Applied Mathematics and Mechanics (English Edition) ›› 2008, Vol. 29 ›› Issue (5): 603-610 .doi: https://doi.org/10.1007/s10483-008-0505-y

• Articles • 上一篇    下一篇

基于iSIGHT平台的三维机翼气动优化设计

银波, 徐典, 安亦然, 陈耀松   

  1. 1.清华大学工程力学系,北京 100084;
    2.北京大学工学院,北京 100871
  • 收稿日期:2007-09-03 修回日期:2008-03-28 出版日期:2008-05-18 发布日期:2008-05-18
  • 通讯作者: 陈耀松

Aerodynamic optimization of 3D wing based on iSIGHT

YIN Bo, XU Dian, AN Yi-ran, CHEN Yao-song   

    1. Department of Engineering Mechanics, Tsinghua University, Beijing 100084, P. R. China;
    2. College of Engineering, Peking University, Beijing 100871, P. R. China
  • Received:2007-09-03 Revised:2008-03-28 Online:2008-05-18 Published:2008-05-18
  • Contact: CHEN Yao-song

摘要: 基于iSIGHT设计平台,结合CFD软件Fluent对三维机翼进行多目标优化设计,以提高其气动性能,设计过程中采用NCGA(neighborbood cultivation)--邻域培植遗传算法,NSGA-
II(non-dominated sorting)-非支配解排序遗传算法为优化算法,以N-S方程作为主控方,对三维机翼优化,经过优化设计后结果表明,机翼的气动性能有了显著改善,该优化方法可推广用于多种翼型和机翼优化。

关键词: 气动计算, 多目标优化, 遗传算法, 三维机翼

Abstract: A method for combining the CFD software, Fluent, with the iSIGHT design platform is presented to optimize a three-dimensional wing to ameliorate its aerodynamics performance. In the optimization design, two kinds of genetic algorithms, the Neighborhood Cultivation Genetic Algorithm (NCGA) and the Non-dominated Sorting Genetic Algorithm (NSGAII), are employed and the Navier-Stoke (N-S) equations are adopted to derive the aerodynamics functions of the 3D wing. The aerodynamic performance of the optimized wing has been significantly improved, which shows that the approach can be extended and employed in other cases.

Key words: aerodynamics computation, multi-objective optimization, genetic algorithm, three-dimensional wing

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