Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in transonic wind tunnel


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    Title :

    Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location


    Contributors:

    Publication date :

    1960-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English