Flowfield Around MUSES-C Superorbital Re-entry Capsule
スポンサーリンク
概要
- 論文の詳細を見る
The spatial flow structure around a model of the MUSES-C capsule traveling at a speed of Mach 10 was investigated utilizing the electric discharge method. The shock shape ahead of the capsule was observed utilizing a technique for visualizing shock shapes, then the streamline following the shock wave was observed utilizing the technique for visualizing streamlines crossing a shock wave. Subsequently, the flow pattern including the re-circulation region such as a separation point, free shear layer, and rear stagnation location behind the capsule was observed utilizing a technique of the electric discharge method. These experiments have made clear the spatial flow structure before and behind the capsule, which had been very difficult to visualize.
- 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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