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極超音速飛行するスペースプレーン周りの流れ場の3次元的研究
https://jaxa.repo.nii.ac.jp/records/14704
https://jaxa.repo.nii.ac.jp/records/14704e5cc94c4-dbca-48fb-85c7-de71760e8ab9
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 極超音速飛行するスペースプレーン周りの流れ場の3次元的研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ場 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スペースプレーン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 放電モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SSTO機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 層流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 仰角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 壁表面 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの可視化 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow field | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electric discharge model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SSTO vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminar flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wall surface | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow visualization | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Investigation of flowfield around hypersonic space plane | |||||
著者 |
中村, 弘明
× 中村, 弘明× 真鍋, 圭司× 瀬崎, 新士× 西尾, 正富× Nakamura, Hiroaki× Manabe, Keiji× Sezaki, Shinji× Nishio, Masatomi |
|||||
著者所属 | ||||||
福山大学 大学院 | ||||||
著者所属 | ||||||
福山大学 工学部 | ||||||
著者所属 | ||||||
福山大学 大学院 | ||||||
著者所属 | ||||||
福山大学 工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Faculty of Engineering | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
宇宙航行の力学シンポジウム 平成14年度 en : Symposium on Flight Mechanics and Astrodynamics 2002 p. 63-66, 発行日 2003-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The flowfield analysis around a model of space plane traveling at Mach 10 has been carried out utilizing the Electric Discharge Method and the Finite Element Method (FEM) scheme. The Electric Discharge Method can visualize almost all important hypersonic flowfield phenomena, such as three-dimensional shock shapes, streamlines near wall surface, distant streamlines from wall surface, boundary layers, etc. In this study, the experiments and the numerical simulations were carried out under the conditions the angles of attack were 0 and 10 deg. Furthermore, the experimental results were compared with the numerical ones. In these comparisons, it was found that they were relatively in good agreement. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045913017 |