Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability


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    Title :

    Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5


    Contributors:

    Publication date :

    1960-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English