Characteristics investigated at Reynolds number of 5,800,000; data on measurements of lift, drag and pitching moment, chordwise distribution of pressure, visual studies of boundary layer flow and surveys of static pressure and velocity distribution within boundary layer.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Boundary-layer and stalling characteristics of NACA 64A006 airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    24 pages


    Remarks:

    Illus, diagrs, charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :