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  1. No Access

    Chapter and Conference Paper

    Effects of Attack Angle on Starting Performance of a Hypersonic Inlet

    Since the boundary of an inlet starting Mach number cannot be obtained easily in high speed wind tunnels. The correlations between changing the attack angle and changing the freestream Mach number which affect...

    Shuaitao Guo, Wenzhi Gao, Enlai Zhang… in 30th International Symposium on Shock Wave… (2017)

  2. No Access

    Chapter and Conference Paper

    Oscillatory Behaviors of a Hypersonic Inlet with Trips

    A hypersonic inlet should be operated in a started mode for the efficient operation of an air-breathing propulsion system [1]. Various factors, either in design or in usage, may cause the hypersonic inlet to u...

    Wenzhi Gao, Shuaitao Guo, Zhufei Li… in 30th International Symposium on Shock Wave… (2017)