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    Title :

    Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Reynolds Number at Supersonic Mach Numbers on the Longitudinal Characteristics of a Wing Twisted and Cambered for Uniform Load


    Contributors:

    Publication date :

    1950-10-09


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English