*HEADING
: NAFEMS TEST FV16, [S8R5]; TEST 3
Shell Elements -- Cantilevered thin square plate
*NODE
 1, 0.0,0.0
 2, 2.5,0.0
 3, 5.0,0.0
 4, 7.5,0.0
 5, 10.,0.0
11, 0.0,2.5
13, 5.0,2.5
15, 10.,2.5
21, 0.0,5.0
22, 2.5,5.0
23, 5.0,5.0
24, 7.5,5.0
25, 10.,5.0
31, 0.0,7.5
33, 5.0,7.5
35, 10.,7.5
41, 0.0,10.
42, 2.5,10.
43, 5.0,10.
44, 7.5,10.
45, 10.,10.
*NSET,NSET=LEFT,GEN
1,41,10
*ELEMENT,TYPE=S8R5
1,1,3,23,21,2,13,22,11
*ELGEN,ELSET=SHELLS
1, 2,2,1, 2,20,10
*SHELL SECTION,ELSET=SHELLS,MATERIAL=MAT
0.05, 
*MATERIAL,NAME=MAT
*ELASTIC
200.E9,0.3
*DENSITY
8000., 
*BOUNDARY
LEFT,1,3
LEFT,5
*STEP
*FREQUENCY, eigensolver=lanczos, SIM=NO
9, , 
**
** NOTE : 4TH EIGENVALUE DOES NOT CORRESPOND TO A PHYSICAL MODE
**        PER 7-28-1993
**
*OUTPUT,FIELD,VAR=PRESELECT,MODE LIST
3,4,6,7,8,9
*NODE PRINT,F=0
*EL PRINT,F=0
*ENDSTEP