An analytical approach for postbuckling of eccentrically or concentrically stiffened composite double curved panel on nonlinear elastic foundation

被引:9
作者
Bohlooly, Mehdi [1 ]
Mirzavand, Babak [2 ]
Fard, Keramat Malekzadeh [3 ]
机构
[1] Aircraft Res Ctr, Tehran, Iran
[2] Univ Tehran, Fac New Sci & Technol, Tehran, Iran
[3] Malek Ashtar Univ Technol, Dept Mech Engn, Tehran, Iran
关键词
Cylindrical; Doubly curved; 3rd parameter; Stiffener; PLATES; SHELLS;
D O I
10.1016/j.apm.2018.06.008
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper presents a detailed analytical investigation on the buckling and postbuckling behavior of laminated composite double curved panels with eccentrically and/or concentrically ortho-grid stiffeners subjected to in-plane compression, lateral pressure, thermal environment, and combined loads. The panels are surrounded by three parameter elastic foundations. Different types of simple-supported boundary conditions are considered. The equilibrium and compatibility equations of panel are derived based on Kirchhoff assumptions incorporating nonlinear von-Karman relations. The stress function and Galerkin method are applied to obtain explicit expressions of the buckling load and load-deflection relations. New results are presented to show effects of the combined loads, position of stiffener, and elastic foundation. As a key finding of these results, the buckling load and the postbuckling curves of concentrically stiffened panels are higher than eccentrically stiffened panels. (C) 2018 Elsevier Inc. All rights reserved.
引用
收藏
页码:415 / 435
页数:21
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