Flight and wind tunnel studies have shown that compressibility will have serious adverse effects on characteristics of usual flap type control surface; tests made to investigate these effects.


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    Title :

    High-speed wind-tunnel tests of NACA 0009-64 airfoil having 33.4-percent chord flap with overhang 20.1 percent of flap chord


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    33 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :