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引入最优顶点的混合方法及其在翼型优化设计中的应用

田晓虎 张彬乾 沈冬

机械科学与技术2012,Vol.31Issue(12):2010-2013,4.
机械科学与技术2012,Vol.31Issue(12):2010-2013,4.

引入最优顶点的混合方法及其在翼型优化设计中的应用

Hybrid Optimization Method Based on the Best Vertex and Its Application to Optimization Design of Airfoil

田晓虎 1张彬乾 1沈冬1

作者信息

  • 1. 西北工业大学航空学院,西安710072
  • 折叠

摘要

Abstract

In order to improve the computational efficiency of genetic algorithm (GA) and avoid getting a local optimum solution in complex method (CM), these two methods were combined together using their advantages to form a hybrid optimization method based on the best vertex (GA&CM) in this investigation. In this method, GA was used to get an approximate global optimum solution in design space. Then this solution was taken as the initial vertex of CM to search for a final solution. GA, CM and the hybrid method have been used in the aerodynamic optimization design of RAE2822 airfoil. The results show that the hybrid method is more efficient and can converge to global optimum solution better.

关键词

遗传算法/复合形法/最优顶点/混合优化方法/翼型优化

Key words

genetic algorithm/complex method/best vertex/hybrid optimization method/airfoil optimization

分类

航空航天

引用本文复制引用

田晓虎,张彬乾,沈冬..引入最优顶点的混合方法及其在翼型优化设计中的应用[J].机械科学与技术,2012,31(12):2010-2013,4.

机械科学与技术

OA北大核心CSCDCSTPCD

1003-8728

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