An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the aerodynamic characteristics of a revised target drone vehicle through a Mach number range from 1.60 to 2.86. The vehicle had canard surfaces and a swept clipped-delta wing with twin tip-mounted vertical tails.


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    Title :

    Aerodynamic Characteristics of a Revised Target Drone Vehicle at Mach Numbers from 1.60 to 2.86


    Contributors:
    A. B. Blair (author) / C. D. Babb (author)

    Publication date :

    1968


    Size :

    54 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English