*HEADING
: NAFEMS TEST FV16, [S8R5] TEST 2  
Shell Elements -- Cantilevered thin square plate
*RESTART,WRITE,FREQ=999
*NODE
 1, 0,0
 9,10,0
81, 0,10
89,10,10
24,3.5,2.375
26,6,2.625
37,7.375,3.75
57,7.675,6
66,6.5,7.25
64,3.75,7.25
53,2.375,6
33,2.375,3.5
44,3.25,4.375
35,4.375,3.25
57,7.625,6
55,4.625,5.625
22,1.125,2.375
42,1.25,4.875
62,1.125,7.375
73,2.375,8.625
75,5.125,8.625
77,7.625,8.625
45,4,4
46,5.75,4.375
23,2.25,2.25
25,4.75,2.5
27,7.25,2.75
47,7.5,4.75
67,7.75,7.25
65,5.25,7.25
63,2.25,7.25
43,2.5,4.75
68,8.875,7.375
48,8.75,4.875
28,8.625,2.625
17,7.375,1.375
15,4.875,1.25
13,2.375,1.125
*NGEN,NSET=SIDE
1,9
1,81,10
81,89
9,89,10
*NSET,NSET=LEFT,GEN
1,81,10
*ELEMENT,TYPE=S8R5
1, 1,3,23,21,2,13,22,11
*ELGEN,ELSET=SHELLS
1, 4,2,1, 4,20,10
*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
6, , 
*OUTPUT,FIELD,VAR=PRESELECT
*NODE PRINT,F=0
*EL PRINT,F=0
*ENDSTEP