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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