Art

J-GLOBAL ID：202002278695819222   Reference number：20A0645275

Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles

種々のノズルを持つ回転デトネーションエンジンの推進性能と加熱環境【JST・京大機械翻訳】

Author (10)： Goto Keisuke (Nagoya University, Nagoya 464-8603, Japan) ,  Nishimura Junpei (Nagoya University, Nagoya 464-8603, Japan) ,  Kawasaki Akira (Nagoya University, Nagoya 464-8603, Japan) ,  Matsuoka Ken (Nagoya University, Nagoya 464-8603, Japan) ,  Kasahara Jiro (Nagoya University, Nagoya 464-8603, Japan) ,  Matsuo Akiko (Keio University, Yokohama 223-8522, Japan) ,  Funaki Ikkoh (Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan) ,  Nakata Daisuke (Muroran Institute of Technology, Muroran, Hokkai-do 050-8585, Japan) ,  Uchiumi Masaharu (Muroran Institute of Technology, Muroran, Hokkai-do 050-8585, Japan) ,  Higashino Kazuyuki (Muroran Institute of Technology, Muroran, Hokkai-do 050-8585, Japan)
Material： Journal of Propulsion and Power  (J Propul Power)
Volume： 35  Issue： 1  Page： 213-223  Publication year： 2019 
JST Material Number： C0207B  ISSN： 1533-3876  CODEN： JPPOEL  Document type： Article
Article type： 原著論文  Country of issue： United States (USA)  Language： ENGLISH (EN)

Abstract/Point： Geometric throats are commonly...

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Thesaurus term： adaptability ,  specific thrust ,  mass flux ,  back pressure ,  heat flux ,  thrust ,  combustor ,  heat resisting material ,  vacuum vessel ,  doublet ,  diaphragm(optics) ,  rocket ,  *propulsive performance ,  injector ,  channel

JST classification (1)： Gas turbines  (PB02040Y)

Terms in the title (3)： デトネーション ,  推進性能 ,  熱環境