Post-buckling analysis of functionally graded multilayer graphene platelet reinforced composite cylindrical shells under axial compression

Author:

Sun Jiabin1,Zhu Shengbo2,Tong Zhenzhen3,Zhou Zhenhuan2ORCID,Xu Xinsheng2

Affiliation:

1. State Key Laboratory of Structural Analysis of Industrial Equipment and School of Ocean Science and Technology, Dalian University of Technology, Panjin 124221, People's Republic of China

2. State Key Laboratory of Structure Analysis of Industrial Equipment and Department of Engineering Mechanics, Dalian University of Technology, International Center for Computational Mechanics, Dalian 116024, People's Republic of China

3. College of Locomotive and Rolling Stock Engineering, Dalian Jiaotong University, Dalian 116028, People's Republic of China

Abstract

Axially compressed composite cylindrical shells can attain multiple bifurcation points in their post-buckling procedure because of the natural transverse deformation restraint provided by their geometry. In this paper, the post-buckling analysis of functionally graded (FG) multilayer graphene platelets reinforced composite (GPLRC) cylindrical shells under axial compression is carried out to investigate the stability of such shells. Rather than the critical buckling limit, the focus of the present study is to obtain convergence post-buckling response curves of axially compressed FG multilayer GPLRC cylindrical shells. By introducing a unified shell theory, the nonlinear large deflection governing equations for post-buckling of FG multilayer GPLRC cylindrical shells with wide range of thickness are established, which can be easily changed into three widely used shell theories. Load-shortening curves for both symmetric and asymmetric post-buckling modes are obtained by Galerkin's method. Numerical results illustrate that the present solutions agree well with the existing theoretical and experimental data. The effects of geometries and material properties on the post-buckling behaviours of FG multilayer GPLRC cylindrical shells are investigated. The differences in the three shell theories and their scopes are discussed also.

Funder

Dalian Innovation Foundation of Science and Technology

Fundamental Research Funds for the Central Universities

Aeronautical Science Foundation of China

State Key Laboratory of Structural Analysis for Industrial Equipment

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

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