平流层飞艇充气柔性膜结构的区间不确定优化
INTERVAL UNCERTAINTY OPTIMIZATION OF AIRSHIP’S AIR-SUPPORTED FLEXIBLE MEMBRANE STRUCTURE
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摘要: 根据随体坐标描述法,以变形后的构型作为参考基准,研究构建准确的充气膜结构应变/位移几何关系。利用虚功原理建立平衡方程,同时使用更新的拉格朗日格式(UL格式)保证膜结构分析求解的精度和稳定性。在充气柔性膜结构的分析和优化中引入不确定性参数,通过区间数学理论对其进行刻画。基于区间不确定性优化的模型和算法,对充气膜结构进行区间可靠性优化,为提高膜结构在复杂工况下的可靠性,降低失效概率提供借鉴和参考。Abstract: Following the Lagrangian Coordinate Method, the deformed configuration was used as a reference in order to build an accurate strain/displacement geometry. The balance equation was created using the principle of virtual work, and the accuracy and stability of the solution was ensured by using the Updated Lagrangian Formulation. The uncertain parameters which are introduced during the analysis and optimization of the aerated flexible membrane structure are portrayed using interval mathematical theory. The interval reliability optimization of an air-supported flexible membrane structure is developed based on the interval uncertainty optimization model. In this way the reliability of the membrane structure under complex conditions is improved and the probability of structural failure is reduced.