首页> 外文会议>35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Pt.4, Apr 18-20, 1994, Hilton Head, SC >MINIMUM THICKNESS DESIGN OF COMPOSITE LAMINATES SUBJECT TO BUCKLING AND STRENGTH CONSTRAINTS BY GENETIC ALGORITHMS
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MINIMUM THICKNESS DESIGN OF COMPOSITE LAMINATES SUBJECT TO BUCKLING AND STRENGTH CONSTRAINTS BY GENETIC ALGORITHMS

机译:遗传算法对屈曲和强度约束下复合材料薄板的最小厚度设计

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In an earlier paper, the authors have shown that using a binary tree for storing past designs and employing approximation-based local improvement substantially reduces the cost of genetic algorithms for buckling load maximization of composite plates. This paper describes the application of the same techniques to the stacking sequence optimization of a laminated composite plate for thickness minimization. The thickness minimization requires use of variable length genetic strings with an objective function that includes both the thickness and constraint margins. The design variables are coded orientations in the lamination sequence. Genetic algorithms are shown to be effective for producing several alternative designs. The binary tree and local improvement techniques are shown to help in substantially reducing the number of required analyses.
机译:在较早的论文中,作者已经表明,使用二叉树来存储过去的设计并采用基于近似的局部改进,可以大大降低用于最大化复合板屈曲载荷的遗传算法的成本。本文介绍了相同技术在层压复合板厚度最小化的堆叠顺序优化中的应用。最小化厚度需要使用可变长度的遗传字符串,其目标函数应同时包括厚度和约束余量。设计变量是层压顺序中的编码方向。遗传算法被证明对于产生几种替代设计是有效的。显示了二叉树和局部改进技术可帮助实质上减少所需分析的数量。

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