Vibration Analysis of Anisotropic Simply Supported Plates by Using Variable Kinematic and Rayleigh-Ritz Method

Author:

Carrera Erasmo1,Fazzolari Fiorenzo Adolfo2,Demasi Luciano3

Affiliation:

1. Aeronautics and Space Engineering Department, Politecnico di Torino, Torino, Italy

2. School of Engineering and Mathematical Sciences, City University London, Northampton Square, London EC1V 0HB United Kingdom

3. Department of Aerospace Engineering and Engineering Mechanics, San Diego State University, San Diego, CA 92182-1308

Abstract

This work deals with accurate free-vibration analysis of anisotropic, simply supported plates of square planform. Refined plate theories, which include layer-wise, equivalent single layer and zig-zag models, with increasing number of displacement variables are take into account. Linear up to fourth N-order expansion, in the thickness layer-plate direction have been implemented for the introduced displacement field. Rayleigh-Ritz method based on principle of virtual displacement is derived in the framework of Carrera’s unified formulation. Regular symmetric angle-ply and cross-ply laminates are addressed. Convergence studies are made in order to demonstrate that accurate results are obtained by using a set of trigonometric functions. The effects of the various parameters (material, number of layers, and fiber orientation) upon the frequencies and mode shapes are discussed. Numerical results are compared with available results in literature.

Publisher

ASME International

Subject

General Engineering

Reference54 articles.

1. “Vibration of Plates,”;Leissa

2. Germain, S. , 1821, Researches Sur la Theorie des Surfaces Elastiques, Paris.

3. Lagrange, J. L. , 1828, Note Communiquee Aux Commissaires Pour Le Prix de la Surface Elastique (Dec. 1811), ct. Annales de Chimie, Vol. 39, pp. 149 and 207.

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