Technical Papers
Nov 11, 2016

Buckling Analysis of Composite Cylindrical Shell Panels by Using Legendre Polynomials Hierarchical Finite-Strip Method

Publication: Journal of Engineering Mechanics
Volume 143, Issue 4

Abstract

A semianalytical method hybridizing hierarchical theory and finite-strip method (FSM) is developed to analyze buckling behavior of composite laminate shells in this paper. The Legendre orthogonal polynomial series are chosen as the hierarchical shape functions for the shell strips. The critical buckling loads and modes of cylinder shells with various radiuses subjected to axial loads are calculated by the proposed hierarchical finite-strip method (HFSM). The efficiency of HFSM is noted as the method combines the advantages of both hierarchical theory and FSM. The convergence and precision of HFSM are also demonstrated by several numerical examples.

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Acknowledgments

The partial support for this study by the National Natural Science Foundation of China through grant number 11202243 is gratefully acknowledged.

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Go to Journal of Engineering Mechanics
Journal of Engineering Mechanics
Volume 143Issue 4April 2017

History

Received: Dec 24, 2015
Accepted: Aug 23, 2016
Published online: Nov 11, 2016
Published in print: Apr 1, 2017
Discussion open until: Apr 11, 2017

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Authors

Affiliations

Kan Feng
Assistant Professor, Faculty of Civil Engineering and Mechanics, Jiangsu Univ., Zhenjiang, Jiangsu 212013, China.
Jifeng Xu, M.ASCE [email protected]
Deputy Chief Engineer and Senior Technical Fellow, Beijing Key Laboratory of Civil Aircraft Structures and Composite Materials, Beijing Aeronautical Science and Technology Research Institute of COMAC, Beijing 102211, China (corresponding author). E-mail: [email protected]

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