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

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Other TitleEffects of the distance between a parallelly placed delta wing and a round-headed circular rod on the aerodynamic interference field
Author(jpn)西野 敦洋; 小澤 啓伺; 中村 佳朗
Author(eng)Nishino, Atsuhiro; Ozawa, Hiroshi; Nakamura, Yoshiaki
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
Author Affiliation(eng)Nagoya University Graduate School; Nagoya University Graduate School; Nagoya University School of Engineering
Issue Date2005-03
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16年度
Symposium on Flight Mechanics and Astrodynamics 2004
Start page114
End page117
Publication date2005-03
Keywordsdelta wing; aerodynamic characteristic; round-headed circular rod; aerodynamic interference; supersonic wind tunnel; hypersonic flow; flow visualization; Schlieren photography; shock wave interaction; wind tunnel test; デルタ翼; 空力特性; 半球円柱; 空力干渉; 超音速風洞; 極超音速流; 流れの可視化; シュリーレン写真法; 衝撃波干渉; 風洞試験
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

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