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Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor
http://hdl.handle.net/2237/00030143
http://hdl.handle.net/2237/0003014352280bb8-cda6-42ab-92bc-c9831d34c7f2
名前 / ファイル | ライセンス | アクション |
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2019-05-09 | |||||
タイトル | ||||||
タイトル | Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor | |||||
言語 | en | |||||
著者 |
Yamaguchi, Masato
× Yamaguchi, Masato× Matsuoka, Ken× Kawasaki, Akira× Kasahara, Jiro× Watanabe, Hiroaki× Matsuo, Akiko |
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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 | |||||
権利 | ||||||
言語 | en | |||||
権利情報 | © 2019. This manuscript version is made available under the CC-BY-NC-ND 4.0 license http://creativecommons.org/licenses/by-nc-nd/4.0/ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shock induced combustion | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Reflected shock wave | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Reflective shuttling detonation combustor | |||||
抄録 | ||||||
内容記述 | As a novel detonation combustor that differs from a pulse and a rotating detonation engine, a reflective shuttling detonation combustor (RSDC), in which detonation waves shuttle repeatedly, was proposed. In a fan-shaped two-dimensional combustor, detonation waves propagate, repeating attenuation and re-ignition by a shock reflection at the side wall. In the demonstration experiment, chemiluminescence visualization and pressure measurement with ethylene–oxygen mixture were conducted at the same time. As the result, a single shuttling wave coupled with pressure rise was observed in the combustor. The tangential velocity of the wave was 1526 ± 12 m/s and approximately 60% of the estimated Chapman–Jouguet velocity of 2513 m/s. The ratio of pressure in front of the wave to one behind the primary wave or the reflected wave was in good agreement with one-dimensional shock theory, and it was suggested that the rapid reaction behind the reflected shock wave sustained the continuous propagation of the shock wave. | |||||
言語 | en | |||||
内容記述タイプ | Abstract | |||||
内容記述 | ||||||
内容記述 | ファイル公開:2021-01-01 | |||||
言語 | ja | |||||
内容記述タイプ | Other | |||||
出版者 | ||||||
言語 | en | |||||
出版者 | Elsevier | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプresource | http://purl.org/coar/resource_type/c_6501 | |||||
タイプ | journal article | |||||
出版タイプ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
DOI | ||||||
関連タイプ | isVersionOf | |||||
識別子タイプ | DOI | |||||
関連識別子 | https://doi.org/10.1016/j.proci.2018.06.210 | |||||
ISSN(print) | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 1540-7489 | |||||
書誌情報 |
en : Proceedings of the Combustion Institute 巻 37, 号 3, p. 3741-3747, 発行日 2019 |
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著者版フラグ | ||||||
値 | author |