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    Title :

    Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85


    Contributors:

    Publication date :

    1954-10-11


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    Experiment of Dynamic Angle-of-Attack on a Side Wall Compression Scramjet Inlet at Mach 3.85

    Liu, K. / Zhang, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011