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TSTOオービタ形状の超音速空力干渉流れ場への影響
http://hdl.handle.net/2237/13875
http://hdl.handle.net/2237/13875075774ae-b310-4cb2-899a-730651bf0e33
名前 / ファイル | ライセンス | アクション |
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2010-07-27 | |||||
タイトル | ||||||
タイトル | TSTOオービタ形状の超音速空力干渉流れ場への影響 | |||||
言語 | ja | |||||
その他のタイトル | ||||||
その他のタイトル | Effects of TSTO Orbiter Configuration on Supersonic Flow Field with Aerodynamic Interactions | |||||
言語 | en | |||||
著者 |
北村, 圭一
× 北村, 圭一× KITAMURA, Keiichi× 森, 浩一× MORI, Koichi× 花井, 勝祥× HANAI, Katsuhisa× 矢橋, 務× YABASHI, Tsutomu× 小澤, 啓伺× OZAWA, Hiroshi× 中村, 佳朗× NAKAMURA, Yoshiaki |
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アクセス権 | ||||||
アクセス権 | open access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TSTO | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Supersonic Flow | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shock/Shock Interaction | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shock/Boundary-Layer Interaction | |||||
抄録 | ||||||
内容記述 | Supersonic flow fields around Two-Stage-To-Orbit (TSTO) models with different configurations have been experimentally examined in this paper. Four configurations for the orbiter have been considered: A) a hemisphere-cylinder, B) a hemisphere-cylinder with a flat bottom, C) an obliquely truncated circular cylinder, and D) a cone-cylinder. All the flow fields around these models showed complicated shock/shock and shock/boundary-layer interactions, which can be categorized into three patterns, depending on the extent to which the separation shock wave contributes to these interactions. The models B, C and D were proposed to suppress the pressure rise due to the interactions observed in the model A. As a result, the model B showed almost the same interactions as the model A, while in the model C they did not present. In the model D, a large pressure rise was seen in the case with no clearance, whereas the model undergoes the least aerodynamic interaction at a rather large clearance. It is concluded from these results that the model C is less affected by aerodynamic interactions due to the clearance than the other models. | |||||
言語 | en | |||||
内容記述タイプ | Abstract | |||||
出版者 | ||||||
言語 | ja | |||||
出版者 | 日本航空宇宙学会 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプresource | http://purl.org/coar/resource_type/c_6501 | |||||
タイプ | journal article | |||||
出版タイプ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
ISSN | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 1344-6460 | |||||
書誌情報 |
ja : 日本航空宇宙学会論文集 巻 55, 号 646, p. 509-515, 発行日 2007-11-05 |
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フォーマット | ||||||
application/pdf | ||||||
著者版フラグ | ||||||
値 | publisher | |||||
URI | ||||||
識別子 | http://hdl.handle.net/2237/13875 | |||||
識別子タイプ | HDL |