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Analytical and finite-element solutions for the buckling of composite sandwich conical shell with clamped ends under external pressure

机译:两端受压端部复合夹心圆锥壳屈曲的解析解和有限元解

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This paper focuses on the buckling analysis of composite sandwich conical shells subjected to a uniform external lateral pressure based on the first-order shear deformation theory. Approximate analytical solutions are assumed to satisfy fully clamped boundary conditions and then Fourier decomposition and Galerkin method is applied to achieve closed-form relations of buckling loads. The closed analytical formula for the critical pressure has been verified by comparison with the finite-element solutions and a special case where the angle of the conical shell approaches zero, that is, a cylindrical shell. Based on this formula buckling analyses of sandwich conical shells with different types of core materials have been accomplished. The outcomes are achieved considering the effects of half-vertex cone angle, core thickness and indicating applicability, accuracy, and stability of the present method.
机译:本文基于一阶剪切变形理论,对复合材料夹层圆锥壳在均匀的侧向压力作用下的屈曲进行了分析。假定近似解析解满足完全夹紧的边界条件,然后应用傅立叶分解和Galerkin方法获得屈曲载荷的闭合形式关系。通过与有限元解决方案进行比较,以及在圆锥形壳的角度接近于零(即圆柱壳)的特殊情况下,已经验证了临界压力的封闭分析公式。基于该公式,完成了不同类型芯材的夹心圆锥壳的屈曲分析。考虑到半顶点锥角,芯厚度并指示本方法的适用性,准确性和稳定性,可以达到预期的结果。

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