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宇宙機研究のための小型自由ピストン型高エンタルピ衝撃風洞の開発
http://hdl.handle.net/10258/166
http://hdl.handle.net/10258/1666aab09de-b430-43f1-8775-fd5a7f49d3cf
名前 / ファイル | ライセンス | アクション |
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49-187.pdf (2.0 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||||||||||||
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公開日 | 2007-06-12 | |||||||||||||||||
タイトル | ||||||||||||||||||
言語 | ja | |||||||||||||||||
タイトル | 宇宙機研究のための小型自由ピストン型高エンタルピ衝撃風洞の開発 | |||||||||||||||||
タイトル | ||||||||||||||||||
言語 | en | |||||||||||||||||
タイトル | Development of Small-Scale Free Piston Type High Enthalpy Shock Tunnel for the Study of Space Plane Physics | |||||||||||||||||
言語 | ||||||||||||||||||
言語 | jpn | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | high enthalpy flow | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | hypersonic flow | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | shock tunnel | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | space plane | |||||||||||||||||
資源タイプ | ||||||||||||||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||||||||||||
資源タイプ | departmental bulletin paper | |||||||||||||||||
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 | |||||||||||||||||
著者 |
新井, 隆景
× 新井, 隆景× 杉山, 弘
WEKO
489
× 溝端, 一秀
WEKO
801
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室蘭工業大学研究者データベースへのリンク | ||||||||||||||||||
溝端 一秀(MIZOBATA Kazuhide) | ||||||||||||||||||
http://rdsoran.muroran-it.ac.jp/html/100000207_ja.html | ||||||||||||||||||
抄録 | ||||||||||||||||||
内容記述タイプ | Abstract | |||||||||||||||||
内容記述 | A Small-Scale Free Piston Type High Enthalpy Shock Tunnel has been developed at the Aeronautical and Space Engineering Division of Mechanical Systems Engineering in Muroran Institute of Technology for the study of hypersonic and high enthalpy flow being essential for space plane. By employing this shock tunnel, obtained free stream Mach number and total pressure were about 8 and 0.03MPa, respectively. The flow duration was about 1ms and estimated flow enthalpy was about 3MJ/kg. Photographs taken by CCD camera showed the developing shock wave and the shape of radiating region around the model. And also, the interaction of the hypersonic flow and sonic jet injected normally into free stream was observed. The future works such as the real gas effect problems, supersonic combustion in high enthalpy flow and so on, which are related to space plane development, will be able to be conducted using this high enthalpy facility. | |||||||||||||||||
言語 | en | |||||||||||||||||
書誌情報 |
ja : 室蘭工業大学紀要 en : Memoirs of the Muroran Institute of Technology 巻 49, p. 187-194, 発行日 1999-11-30 |
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注記 | ||||||||||||||||||
内容記述タイプ | Other | |||||||||||||||||
内容記述 | 投稿論文 | |||||||||||||||||
言語 | ja | |||||||||||||||||
出版者 | ||||||||||||||||||
言語 | ja | |||||||||||||||||
出版者 | 室蘭工業大学 | |||||||||||||||||
論文ID(NAID) | ||||||||||||||||||
関連タイプ | isIdenticalTo | |||||||||||||||||
識別子タイプ | NAID | |||||||||||||||||
関連識別子 | 110000076540 | |||||||||||||||||
日本十進分類法 | ||||||||||||||||||
主題Scheme | NDC | |||||||||||||||||
主題 | 538 | |||||||||||||||||
ISSN | ||||||||||||||||||
収録物識別子タイプ | PISSN | |||||||||||||||||
収録物識別子 | 13442708 | |||||||||||||||||
書誌レコードID | ||||||||||||||||||
収録物識別子タイプ | NCID | |||||||||||||||||
収録物識別子 | AA11175464 | |||||||||||||||||
権利 | ||||||||||||||||||
言語 | ja | |||||||||||||||||
権利情報 | © 1999 室蘭工業大学 | |||||||||||||||||
著者版フラグ | ||||||||||||||||||
出版タイプ | VoR | |||||||||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||||||||
フォーマット | ||||||||||||||||||
内容記述タイプ | Other | |||||||||||||||||
内容記述 | application/pdf |