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Vibrations and buckling of cylindrical shell made of a general anisotropic elastic material

机译:由一般各向异性弹性材料制成的圆柱形壳的振动和屈曲

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Free vibrations and buckling under uniform external pressure of thin elastic circular cylindrical shells are studied in assumption that the shell material is generally anisotropic and described by 21 elastic moduli. Non-classical equations based on the generalized Timoshenko-Reissner hypotheses are applied for the analysis of shell vibrations and buckling. The natural frequencies, the critical external pressure and the vibration and buckling modes are obtained by means of asymptotic method. As an example of the general anisotropy, a composite structure consisting of a matrix reinforced by the system of fibers inclined to the midsurface is considered. The asymptotic and numerical results of the vibration problem converge.
机译:根据薄弹性圆柱形壳的均匀外部压力下的自由振动和弯曲是假设壳材料通常是各向异性的并且由21个弹性模量描述。基于广义TimosheOnko-Reissner假设的非古典方程用于分析壳振动和屈曲。通过渐近法得到自然频率,临界外部压力和振动和屈曲模式。作为一般各向异性的示例,考虑了由倾向于沿脑表面的纤维系统增强的基质组成的复合结构。振动问题的渐近和数值结果会聚。

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