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AA1530024013.pdf866.93 kB
titleHST低速性能実験機の電動ファンエンジン駆動を伴う風洞試験について: その2
Other TitleWind Tunnel Tests on a HST Low-Speed Performance Verification Model with an Electric Ducted Fan Engine, Part 2
Author(jpn)古賀, 星吾; 廣谷, 智成; 田口, 秀之; 藤川, 貴弘; 要田, 大輔; 早坂, 陽; 土屋, 武司
Author(eng)Koga, Seigo; Hirotani, Tomonari; Taguchi, Hideyuki; Fujikawa, Takahiro; Kanameda, Daisuke; Hayasaka, Akira; Tsuchiya, Takeshi
Author Affiliation(jpn)宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 東京大学; 東京大学; 東京大学; 東京大学
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); The University of Tokyo; The University of Tokyo; The University of Tokyo; The University of Tokyo
Issue Date2015-03-25
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第86-第90回風洞研究会議論文集
JAXA special publication: Proceedings of the Wind Tunnel Technology Association 86th-90th meeting
VolumeJAXA-SP-14-011
Start page68
End page71
Publication date2015-03-25
Languagejpn
eng
AbstractWind tunnel tests to obtain low-speed aerodynamic characteristics of a hypersonic passenger aircraft were conducted at the JAXA 2m×2m Low-Speed Wind Tunnel. The wind tunnel test model has an electric ducted fun (EDF) engine. This paper mainly describes improved methods for wind tunnel tests with an EDF engine and examples of the application.
Description会議情報: 第90回風洞研究会議 (2014年5月22日-23日)
形態: カラー図版あり
Meeting Information: Wind Tunnel Technology Association 90th Meeting (May 22-23, 2014)
Physical characteristics: Original contains color illustrations
KeywordsWind Tunnel Test; Hypersonic Aircraft; Low-Speed Aerodynamics
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryAerodynamics
ISSN1349-113X
NCIDAA11984031
SHI-NOAA1530024013
Report NoJAXA-SP-14-011
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/453886


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