The Proceedings of the Fluids engineering conference
Online ISSN : 2424-2896
2000
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Study on Scramjet Intake Flows Using a High Enthalpy Shock Tunnel
Takakage ARAI, Jiro KASAHARA, Takashi KOKUBO, Nobutaka AKAI, Koji MUKAI
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Keywords: Scramjet engine, shock system, interaction between the supersonic hot stream and normal gas injection
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Pages 43-

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© 2000 The Japan Society of Mechanical Engineers
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