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

压气机/风扇二维叶型自动优化设计
引用本文:周正贵,邱名,徐夏,苗雨露.压气机/风扇二维叶型自动优化设计[J].航空学报,2011,32(11):1987-1997.
作者姓名:周正贵  邱名  徐夏  苗雨露
作者单位:南京航空航天大学能源与动力学院,江苏南京,210016
摘    要:通过压气机叶片自动优化设计关键技术研究,提出采用并行遗传算法以实现全局寻优和并行优化缩短优化耗时;采用基于修改量参数化方法,达到优化过程生成叶型的可控性和合理性;提出兼顾非设计点性能的目标函数设置方法,实现全T况优化;并进一步研制出二维平面和任意回转面叶型自动优化设计软件.软件中流场计算模块与商用软件相比一致性较好,表...

关 键 词:压气机  风扇  叶片  数值优化  遗传算法
收稿时间:2011-02-24;

Automatic Optimization Design of Compressor/Fan 2D Blade Profiles
ZHOU Zhenggui,QIU Ming,XU Xia,MIAO Yulu.Automatic Optimization Design of Compressor/Fan 2D Blade Profiles[J].Acta Aeronautica et Astronautica Sinica,2011,32(11):1987-1997.
Authors:ZHOU Zhenggui  QIU Ming  XU Xia  MIAO Yulu
Institution:ZHOU Zhenggui,QIU Ming,XU Xia,MIAO Yulu College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Abstract:In this paper,the key techniques of automatic compressor blade optimization are investigated.A parallel genetic algorithm is adopted as the numerical optimization method for its global and parallel optimization ability.The blade profile parameterization is based on geometry modification to generate controllable and reasonable blade profiles in the process of optimization.To realize the optimization in the whole work range,an objective function is set which also taken into consideration the performance at no...
Keywords:compressor  fan  blade  numerical optimization  genetic algorithm  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》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