A wind tunnel investigation has been conducted to determine the longitudinal and lateral aerodynamic characteristics of a model of a supersonic cruise fighter configuration with a design Mach number of 2.60. The configuration is characterized by a highly swept arrow wing twisted and cambered to minimize supersonic drag due to lift, twin wing mounted vertical tails, and an aft mounted integral underslung duel-engine pod. The investigation also included tests of the configuration with larger outboard vertical tails and with small nose strakes.


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    Title :

    Subsonic and Supersonic Aerodynamic Characteristics of a Supersonic Cruise Fighter Model with a Twisted and Cambered Wing with 74 Deg Sweep


    Contributors:

    Publication date :

    1977


    Size :

    63 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English