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    Title :

    An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47 Degrees Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-Foot High-Speed Tunnel


    Contributors:

    Publication date :

    1951-10-31


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English