TEST CASE 2.5 EIGENFREQUENCIES OF CIRCULAR PLATE SIMPLY-SUPPORTED 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. 2.5
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 2.5
# of mode |
Frequency, rad/s |
Deviation, % |
|
Analytical solution |
Solution results by LIRA 10.4
|
||
1 |
306 |
306(318.7) |
0(4.15) |
2, 3 |
861.8 |
861.8(875) |
0(1.53) |
4, 5 |
1588.2 |
1589.4(1603.3) |
0.08(0.95) |
6 |
1842.9 |
1843.1 (1858.8) |
0.01 (0.86) |
7, 8 |
2477.7 |
2481.4 (2494.8) |
0.15 (0.69) |
9, 10 |
3006.1 |
3008.1(3024.8) |
0.07 (0.62) |
11, 12 |
3524.6 |
3531.6 (3543.8) |
0.2 (0.54) |
13, 14 |
4347.8 |
4362 (4369.5) |
0.33 (0.5) |
15 |
4598.3 |
4597(4620.2) |
0.03 (0.48) |
- solution results using finite elements with intermediate nodes are specified within the brackets