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

There are no files associated with this item.

Other TitleStabilization time of the flow field around spacecraft in an experiment using a shock tunnel
Author(jpn)西尾 正富; 真鍋 圭司; 瀬崎 新士; 中村 弘明
Author(eng)Nishio, Masatomi; Manabe, Keiji; Sezaki, Shinji; Nakamura, Hiroaki
Author Affiliation(jpn)福山大学 工学部; 福山大学 工学部; 福山大学 大学院; 福山大学 大学院
Author Affiliation(eng)Fukuyama University Faculty of Engineering; Fukuyama University Faculty of Engineering; Fukuyama University Graduate School; Fukuyama University Graduate School
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 page29
End page30
Publication date2004-05
Keywordsstabilization; shock tunnel; wind tunnel model; hypersonic gun tunnel; space capsule; schlieren photography; flow field; dimensional analysis; 安定化; 衝撃風洞; 風洞模型; 極超音速ガンタンネル; 宇宙カプセル; シュリーレン写真法; 流れ場; 次元解析
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.