Aerodynamic optimization designing of airfoil based on Isight

Wei Wang, Rong Mo, Zhiyong Chang, Huibin Sun
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引用次数: 2

Abstract

In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling software, the CFD software with Isight platform was presented, it was used to optimize the airfoil to ameliorate its aerodynamic performance. During the process of optimization designing, first, we adopted the design of experiment (DOE) method to search the designing space, achieved the optimal initialization design. Then, we adopted Non-dominated Sorting Genetic Algorithm (NSGA-II) to optimize the airfoil, got the optimal airfoil aerodynamic solution. The optimized solution proved that the aerodynamic performance of the airfoil has been significantly improved, which shows the optimization designing method was reasonable and feasible.
基于Isight的翼型气动优化设计
为了提高翼型优化设计效率,实现翼型优化设计的自动化,提出了将翼型参数化建模软件、CFD软件与Isight平台相结合的方法,对翼型进行优化设计,改善翼型气动性能。在优化设计过程中,首先采用实验设计(DOE)方法搜索设计空间,实现最优初始化设计。然后,采用非支配排序遗传算法(NSGA-II)对翼型进行优化,得到最优翼型气动解。优化结果表明,翼型气动性能得到明显改善,表明优化设计方法的合理性和可行性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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