JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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title超音速流れにおける双胴模型の空力特性に関する基礎実験
Other TitleBasic Experiment on Aerodynamic Characteristics of the Twin-Body Aircraft Model in Supersonic Flows
Author(jpn)樫谷, 賢士; 山口, 裕; 楠瀬, 一洋
Author(eng)Kashitani, Masashi; Yamaguchi, Yutaka; Kusunose, Kasuhiro
Author Affiliation(jpn)防衛大学校; 長崎総合科学大学; 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)National Defense Academy; Nagasaki Institute Applied Science; Japan Aerospace Exploration Agency (JAXA)
Issue Date2016-03
Publisher宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)
Publication title平成27年度衝撃波シンポジウム 講演論文集
Proceedings of the Symposium on Shock Waves in Japan, FY2015
Publication date2016-03
Languagejpn
Description会議情報: 平成27年度衝撃波シンポジウム (2016年3月7日-9日. 熊本大学 黒髪南地区)熊本市, 熊本県
Meeting Information: Symposium on Shock Waves in Japan, FY2015 (March 7-9, 2016. Kumamoto University), Kurokami Chuo-ku, Kumamoto, Japan
KeywordsShock Wave; Supersonic Transporter; Aerodynamics; Twin Body; Flow Visualization
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOSA6000049085
Report No3A1-1
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/562639


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