TEST CASE 2.4 EIGENFREQUENCIES OF RECTANGULAR PLATE CLAMPED ON ALL EDGES
Reference:
I.A. Birger, Y.G. Panovko, Strength, stability, vibrations, Handbook in three volumes, Volume 3, Moscow, Mechanical Engineering, 1968, p. 377.
Problem sketch:
Fig. 2.4
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 19).
Mesh: 20x20 FE - classic analysis; 10x10 FE - analysis using finite elements with intermediate nodes.
Modal analysis has been performed to solve the problem.
Calculation results has been compared to analytical solution using Rayleigh-Ritz method.
Calculation results:
Table 2.
4
# of mode |
Frequency, rad/s |
Deviation, % |
|
Analytical solution |
Solution results by LIRA 10.4 |
||
1 |
560.1 |
556.38 (557.80) |
0.66 (0.41) |
2 |
1143.2 |
1133.68 (1137.57) |
0.83 (0.49) |
3 |
1143.2 |
1133.68 (1137.57) |
0.83 (0.49) |
4 |
1686.6 |
1663.98 (1677.33) |
1.34 (0.55) |
5 |
2054.0 |
2031.91 (2039.12) |
1.07 (0.72) |
6 |
2054.0 |
2042.13 (2048.76) |
0.58 (0.26) |
- solution results using finite elements with intermediate nodes are specified within the brackets.