,STABILIZE,FACTOR=1.25535E+05
0.1,1.,0.,0.1,
*CLOAD
61,1,-333. 
*MONITOR,NODE=61,DOF=1
*NODE PRINT,FREQUENCY=2
U, 
RF, 
VF
*NODE FILE,NSET=N61
U,CF,VF
*EL PRINT,FREQUENCY=2
SF,
SSAVG,
*EL FILE,FREQ=9999
ELEN,
*ENERGY FILE 
*OUTPUT,FIELD,FREQ=9999
*ELEMENT OUTPUT
ELEN,
ELEDEN,
*NODE OUTPUT
U,VF,
*OUTPUT,HISTORY
*ENERGY OUTPUT
*END STEP