Aerodynamic optimization design of airfoil based on directly manipulated FFD technique

Jun Qiang Bai, Song Chen

科研成果: 书/报告/会议事项章节会议稿件同行评审

5 引用 (Scopus)

摘要

The method of applying direct manipulated FFD (DFFD) technique into aerodynamic shape optimization has been proposed and researched. Due to the disadvantage of the original FFD method within which the geometrical manipulation is not direct and intuitive, the DFFD approach has been developed by solving each displacement of the FFD control points with some specified geometry points' movements, so that the deformation of the target geometry could be directly manipulated. Besides, it has been illustrated that by DFFD method a relatively small number of design variables together with high order FFD control frame could be accomplished. The study cases has shown that applying this method in aerodynamic shape optimization of airfoil for drag reduction is of good feasibility and result, and could be coupled with effective geometrical constraints like airfoil thickness.

源语言英语
主期刊名Mechanical and Aerospace Engineering IV
121-128
页数8
DOI
出版状态已出版 - 2013
活动2013 4th International Conference on Mechanical and Aerospace Engineering, ICMAE 2013 - Moscow, 俄罗斯联邦
期限: 20 7月 201321 7月 2013

出版系列

姓名Applied Mechanics and Materials
390
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议2013 4th International Conference on Mechanical and Aerospace Engineering, ICMAE 2013
国家/地区俄罗斯联邦
Moscow
时期20/07/1321/07/13

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