Tests carried out on NACA 2414.5 wing section over range of airplane speeds giving max Reynolds Number of 15,000,000; tests also made to locate point of transition from laminar to turbulent boundary layer and to determine velocity distribution along upper surface of wing.


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    Title :

    Determination of profile drag of airplane wing in flight at high Reynolds numbers


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1939


    Size :

    9 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :