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    Title :

    An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : stability and control characteristics at a Mach number of 1.61 of the complete configuration equipped with spoilers


    Contributors:

    Publication date :

    1954-09-10


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English