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首页> 外文期刊>Advances in Aircraft and Spacecraft Science >Analysis of laminated and sandwich spherical shells using a new higher-order theory
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Analysis of laminated and sandwich spherical shells using a new higher-order theory

机译:使用新的高阶理论分析叠层和夹层球壳

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摘要

In the present study, a fifth-order shear and normal deformation theory using a polynomial function in the displacement field is developed and employed for the static analysis of laminated composite and sandwich simply supported spherical shells subjected to sinusoidal load. The significant feature of the present Iheory is that it considers the effect of transverse normal strain in the displacement field which is eliminated in classical, first-order and many higher-order shell theories, while predicting the bending behavior of the shell. The present theory satisfies the zero transverse shear stress conditions at the top and bottom surfaces of the shell. The governing equations and boundary conditions are derived using the principle of virtual work. To solve the governing equations, the Navier solution procedure is employed. The obtained results are compared with Reddy's and Mindlin's theory for the validation of the present theory.
机译:在本研究中,开发了在位移场中使用多项式函数的五阶剪切和法向变形理论,并将其用于层状复合材料和夹层简支球形壳体在正弦载荷下的静力分析。目前的Iheory的重要特征是,它考虑了位移场中的横向法向应变的影响,在预测壳的弯曲行为的同时,经典的,一阶的和许多高阶壳理论中消除了这种影响。本理论满足了在壳体的顶面和底面的零横向剪切应力条件。利用虚拟功原理推导了控制方程和边界条件。为了求解控制方程,采用了Navier解法。将所得结果与Reddy和Mindlin理论进行比较,以验证本理论。

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