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http://dx.doi.org/10.12989/scs.2018.27.5.555

Buckling and post-buckling behaviors of 1/3 composite cylindrical shell with an opening  

Ma, Yihao (School of Aeronautic Science and Engineering, Beihang University)
Cheng, Xiaoquan (School of Aeronautic Science and Engineering, Beihang University)
Wang, Zhaodi (Institute 306 of the 3rd Academy of CASIC)
Guo, Xin (School of Aeronautic Science and Engineering, Beihang University)
Zhang, Jie (School of Aeronautic Science and Engineering, Beihang University)
Xu, Yahong (Institute 306 of the 3rd Academy of CASIC)
Publication Information
Steel and Composite Structures / v.27, no.5, 2018 , pp. 555-566 More about this Journal
Abstract
A 1/3 composite cylindrical shell with a central rectangular opening was axially compressed experimentally, and its critical buckling load and displacement, and strains were measured. A finite element model (FEM) of the shell with Hashin failure criteria was established to analyze its buckling and post-buckling behaviors by nonlinear Newton-Raphson method. The geometric imperfection sensitivity and the effect of side supported conditions of the shell were investigated. It was found that the Newton-Raphson method can be used to analyze the buckling and post-buckling behaviors of the shell. The shell is not sensitive to initial geometric imperfection. And the support design of the shell by side stiffeners is a good way to obtain the critical buckling load and simplify the experimental fixture.
Keywords
composite shell; opening; post-buckling; Newton-Raphson method; FEM; axial compression;
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Times Cited By KSCI : 6  (Citation Analysis)
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