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

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Other TitleAerodynamic interference of a flow field between a delta wing and a hemispheric cylinder in a supersonic flow
Author(jpn)西野 敦洋; 石川 尊史; 中村 佳朗; 入門 朋子
Author(eng)Nishino, Atsuhiro; Ishikawa, Takafumi; Nakamura, Yoshiaki; Irikado, Tomoko
Author Affiliation(jpn)名古屋大学 大学院; 名古屋大学 大学院; 名古屋大学 工学部; 宇宙航空研究開発機構 宇宙科学研究本部
Author Affiliation(eng)Nagoya University Graduate School; Nagoya University Graduate School; Nagoya University Faculty of Engineering; Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Issue Date2004-05
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
Publication title宇宙航行の力学シンポジウム 平成15年度
Symposium on Flight Mechanics and Astrodynamics 2003
Start page35
End page38
Publication date2004-05
Keywordsdelta wing; flow field; boundary layer; hemispheric cylinder; wind tunnel model; aerodynamic interference; supersonic wind tunnel; flow visualization; デルタ翼; 流れ場; 境界層; 球頭円柱; 風洞模型; 空力干渉; 超音速風洞; 流れの可視化
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

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