A Thermochemical Nonequilibrium Flow around a Super Orbital Reentry Capsule with Ablation
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概要
- 論文の詳細を見る
The aerodynamic heating to the super orbital reentry capsule of MUSES-C with ablation was numerically studied by using thermochemical nonequilibrium full viscous shock layer (VSL) equations. An 11 air-species model was used for non-ablating boundary condi
- 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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Nishida M
Department Of Aeronautics And Astronautics Kyushu University
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Doihara Ryouji
Department of Aeronautics and Astronautics, Kyushu University
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Doihara R
Department Of Aeronautics And Astronautics Kyushu University
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Doihara Ryouji
Department Of Aeronautics And Astronautics Kyushu University
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