首页 | 本学科首页   官方微博 | 高级检索  
     


Multi-objective optimization design of airfoil and wing
Authors:Zhu?Ziqiang?  author-information"  >  author-information__contact u-icon-before"  >  mailto:Zhuu@public.fhnet.cn.net"   title="  Zhuu@public.fhnet.cn.net"   itemprop="  email"   data-track="  click"   data-track-action="  Email author"   data-track-label="  "  >Email author,Fu?Hongyan,Yu?Rixin,Liu?Jie
Affiliation:Beijing University of Aeronautics and Astronautics, Beijing 100083,China
Abstract:To extend available monoobjective optimization methods to multiobjective and multidisciplinary optimization, the construction of a suitable resultant objective function(in deterministic method-DM) or a fitness function(in genetic algorithm-GA) is important. An objective function combination method (OFCM) of constructing such a function for constrained optimization problems is suggested. How to use both deterministic and genetic algorithms to biobjective and bidisciplinary optimal design of high performance airfoils and wings is discussed. Numerical results in both 2D (airfoil) and 3D (wing) cases show that the present method can be used to optimaize different kinds of initial airfoils and wings. The performance of optimized shape is improved significantly. The method is successful and effective.
Keywords:multiobjective optimization   genetic algorithm   deterministic optimization method.
本文献已被 CNKI 万方数据 SpringerLink 等数据库收录!
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