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AIRFOIL AND WING DESIGN THROUGH HYBRID OPTIMIZATION STRATEGIES

机译:通过混合优化策略进行机翼和机翼设计

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摘要

Real-world design problems need robust and effective system-level optimization tools inasmuch as they are ruled by several criteria. most often in multidisciplinary environments. In this work a hybrid optimization algorithm has been obtained by adding a gradient-based technique to the set of operators of a multiobjective genetic algorithm. This makes it possible to increase the computational efficiency of the genetic algorithm while preserving its favorable features of robustness, problem independence, and multionbjective optimization capabilities. Aerodynamic shape design problems, including both airfoil and wing designs, are considered.
机译:现实世界中的设计问题需要鲁棒且有效的系统级优化工具,因为它们受多个标准约束。最常见于多学科环境。在这项工作中,通过将基于梯度的技术添加到多目标遗传算法的算子集中,获得了一种混合优化算法。这使得可以提高遗传算法的计算效率,同时保留其健壮性,问题独立性和多对象优化能力的有利特征。考虑了空气动力学形状设计问题,包括机翼和机翼设计。

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