Viscous Shock Layer Studies of a Super Orbital Reentry Capsule Using a Multi Vibrational Temperature Model
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概要
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Numerical studies of the shock layer of a super orbital reentry capsule have been conducted by using thermochemical nonequilibrium VSL (Viscous Shock Layer) equations. In the present analysis, vibrational temperature has been treated as individual molecul
- 宇宙航空研究開発機構の論文
著者
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Nishida Michio
Department Of Aemonautical Engineering Kyushu University
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Doihara Ryouji
Department of Aeronautics and Astronautics, Kyushu University
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Doihara Ryouji
Department Of Aeronautics And Astronautics Kyushu University
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