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titleA study on improvement of aerodynamic characteristic of next generation SST by active flow control
Other TitleA study on improvement of aerodynamic characteristic of next generation SST by active flow control
Author(jpn)麻生 茂; 辛島 桂一
Author(eng)Aso, Shigeru; Karashima, Keiichi
Author Affiliation(jpn)九州大学 工学部 航空工学科; 西日本工業大学
Author Affiliation(eng)Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering; Nishinippon Institute of Technology
Issue Date2007-03-30
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication titleProceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)
Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)
Start page417
End page418
Publication date2007-03-30
Languageeng
DescriptionJAXA Special Publication
宇宙航空研究開発機構特別資料
Keywordssupersonic aircraft; aircraft design; aerodynamic characteristic; computational fluid dynamics; lift drag ratio; arrow wing; aspect ratio; wind tunnel test; transonic wind tunnel; active flow control; 超音速機; 航空機設計; 空力特性; 計算流体力学; 揚抗比; アロー翼; アスペクト比; 風洞試験; 遷音速風洞; 能動的流動制御
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
SHI-NOAA0063609051
Report NoJAXA-SP-06-029E
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/28632


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