In wind tunnel investigation, pressure distributions, tuft studies, and boundary layer measurements were obtained for Reynolds number of 5.8 million.


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    Title :

    Boundary-layer and stalling characteristics of NACA 63-009 airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Gault, D.E. (author)


    Publication date :

    1949


    Size :

    30 pages


    Remarks:

    Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Boundary-layer and stalling characteristics of NACA 64a010 airfoil section

    Peterson, R.F. | Engineering Index Backfile | 1950


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

    McCullough, G.B. / Gault, D.E. | Engineering Index Backfile | 1949



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

    McCullough, George B. / Gault, Donald E. | TIBKAT | 1949