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Buckling of Anisotropic Cylindrical Shells Subjected to Combined Axial Compression, Normal Pressure, Bending and Shear Loading

机译:各向异性圆柱壳在组合轴向压力,常压,弯曲和剪切载荷作用下的屈曲

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The dissertation deals with the stability behavior of anisotropic cylindrical shells subjected to compressive stresses. It is an extension of the work done by Meyer. He investigated the stability behavior of orthotropic cylinders. First an analytical derivation of the stability matrix is performed. This stability matrix will be used to calculate the critical buckling load of a perfect cylinder. Next, computer programs are developed to calculate the critical buckling load. Finally, to explain the working of this software and to illustrate some problems and their solution, a numerical calculation is performed for an anisotropic cylinder.

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