Compressibility effects investigated from pressure distributions obtained at various airfoil angles of attack and aileron angles for Mach numbers from 0.25 to approximately 0.76; wind tunnel data indicated reduction in stick force and improvement in stick force characteristics at high diving speeds.


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    Title :

    Effect of compressibility on section characteristics of airfoil with round-nose slotted Frise Aileron


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Luoma, A.A. (author)


    Publication date :

    1946


    Size :

    17 pages


    Remarks:

    Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :