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An Experiential Optimization Design Method for Orthogonal Rib-Stiffened Thin Walled Cylindrical Shells under Axial Loading

机译:轴向载荷下正交肋加强薄壁圆柱形壳体的经验优化设计方法

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Parametric structural FEA (Finite Element Analysis) models of the orthogonal rib-stiffened thin walled cylindrical shells are established using APDL (ANSYS Parametric Design Language). An experiential optimization design method is then developed based on conclusions of series numerical analysis investigating the effects of parameters' modification upon buckling loads and modes of the structure. The effects of single design parameter modification under both variational and fixed volume (mass) constraints upon the buckling loads and modes indicate that, only one design scheme is able to obtain maximum buckling load when deployment of the strengthening ribs and volume (mass) parameter were settled previously, and minimum mass would be obtained while this maximum buckling load equals to the required design load. Optimization calculations for aluminum alloy material and layered C/E (Carbon/Epoxy) composite material shells with three layering styles are implemented and discussed, and some useful conclusions are obtained. Method and approach developed in this paper provide certain reference value for the optimal design of such structures.
机译:使用APDL(ANSYS参数设计语言)建立正交肋骨加强薄壁圆柱形壳体的参数结构FEA(有限元分析)模型。然后基于串联数值分析的结论来开发经验性优化设计方法,研究参数改造对屈曲负荷的影响和结构的模式。在屈曲负荷和模式下的变分和固定体积(质量)约束下单个设计参数修改的影响表明,当强化肋和体积(质量)参数的展开时,只有一个设计方案能够获得最大屈曲负载先前稳定,并且将获得最小质量,而该最大屈曲负载等于所需的设计负载。实施和讨论了具有三种分层型型铝合金材料和层状C / E(碳/环氧)复合材料壳的优化计算,并获得了一些有用的结论。本文开发的方法和方法为这种结构的最佳设计提供了一定的参考值。

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