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    Title :

    Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket Propelled Vehicles


    Contributors:

    Publication date :

    1952-07-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English