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首页> 外文期刊>Mechanics of Advanced Materials and Structures >Global/Local Iteration for Blended Composite Laminate Panel Structure Optimization Subproblems
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Global/Local Iteration for Blended Composite Laminate Panel Structure Optimization Subproblems

机译:混合复合层压板结构优化子问题的全局/局部迭代

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摘要

Composite panel structure optimization is commonly decomposed into panel optimization sub-problems. Previous work applied a guide based design approach to the problem for a structure where the local loads were assumed to be fixed for each panel throughout the design process. This paper examines the application of guide based design to a more realistic representation of the structure where the local loads for each panel are determined through a global level analysis that is coupled with the stacking sequence for every design panel. A small problem is selected for which an exhaustive search of the subproblem design space verifies the op-timality of the solution found through the global/local iteration process introduced in this work. The efficient discovery of solutions to these guide based design subproblems creates an opportunity to incorporate the solutions into a global level optimization process. A parallel genetic algorithm is proposed to control global optimization in which evaluating the fitness of each member of the population requires the solution of a guide based design sub-problem where parallelism is solely within fitness evaluations. Results are presented for a wingbox design problem and compared with known solutions for the same problem to demonstrate weight reductions in a problem thought to already be near optimally solved.
机译:复合面板结构优化通常分解为面板优化子问题。先前的工作针对结构问题采用了基于指南的设计方法,该结构假定在整个设计过程中每个面板的局部载荷都是固定的。本文研究了基于指南的设计在结构的更真实表示中的应用,在该结构中,通过全局级别分析与每个设计面板的堆叠顺序相结合,确定了每个面板的局部载荷。选择了一个小问题,通过对该问题的详尽搜索来验证通过此项工作中引入的全局/局部迭代过程找到的解决方案的最优性。对这些基于指南的设计子问题的解决方案的有效发现为将解决方案整合到全局级别的优化过程中提供了机会。提出了一种并行遗传算法来控制全局优化,其中评估总体每个成员的适应性要求解决基于指南的设计子问题,其中并行性仅在适应性评估之内。给出了机翼箱设计问题的结果,并将结果与​​相同问题的已知解决方案进行了比较,以证明在认为已经可以最佳解决的问题中减轻了重量。

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