首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于混合遗传算法的压气机叶型自动优化设计
引用本文:金东海,展昭,桂幸民.基于混合遗传算法的压气机叶型自动优化设计[J].推进技术,2006,27(4):349-353.
作者姓名:金东海  展昭  桂幸民
作者单位:北京航空航天大学,能源与动力工程学院,北京,100083
摘    要:1引言遗传算法(Genetic A lgorithms,简称GA)是模拟生物在自然环境中的遗传选择和自然淘汰的进化过程而形成的一种全局优化概率搜索算法。遗传算法实施群体搜索,概率转移,不需要目标函数的导数信息,其全局搜索能力强,简单通用,适于并行处理,因而广泛应用于各种复杂系统的优化问

关 键 词:压气机  混合遗传算法~    复合形法~    叶型  优化设计
文章编号:1001-4055(2006)04-0349-05
收稿时间:2005-08-20
修稿时间:2005-11-15

Automatic design optimization of compressor blades based on hybrid genetic algorithm
JIN Dong-hai,ZHAN Zhao and GUI Xing-min.Automatic design optimization of compressor blades based on hybrid genetic algorithm[J].Journal of Propulsion Technology,2006,27(4):349-353.
Authors:JIN Dong-hai  ZHAN Zhao and GUI Xing-min
Institution:School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100053, China
Abstract:One of the hybrid genetic algorithms applied in automatic design optimization has been estab-lished by combining a real-number encoded self-adaptive genetic algorithm with complex method.The introduction of complex method has notably improved the capability of local search.Compare with self-adaptive genetic algorithm,the hybrid genetic algorithm(HGA) has much higher efficiency.Having few control points,but allowing flexible manipulation,the Bezier representation was chosen to describe the compressor blade elements.The numerical simulation was carried out by a CFD code based on solution of two dimensional N-S equations.The optimization result for certain NACA airfoil demonstrates that the developed platform based on HGA is effective and efficient.
Keywords:Compressor  Hybrid genetic algorithm~+  Complex method  Blade  Optimum design
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号