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デトネーション駆動形衝撃波管の作動特性
https://sucra.repo.nii.ac.jp/records/12656
https://sucra.repo.nii.ac.jp/records/12656bdcd8280-8582-4b78-a789-f877cfc5ac45
名前 / ファイル | ライセンス | アクション |
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A3000069.pdf (546.7 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2007-09-10 | |||||
タイトル | ||||||
タイトル | デトネーション駆動形衝撃波管の作動特性 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Combustion | |||||
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 | Shock Tube | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Detonation-Driver | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Mach Number | |||||
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 | A Study on Performance of a Detonation-Driven Shock Tube | |||||
著者 |
山中, 昭央
× 山中, 昭央× 有賀, 洋介× 小原, 哲郎× 蔡, 品× 大八木, 重治 |
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著者 ローマ字 | ||||||
YAMANAKA, Akio | ||||||
著者 ローマ字 | ||||||
ARIGA, Yousuke | ||||||
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(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 巻 66, 号 651, p. 2992-2998, 発行日 2000 |
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年月次 | ||||||
2000-11 | ||||||
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 | 03875016 | |||||
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 as a useful facilities capable of producing high-enthalpy flow. In this apparatus, a strong shock wave is generated by detonating oxygen-hydrogen (oxyhydrogen) mixture and has characteristics that temperature as well as pressure of driver gas is extremely high compared with conventional shock tubes. However, a structure of detonation wave is not uniform e.g., detonation wave has three-dimensional cellular structures and multiple transverse waves. Furthermore, the detonation wave is followed by a Taylor expansion fan and 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 a profile of ionization current behind detonation wave. As a result, (i) the pressure histories of detonation wave is clarified and it shows reasonable agreement with a result obtained by KASIMIR shock tube simulation code. (ii) A propagation velocity of detonation wave is coincided well with theoretical predictions assuming Chapman-Jouguet detonation wave. (iii) An equivalence ratio of oxyhydrogen mixture to produce a highest Mach number of the shock wave is evaluated as 〓≃1.7. | |||||
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 | ||||||
A3000069 |