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Study on Performance of Detonation-Driven Shock Tube(Compressible Flow and Detonation)
https://sucra.repo.nii.ac.jp/records/13478
https://sucra.repo.nii.ac.jp/records/13478ab25ab17-dfb0-43e8-aa77-d7d970ee1786
名前 / ファイル | ライセンス | アクション |
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A1003168.pdf (802.1 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2009-09-09 | |||||
タイトル | ||||||
タイトル | Study on Performance of Detonation-Driven Shock Tube(Compressible Flow and Detonation) | |||||
言語 | ||||||
言語 | eng | |||||
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 | |||||
著者 |
YAMANAKA, Akio
× YAMANAKA, Akio× ARIGA, Yosuke× 小原, 哲郎× CAI, Pin× 大八木, 重治 |
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著者 ローマ字 | ||||||
YAMANAKA, Akio | ||||||
著者 ローマ字 | ||||||
ARIGA, Yosuke | ||||||
著者 ローマ字 | ||||||
OBARA, Tetsuro | ||||||
著者 ローマ字 | ||||||
CAI, Pin | ||||||
著者 ローマ字 | ||||||
OHYAGI, Shigeharu | ||||||
著者 所属 | ||||||
埼玉大学大学院理工学研究科 | ||||||
著者 所属 | ||||||
埼玉大学大学院理工学研究科 | ||||||
著者 所属 | ||||||
埼玉大学工学部機械工学科 | ||||||
著者 所属 | ||||||
埼玉大学工学部機械工学科 | ||||||
著者 所属 | ||||||
埼玉大学工学部機械工学科 | ||||||
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) | ||||||
Department of Mechanical Engineering, Faculty of Engineering, Saitama University | ||||||
著者 所属(別言語) | ||||||
Department of Mechanical Engineering, Faculty of Engineering, Saitama University | ||||||
著者 所属(別言語) | ||||||
Department of Mechanical Engineering, Faculty of Engineering, Saitama University | ||||||
書誌情報 |
JSME international journal. Series B, Fluids and thermal engineering 巻 45, 号 2, p. 425-431, 発行日 2002 |
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年月次 | ||||||
2002-5 | ||||||
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 | 13408054 | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | A detonation-driven shock tube firstly designed by H.R. Yu is considered to be a useful apparatus for producing high-enthalpy flow. In this apparatus, a strong shock wave is generated by detonating an oxygen-hydrogen mixture (oxy-hydrogen) and the driver gas temperature and pressure are extremely high compared with those of a conventional shock tube. However, the structure of the detonation wave is not uniform, e.g., the detonation wave has three-dimensional cellular structures and multiple transverse waves. Furthermore, the detonation wave is followed by a Taylor expansion fan and the performance of detonation-driven shock tube is not well understood. In this preliminary study, a detonation-driven shock tube is constructed and its performance is experimentally investigated by measuring pressure histories and the profile of the ionization current behind the detonation wave. As a result, (i)the pressure history of the detonation wave is clarified and shows reasonable agreement with the result obtained by the KASIMIR shock tube simulation code. (ii) The propagation velocity of the detonation wave coincides well with the theoretical prediction assuming a Chapman-Jouguet detonation wave. (iii) The equivalence ratio of the oxy-hydrogen mixture to produce the highest Mach number of the shock wave is evaluated to be Φ≃1.7. | |||||
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/110003479056/ |
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版 | ||||||
[出版社版] | ||||||
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 | |||||
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 | 2009-09-09 | |||||
日付タイプ | Created | |||||
アイテムID | ||||||
A1003168 |