TEST CASE 2.6 EIGENFREQUENCIES OF CIRCULAR PLATE CLAMPED ALONG THE EDGE
Reference:
V.N. Chelomey, Vibration in technics, Handbook in six volumes;
V.V. Bolotin, Volume 1, The vibrations of linear systems, Moscow, Mechanical Engineering, 1978, p. 207.
Problem sketch:
Fig. 2.6
Type of created problem:
Flat plate or grillage ( Z , UX
, UY).
Input data:
;
;
Material properties:
Isotropic elastic:
;
;
Boundary conditions:
Across perimeter:
;
Problem description:
System was modeled using finite elements of thin plate (FE 12, FE 19).
Mesh: R16xL72 FE - classic analysis; R8xL36 FE - analysis using finite elements with intermediate nodes.
Modal analysis has been performed to solve the problem.
Calculation results:
Table 2.6
# of mode |
Frequency, rad/s |
Deviation, % |
|
Analytical solution |
Solution results by LIRA 10.4
|
||
1 |
633.5 |
634.6 (636.8) |
0.17(0.52) |
2, 3 |
1318.3 |
1321(1324.9) |
0.2 (0.5) |
4, 5 |
2162.7 |
2170 (2173.2) |
0.34 (0.49) |
6 |
2466.1 |
2469.9(2477.8) |
0.15 (0.47) |
7, 8 |
3164.3 |
3178.4 (3178.9) |
0.45(0.46) |
9, 10 |
3771.9 |
3780.6(3788.1) |
0.23(0.43) |
11, 12 |
4319.8 |
4324.2(4338.7) |
0.1(0.44) |
13, 14 |
5244.8 |
5275.1(5266.5) |
0.58(0.41) |
15 |
5525.2 |
5530.9(5546.5) |
0.1(0.39) |
- solution results using finite elements with intermediate nodes are specified within the brackets