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    Title :

    Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Characteristics Throughout the Subsonic Speed Range with the Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25


    Contributors:

    Publication date :

    1949-08-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English