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    Title :

    Results of Initial Wind-tunnel Flutter Experiments at Low Speed with a Towed Airplane Model Having a 40 Degree Sweptback Wing of Aspect Ratio 3.62 Equipped with Pylon-mounted Stores


    Contributors:

    Publication date :

    1955-03-24


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English