用于层合复合材料球壳分析的各种壳体理论的统一表述

A. S. Sayyad, Y. Ghugal
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引用次数: 0

摘要

采用各种精细剪切变形理论,研究了正交各向异性层合复合材料球壳的静振动和自由振动响应。通过统一的数学公式,提出了基于位移的精细剪切变形理论,用于层合复合材料球壳的分析。与本理论有关的运动方程是在汉密尔顿原理的框架内推导出来的。在简支边界条件下,利用Navier技术得到了层合球壳静力振动和自由振动问题的解析解。很少有高阶理论和经典理论从目前的统一表述中恢复过来;然而,许多其他理论可以从目前的统一表述中恢复出来。得到了对称和反对称层合壳的数值结果。本文的结果与先前发表的结果和三维弹性解进行了比较。数值结果表明,本文的理论与其他高阶理论和三维解是一致的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A unified formulation of various shell theories for the analysis of laminated composite spherical shells
This study investigates the static and free vibration responses of orthotropic laminated composite spherical shells using various refined shear deformation theories. Displacement-based refined shear deformation theories are presented herein for the analysis of laminated composite spherical shells via unified mathematical formulations. Equations of motion associated with the present theory are derived within the framework of Hamilton's principle. Analytical solutions for the static and free vibration problems of laminated spherical shells are obtained using Navier's technique for the simply supported boundary conditions. Few higher order and classical theories are recovered from the present unified formulation; however, many other theories can be recovered from the present unified formulation. The numerical results are obtained for symmetric as well as anti-symmetric laminated shells. The present results are compared with previously published results and 3-D elasticity solution. From the numerical results, it is concluded that the present theories are in good agreement with other higher order theories and 3-D solutions.
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