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    Title :

    Effects of a fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24 as determined by the NACA wing flow method


    Contributors:

    Publication date :

    1951-02-08


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English