Experimental Study of Nonequilibrium Phenomena behind Strong Shock Waves Generated in Super-orbital Reentry Flight

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The flow behavior in a thin air behind the shock wave with a shock velocity around 12 km/sec was investigated experimentally. For the experiment, a free-piston-driven shock tube was used and a radiation from behind the shock front was investigated spectro
宇宙航空研究開発機構の論文

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