An investigation of a 1/4-scale supersonic target drone model was performed in the Langley Unitary Plan wind tunnel to determine the effects of various sizes of canards, vertical tails, and ailerons on the aerodynamic characteristics. The tests were made at Mach numbers from 1.57 to 2.10 through an angle-of-attack range from about -5 to 23 deg.


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    Title :

    Aerodynamic Characteristics of a Target Drone Vehicle at Mach Numbers from 1.57 to 2.10


    Contributors:

    Publication date :

    1968


    Size :

    72 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English