Investigation made in NACA 7 by 10-ft wind tunnel; various arrangements were tested to determine effect of number of slats and chords of slats used to form flap, of slot gap between slats, and of position of slats with respect to each other and to wing.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Rogallo, F.M. (author) / Spano, B.S. (author)


    Publication date :

    1942


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :