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  1. B200 工学部/工学研究科
  2. B200a 雑誌掲載論文
  3. 学術雑誌

Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor

http://hdl.handle.net/2237/00030143
http://hdl.handle.net/2237/00030143
52280bb8-cda6-42ab-92bc-c9831d34c7f2
名前 / ファイル ライセンス アクション
Supersonic_combustion.pdf Supersonic_combustion (964.5 kB)
Item type 学術雑誌論文 / Journal Article(1)
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

WEKO 90976

en Yamaguchi, Masato

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Matsuoka, Ken

× Matsuoka, Ken

WEKO 90977

en Matsuoka, Ken

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Kawasaki, Akira

× Kawasaki, Akira

WEKO 90978

en Kawasaki, Akira

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Kasahara, Jiro

× Kasahara, Jiro

WEKO 90979

en Kasahara, Jiro

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Watanabe, Hiroaki

× Watanabe, Hiroaki

WEKO 90980

en Watanabe, Hiroaki

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Matsuo, Akiko

× Matsuo, Akiko

WEKO 90981

en Matsuo, Akiko

Search repository
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
著者版フラグ
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