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    Title :

    Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness of an Elevon as a Longitudinal Control and the Effects of Camber and Twist on the Maximum Lift-drag Ratio at Supersonic Speeds


    Contributors:

    Publication date :

    1950-05-08


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English