Tests made to define characteristics of two of configurations used in comprehensive investigation of control surface characteristics and also to provide additional data for comparison with previous boundary layer analyses.


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    Title :

    Wind-tunnel investigation of boundary layer on NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    53 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :