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    Title :

    Wind-tunnel Investigation of the Effects of Lip Geometry on Drag and Pressure Recovery of a Normal-shock Nose Inlet on a Body of Revolution at Mach Numbers of 1.41 and 1.81


    Contributors:

    Publication date :

    1958-02-03


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English