Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of NACA 653-418, a = 1.0 Airfoil Section (Confidential Bul L5J04).


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    Title :

    Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of NACA 653-418, a = 1.0 airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1945


    Size :

    7 pages


    Remarks:

    8 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :