Utilization of Expansion Tube for MUSES-C Reentry Simulation
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概要
- 論文の詳細を見る
An expansion tube has a unique capability of generating a hypervelocity flow without experiencing a stagnation condition of the test gas. Related to MUSES-C superorbital reentry flow condition, experimental and numerical simulations were conducted in dome
- 宇宙航空研究開発機構の論文
著者
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Sawada Keisuke
Department Of Aeronautical Engineering Kyoto University
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Sawada Keisuke
Department Of Aeronautics And Space Engineering Tohoku University
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Abe Takashi
Institute of Space and Astronautical Science (ISAS)
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Sasoh Akihiro
Shock Wave Research Cener Institute Of Fluid Science Tohoku University
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Otsu Hirotaka
Department Of Mechanical Engineering Shizuoka University
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Mizuno Hiroyasu
Department of Aeronautics and Space Engineering, Tohoku University
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Mizuno Hiroyasu
Department Of Aeronautics And Space Engineering Tohoku University
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Abe Takashi
Institute Of Space And Astronautical Science
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