An experimental investigation was conducted on a model of a wing control version of the Sparrow III type missile to determine the static aerodynamic characteristics over an angle of attack range from 0 deg to 40 deg for Mach numbers from 1.50 to 4.60.


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    Title :

    Supersonic Aerodynamic Characteristics of a Sparrow 3 Type Missile Model with Wing Controls and Comparison with Existing Tail-Control Results


    Contributors:
    W. J. Monta (author)

    Publication date :

    1977


    Size :

    84 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English