Vibration Analyses of Composite Laminates

DOI

10.2991/esac-15.2015.62How to use a DOI?

Keywords

Higher order shear and normal deformable plate theory(HOSNDPT), Chebyshev-LegendreGalerkin(CLG), Composite laiminates, Vibration

Abstract

Chebyshev Legendre Galerkin(CLG) method coupled with higher-order shear and normal deformable plate theory is proposed to analyze free and forced vibrations of laminated composite plates. The laminates of various boundary conditions, side-to-thickness ratios, and material properties are considered by present method and the numerical results agree well with their corresponding analytical solutions. High accuracy, stability and efficiency is illustrated by comparing the presented method with the other methods.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Wei Wang
AU  - Shichao Yi
AU  - Sen Li
AU  - Linquan Yao
PY  - 2015/08
DA  - 2015/08
TI  - Vibration Analyses of Composite Laminates
BT  - Proceedings of the 2015 International Conference on Electronic Science and Automation Control
PB  - Atlantis Press
SP  - 250
EP  - 257
SN  - 2352-538X
UR  - https://doi.org/10.2991/esac-15.2015.62
DO  - 10.2991/esac-15.2015.62
ID  - Wang2015/08
ER  -