Objective

Modal analysis of a thin plate.

Problem statement

To determine the natural frequencies and mode shapes of a thin plate.

Design model

A square plate with material density ρ.

Initial geometry of analytical model

Initial geometry of analytical model

Initial geometry of FE model, variant 1

Initial geometry of FE model, variant 2

Variant 1
Variant 2

Initial geometry of FE model

Reference

M.V. Barton, "Vibration of rectangular and skew cantilever plates", Journal of Applied Mechanics, vol. 18, 1951, P. 129-134.

Geometry

Side length a = 1 m
Thickness t = 0,01 m

Material properties

Modulus of elasticity Е = 2,1 * 108 tf/m2
Poisson's ratio v = 0,3
Material density ρ = 7800 kg/m3

Boundary conditions

Variant 1: All degrees of freedom are restrained along edge DC.
Variant 2: The plate is free of rigid restraints and supported by elastic supports.

Loads

Distributed mass weight for modal analysis (t*ρ*g).

Output data

1st mode shape, variant 1

2nd mode shape, variant 1

3rd mode shape, variant 1

1st mode shape
2nd mode shape
3rd mode shape

4th mode shape, variant 1

5th mode shape, variant 1

6th mode shape, variant 1

4th mode shape
5th mode shape
6th mode shape

Mode shape, variant 1

7th mode shape, variant 2

8th mode shape, variant 2

9th mode shape, variant 2

7th mode shape
8th mode shape
9th mode shape

10th mode shape, variant 2

11th mode shape, variant 2

10th mode shape
11th mode shape

Mode shape, variant 2

Comparison of calculation results

Parameters Mode shape Analytical solution LIRA-FEM Error, %
Frequency, Hz Var.1 1 8,7266 8,668 0,6715
2 21,3042 21,206 0,4609
3 53,5542 52,962 1,1058
4 68,2984 67,487 1,1880
5 77,7448 76,95 1,0223
6 136,0471 134,098 1,4327
Var.2 1 – 3 0 0,3786 -
4 – 6 0 0,3961 -
7 33,7119 33,548 0,4862
8 49,4558 48,568 1,7951
9 61,0513 60,263 1,2912
10 87,516 86,229 1,4706
11 87,516 86,229 1,4706

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