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デトネーション波により駆動される衝撃波管の作動特性に関する実験的研究
https://sucra.repo.nii.ac.jp/records/13388
https://sucra.repo.nii.ac.jp/records/13388d5cb0ea4-eaf4-4e06-af7a-eed7b3946d7d
名前 / ファイル | ライセンス | アクション |
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A3000039.pdf (794.8 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2009-04-20 | |||||
タイトル | ||||||
タイトル | デトネーション波により駆動される衝撃波管の作動特性に関する実験的研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Detonation | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shock Wave | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Compressible Flow | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 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 | journal article | |||||
タイトル(別言語) | ||||||
その他のタイトル | Experimental Study on Performance of Shock Tube Driven by Detonation Wave | |||||
著者 |
金, 泰煥
× 金, 泰煥× 小原, 哲郎× 大八木, 重治× 吉川, 正人 |
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著者 ローマ字 | ||||||
KIM, Tae Hwan | ||||||
著者 ローマ字 | ||||||
OBARA, Tetsuro | ||||||
著者 ローマ字 | ||||||
OHYAGI, Shigeharu | ||||||
著者 ローマ字 | ||||||
YOSHIKAWA, Masato | ||||||
著者 所属 | ||||||
埼玉大学大学院理工学研究科 | ||||||
著者 所属 | ||||||
埼玉大学理工学研究科人間支援・生産科学部門 | ||||||
著者 所属 | ||||||
埼玉大学理工学研究科人間支援・生産科学部門 | ||||||
著者 所属(別言語) | ||||||
Graduate School of Science and Engineering, Saitama University | ||||||
著者 所属(別言語) | ||||||
Graduate School of Science and Engineering, Saitama University | ||||||
著者 所属(別言語) | ||||||
Graduate School of Science and Engineering, Saitama University | ||||||
書誌情報 |
日本機械学會論文集. B編 en : Transactions of the Japan Society of Mechanical Engineers. B 巻 70, 号 691, p. 707-714, 発行日 2004 |
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年月次 | ||||||
2004-3 | ||||||
出版者名 | ||||||
出版者 | 社団法人日本機械学会 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 3875016 | |||||
関連サイト | ||||||
内容記述タイプ | Other | |||||
内容記述 | http://ci.nii.ac.jp/naid/110004999317/ | http://ci.nii.ac.jp/naid/110004999317/ | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | A detonation-driven shock tube is useful apparatus for producing high-enthalpy flow and it can be used to investigate a combustion flow inside Scramjet-engine. This detonation-driven shock tube produces a shock wave of high propagation Mach number using a particularly high-temperature gas behind detonation wave. However, state variables such as pressure and temperature behind detonation wave are not uniform, since a Taylor expansion wave follows precursor detonation wave so as to decrease these variables. Therefore, a performance of this device is necessary to be studied and this report is concerned with characteristics of this facility in order to produce a high-enthalpy flow. Experiments were conducted by applying a combination of sub-combustion tube and spiral-coil to produce a detonation wave. As a result, it was clarified that detonation wave was produced with extremely short distance from an igniter. The propagation Mach number of a shock wave was increased by diluting driver-gas with light-gas. A stagnation enthalpy behind reflected shock wave was evaluated and experimental conditions producing high-enthalpy flow were clarified, which would be practical to investigate a combustion flow inside a Scramjet-engine. | |||||
注記 | ||||||
内容記述タイプ | Other | |||||
内容記述 | rights: 社団法人日本機械学会 rights: 本文データは学協会の許諾に基づきCiNiiから複製したものである relation: isVersionOf: http://ci.nii.ac.jp/naid/110004999317/ |
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資源タイプ | ||||||
内容記述タイプ | Other | |||||
内容記述 | text | |||||
フォーマット | ||||||
内容記述タイプ | Other | |||||
内容記述 | application/pdf | |||||
作成日 | ||||||
日付 | 2007-03-05 | |||||
日付タイプ | Created | |||||
アイテムID | ||||||
A3000039 |