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Finite Element Analysis for Solid Rocket Motor Cases

机译:固体火箭发动机箱体有限元分析

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A finite element development for shells of revolution and cylinders in plane strain is presented. The element is based upon a variational theorem which allows linear displacement expansions in each element, thus, an element is developed which is fully compatible with commonly employed continuum elements. A numerical example is presented along with a computer program listing for shells of revolution. (Author)

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