Item type |
itemtype_ver1(1) |
公開日 |
2021-11-16 |
タイトル |
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タイトル |
Experimental study of internal flow structures in cylindrical rotating detonation engines |
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言語 |
en |
著者 |
Yokoo, Ryuya
Goto, Keisuke
Kasahara, Jiro
Athmanathan, Venkat
Braun, James
Paniagua, Guillermo
Meyer, Terrence R.
Kawasaki, Akira
Matsuoka, Ken
Matsuo, Akiko
Funaki, Ikkoh
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アクセス権 |
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アクセス権 |
open access |
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アクセス権URI |
http://purl.org/coar/access_right/c_abf2 |
権利 |
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言語 |
en |
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権利情報 |
© 2020. 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 |
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主題Scheme |
Other |
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主題 |
Detonation |
キーワード |
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主題Scheme |
Other |
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主題 |
Cylindrical rotating detonation engine |
キーワード |
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主題Scheme |
Other |
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主題 |
Hollow rotating detonation engine |
キーワード |
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主題Scheme |
Other |
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主題 |
Flow structure |
キーワード |
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主題Scheme |
Other |
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主題 |
Optically accessible combustor |
内容記述 |
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内容記述タイプ |
Abstract |
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内容記述 |
The internal flow structures of detonation wave were experimentally analyzed in an optically accessible hollow rotating detonation combustor with multiple chamber lengths. The cylindrical RDC has a glass chamber wall, 20 mm in diameter, which allowed us to capture the combustion self-luminescence. A chamber 70 mm in length was first tested using C2H4single bondO2 and H2–O2 as propellants. Images with a strong self-luminescence region near the bottom were obtained, confirming the small extent of the region where most of the heat release occurs as found in our previous research. Based on the visualization experiments, we tested RDCs with shorter chamber walls of 40 and 20 mm. The detonation wave was also observed in the shorter chambers, and its velocity was not affected by the difference in chamber length. Thrust performance was also maintained compared to the longer chamber, and the short cylindrical RDC had the same specific impulse tendency as the cylindrical (hollow) or annular 70-mm chamber RDC. Finally, we calculated the pressure distributions of various chamber lengths, and found they were also consistent with the measured pressure at the bottom and exit. We concluded that the short-chamber cylindrical RDC with equal length and diameter maintained thrust performance similar to the longer annular RDC, further expanding the potential of compact RDCs. |
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言語 |
en |
内容記述 |
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内容記述タイプ |
Other |
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内容記述 |
Available online 17 August 2020 |
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言語 |
en |
出版者 |
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出版者 |
Elsevier |
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言語 |
en |
言語 |
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言語 |
eng |
資源タイプ |
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資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
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資源タイプ |
journal article |
出版タイプ |
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出版タイプ |
AM |
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出版タイプResource |
http://purl.org/coar/version/c_ab4af688f83e57aa |
関連情報 |
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関連タイプ |
isVersionOf |
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識別子タイプ |
DOI |
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関連識別子 |
https://doi.org/10.1016/j.proci.2020.08.001 |
収録物識別子 |
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収録物識別子タイプ |
PISSN |
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収録物識別子 |
15407489 |
書誌情報 |
en : Proceedings of the Combustion Institute
巻 38,
号 3,
p. 3759-3768,
発行日 2021
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ファイル公開日 |
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日付 |
2022-08-17 |
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日付タイプ |
Available |