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    Title :

    Distribution of lift and pitching moment between wing and fuselage and effects of wing flexibility and dive brake on a 1/30-scale semispan model of the Bell X-5 airplane at transonic speeds as determined by the NACA wing-flow method


    Contributors:

    Publication date :

    1954-03-23


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English