Results indicated that larger flap would provide greater lift increments but would lose lift effectiveness at higher deflections and at lower angle of attack than would smaller flap.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wind-tunnel investigation of NACA 0009 airfoil with 0.25- and 0.50-airfoil-chord plain flaps tested independently and in combination


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :