## ΒΉ" 1 2 y \*w H \*y \*w I \*x \*w J \*x # \*w I \*y \*w J \*y dx dy (10) and indices i, j, k and l are summed over 1, 2 , n. The dynamic behaviour of the structure may be obtained by Lagrange's equations for a conservative system, which leads to ! \* \*t \*ΒΉ \*qR P # \*ΒΉ \*q P ! \*< \*q P
THE NON-LINEAR FREE VIBRATION OF FULLY CLAMPED RECTANGULAR PLATES: SECOND NON-LINEAR MODE FOR VARIOUS PLATE ASPECT RATIOS
β Scribed by M. EL KADIRI; R. BENAMAR; R.G. WHITE
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 252 KB
- Volume
- 228
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
β¦ Synopsis
The theoretical model based on Hamilton's principle and spectral analysis, previously used to obtain the "rst three non-linear modes of a clamped}clamped beam [1], and the "rst non-linear mode of a fully clamped rectangular plate [2], is used here in order to calculate the second non-linear mode of a fully clamped rectangular plate. The large vibration amplitude problem, reduced to a set of non-linear algebraic equations, is solved numerically. Results are given for the second mode of fully clamped rectangular plates, for various plate aspect ratios and vibration amplitudes. The non-linear mode shows a higher bending stress near to the clamps at large de#ections, compared with that predicted by linear theory.
π SIMILAR VOLUMES
A theoretical analysis is presented for the large amplitude vibration of symmetric and unsymmetric composite plates using the non-linear finite element modal reduction method. The problem is first reduced to a set of Duffing-type modal equations using the finite element modal reduction method. The m