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小型高エンタルピー衝撃風洞を用いたスクラムジェットエンジンモデル内の超音速燃焼
http://hdl.handle.net/10258/116
http://hdl.handle.net/10258/116810aeac7-f63b-4d0f-ae02-ceaac8a6e203
名前 / ファイル | ライセンス | アクション |
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51-77.pdf (3.6 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2007-06-06 | |||||
タイトル | ||||||
言語 | ja | |||||
タイトル | 小型高エンタルピー衝撃風洞を用いたスクラムジェットエンジンモデル内の超音速燃焼 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Study on Flows and Combustion Phenomena in Scramjet Engine Used bu A Small Scale High Enthalpy Shock Tunnel | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | scramjet engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock systems | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high enthalpy shock tunnel | |||||
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× 笠原, 次郎× 小久保, 崇× 向井, 幸司 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | To investigate the fiow and combustian in a Scrarmjet engine model at about Mach 7 condition a small high enthalpy shock tunnel was used. A couple of wedge was set in the test section as a Scramjet engine intake and combustion chamber model. The compression process used the oblique shock systems, which was generated by vehicle edge (fore-body) and cowl, was observed. H2 and/or C2H2-air mixture gas was injected normally to supersonic cross flow in thc combustion chamber. A self-emission from combustion gas was observed by using a very high-speed video camera (18,000fps) with image intcnsifier. The wal1 static pressure in the combustion chamber was also measured. It was clarified that the wall pressure increased when the supersonic combustion occurred. | |||||
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 51, p. 77-84, 発行日 2001-11-30 |
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注記 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 小特集 : 「室蘭工大における航空宇宙工学研究の新展開」 | |||||
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 | 110000076573 | |||||
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 | |||||
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 |