Study on Shock-Wave/Boundary-Layer Interaction in Hypersonic Flow
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概要
- 論文の詳細を見る
Investigations on the spatial flowfield of hypersonic shock-wave/boundary-layer interaction have been performed utilizing the electric discharge method. The model geometry used in this experiment is composed of a flat plate and a fin. In general, visualizations of such spatial flowfield were very difficult or impossible. However, in these investigations utilizing the electric discharge method that is the method for visualizing three-dimensional hypersonic flowfield phenomena, the spatial flowfield phenomena could be visualized qualitatively. The experiment is carried out using a hypersonic gun tunnel whose main characteristics are that the Mach number is 10 and the duration is 10ms.
- 福山大学の論文
著者
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Nakamura Hiroaki
Fukuyama University
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NISHIO Masatomi
Department of Mechanical System Engineering, Fukuyama University
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SEZAKI Shinji
Fukuyama University
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NAKAMURA Hiroaki
福山大学工学部機械工学科
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NISHIO Masatomi
福山大学工学部機械工学科
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SEZAKI Shinji
福山大学工学部機械工学科
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Nakamura H
Fukuyama University
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Nishio M
Dept. Of Mechanical Engineering Fukuyama University
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Nishio Masatomi
Department Of Mechanical System Engineering Fukuyama University
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Sezaki S
Fukuyama University
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- Stabilization Time of Wake Behind Hypersonic Capsule
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