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J-GLOBAL ID：201902246612116067   Reference number：19A0336818

Critical condition of inner cylinder radius for sustaining rotating detonation waves in rotating detonation engine thruster

回転デトネーションエンジンスラスタにおける回転デトネーション波を維持するための内部円筒半径の臨界条件【JST・京大機械翻訳】

Author (7)： Kawasaki Akira (Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi 464-8603, Japan) ,  Inakawa Tomoya (Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi 464-8603, Japan) ,  Kasahara Jiro (Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi 464-8603, Japan) ,  Goto Keisuke (Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi 464-8603, Japan) ,  Matsuoka Ken (Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi 464-8603, Japan) ,  Matsuo Akiko (Department of Mechanical Engineering, Keio University, 3-14-1 Hiyoshi, Kouhoku-ku, Yokohama, Kanagawa 223-8522, Japan) ,  Funaki Ikkoh (Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa 252-5210, Japan)
Material： Proceedings of the Combustion Institute  (Proc Combust Inst)
Volume： 37  Issue： 3  Page： 3461-3469  Publication year： 2019 
JST Material Number： A0273A  ISSN： 1540-7489  Document type： Proceedings
Article type： 原著論文  Country of issue： Netherlands (NLD)  Language： ENGLISH (EN)

Abstract/Point： We describe the critical condi...

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Thesaurus term： thrust ,  soot ,  deflagration ,  *cylinder (hollow body) ,  *detonation ,  *detonation wave ,  chemiluminescence ,  combustion chamber ,  shock (mechanics) ,  plume ,  propellant ,  specific thrust ,  outer space ,  *thruster
Semi thesaurus term： ロケット推進 , 【Automatic Indexing@JST】

Author keywords (3)： Rotating detonation engine ,  Critical condition of detonation ,  Detonation

JST classification (1)： Combustion in general  (XE04010W)

Terms in the title (3)： デトネーション波 ,  半径 ,  臨界条件