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エタノール/液体酸素ロケットエンジン燃焼室における平面ピントル型噴射器の推進剤噴射運動量比が燃焼挙動に及ぼす影響

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エタノール/液体酸素ロケットエンジン燃焼室における平面ピントル型噴射器の推進剤噴射運動量比が燃焼挙動に及ぼす影響

Call No. (NDL)
Z74-B503
Bibliographic ID of National Diet Library
027925919
Material type
記事
Author
角銅 洋実ほか
Publisher
東京 : 日本航空宇宙学会
Publication date
2017-02
Material Format
Paper
Journal name
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 65(1):2017.2
Publication Page
p.1-9
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Paper Digital

Material Type
記事
Author/Editor
角銅 洋実
榊 和樹
中谷 辰爾
津江 光洋
金井 竜一郎
稲川 貴大
平岩 徹夫
Alternative Title
Effects of Propellant Momentum Ratio on Combustion Behavior in an Ethanol/Liquid Oxygen Rocket Engine Combustor with a Planar Pintle-type Injector
Periodical title
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
No. or year of volume/issue
65(1):2017.2
Volume
65
Issue
1
Pages
1-9