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首页> 外文期刊>Aerospace science and technology >Nonlinear buckling and post-buckling behavior of shear deformable sandwich toroidal shell segments with functionally graded core subjected to axial compression and thermal loads
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Nonlinear buckling and post-buckling behavior of shear deformable sandwich toroidal shell segments with functionally graded core subjected to axial compression and thermal loads

机译:具有轴向压缩和热负荷的功能渐变芯的剪切可变形夹层环形壳体段的非线性屈曲和屈曲行为

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This paper presents an analytical investigation on buckling and post-buckling of shear deformable sandwich toroidal shell segments with functionally graded core and homogeneous face sheets. The effective material properties of core layer are graded in the thickness direction according to a simple power law distribution in terms of volume fraction index. The shells are surrounded by an elastic foundation and subjected to axial compressive or thermal loads. Reddy's third-order shear deformation shell theory (TSDT) is used to established formulations. A new solution using Galerkin method for solving a governing system of four-partial differential equations is carried out to obtain closed-form expressions of buckling stresses and post-buckling curves. Two cases of bowed-out and bowed-in sandwich toroidal shells are considered. Effects of material, geometric parameters and elastic foundation on stability behavior of the shells is analyzed in detail. The difference between bucking stresses basing on TSDT and those basing on classical shell theory (CST) is also clearly shown in this study. (C) 2020 Elsevier Masson SAS. All rights reserved.
机译:本文介绍了用功能梯度芯和均匀面板屈曲和剪切可变形夹层环形壳体段屈曲和后屈曲的分析研究。根据体积分数指数的简单电力法分布,芯层的有效材料特性在厚度方向上分析。壳体包围有弹性基础,经受轴向压缩或热负荷。 Reddy的三阶剪切变形壳理论(TSDT)用于建立配方。采用Galerkin方法来解决用于求解四部分微分方程的控制系统的新解决方案,以获得屈曲应力和后屈曲曲线的闭合表达。考虑了两种萌芽和弯曲的夹层环形壳。详细分析了材料,几何参数和弹性地基对壳体稳定性行为的影响。本研究还清楚地显示了对TSDT基于TSDT的支配应力与古典壳理论(CST)的差异。 (c)2020 Elsevier Masson SAS。版权所有。

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