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:

    Publication date :

    1977-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :