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Static and free vibration analysis of laminated composite and sandwich spherical shells using a generalized higher-order shell theory

机译:基于广义高阶壳理论的层合复合材料和夹层球形壳静静振动分析

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摘要

In this article, higher-order closed-form solutions are obtained for static bending and free vibration analysis of laminated composite and sandwich spherical shells using a generalized higher-order shell theory. A theory is independent of the choice of shearing stress function (polynomialon-polynomial) which eventually results in a theoretical unification of most of the classical and higher-order shear deformation theories. The present theory yields an accurate distribution of transverse shear stresses through the shell thickness; therefore, it does not require problem dependent shear correction factor. Governing equations and associated boundary conditions of the theory are derived by employing Hamilton's principle. Navier type higher-order closed-form solutions are obtained for simply supported boundary conditions. Displacements, stresses and natural frequencies are presented for laminated composite and sandwich plates as well as shallow and deep spherical shells. The results of parabolic, trigonometric, hyperbolic, and exponential models are compared with each other and previously published results to verify the accuracy and efficiency of the present generalized shell theory.
机译:本文采用广义的高阶壳理论,为层合复合材料和夹层球形壳的静态弯曲和自由振动分析提供了高阶封闭形式解。理论独立于剪切应力函数(多项式/非多项式)的选择,最终导致大多数经典和高阶剪切变形理论的理论统一。本理论产生了贯穿壳厚度的横向剪应力的精确分布;因此,它不需要依赖于问题的剪切校正因子。运用汉密尔顿原理推导了该理论的控制方程和相关的边界条件。对于简单支持的边界条件,获得了Navier型高阶封闭形式解。给出了层压复合材料和夹心板以及浅,深球形壳的位移,应力和固有频率。将抛物线模型,三角函数,双曲线模型和指数模型的结果相互比较,并与先前发表的结果进行比较,以验证当前广义壳理论的准确性和效率。

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