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首页> 外文期刊>Mechanics of Advanced Materials and Structures >Buckling behavior under radial loading of orthotropic oval cylindrical shells with parabolically varying thickness
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Buckling behavior under radial loading of orthotropic oval cylindrical shells with parabolically varying thickness

机译:抛物线形变化的正交各向异性椭圆形圆柱壳在径向载荷下的屈曲行为

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摘要

In this article, the framework of the Flugge's shell theory, the transfer matrix approach, and the Romberg integration method have been employed to investigate the buckling analysis of a radial loaded oval cylindrical shell with parabolically varying thickness along its circumference. Trigonometric functions are used to form the modal displacements of the shell and Fourier's approach is used to separate the variables. The mathematical analysis is formulated to overcome the difficulties related to mode coupling of variable curvature and thickness of the shell. Using the transfer matrix of the shell, the buckling equations of the shell are reduced to eight first-order differential equations in the circumferential coordinate and rewritten in a matrix form and solved numerically. The proposed model is adopted to get the critical buckling loads and the corresponding buckling deformations for the symmetrical and antisymmetrical modes of buckling. The influences of the shell geometry, orthotropic parameters, ovality parameter, and thickness ratio on the buckling parameters and the bending deformations are presented for different type-modes of buckling.
机译:在本文中,已采用Flugge壳理论,传递矩阵方法和Romberg积分方法的框架来研究径向载荷的椭圆形圆柱壳沿其圆周呈抛物线形变化的屈曲分析。三角函数用于形成壳体的模态位移,傅立叶方法用于分隔变量。进行数学分析以克服与可变曲率和壳体厚度的模式耦合有关的困难。使用壳体的传递矩阵,将壳体的屈曲方程在圆周坐标中简化为八个一阶微分方程,并以矩阵形式重写并进行数值求解。采用所提出的模型来获得对称屈曲和反对称屈曲的临界屈曲载荷和相应的屈曲变形。给出了壳的几何形状,正交各向异性参数,椭圆度参数和厚度比对屈曲参数和弯曲变形的影响。

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