Inverse design method of airfoil embedded optimization of pressure distribution

Jiao Zan Li, Zheng Hong Gao

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

Genetic algorithm has been applied to optimize the target pressure distribution for inverse design method. Pressure distribution around airfoil is parameterized and the drag is minimized under constraints on lift, airfoil thickness, etc. Once target pressures are obtained, corresponding airfoil geometries can be computed by an inverse design code coupled with a NS solver. The presented result of designed airfoil for transonic case shows that the method developed is feasible.

源语言英语
主期刊名ICIC 2010 - 3rd International Conference on Information and Computing
101-104
页数4
DOI
出版状态已出版 - 2010
活动3rd International Conference on Information and Computing, ICIC 2010 - Wuxi, Jiang Su, 中国
期限: 4 6月 20106 6月 2010

出版系列

姓名ICIC 2010 - 3rd International Conference on Information and Computing
1

会议

会议3rd International Conference on Information and Computing, ICIC 2010
国家/地区中国
Wuxi, Jiang Su
时期4/06/106/06/10

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