Tests of Clark Y wing model to determine distribution of air loads over both wing and flap; tests made at various flap deflections up to 45° and covered range of angles of attack from zero lift to maximum lift for each flap deflection; deflecting partial-span split flap affected pressures and section normal-force and pitching-moment coefficients over entire wing span. (Price 10¢)


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    Title :

    Pressure distribution over rectangular airfoil with partial-span split flap


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1936


    Size :

    12 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Pressure distribution over a rectangular airfoil with a partial-span split flap

    Wenzinger, Carl J. / Harris, Thomas A. | TIBKAT | 1936


    Pressure distribution over airfoil with balanced split flap

    Ames, Jr., M.B. / Lowry, J.G. | Engineering Index Backfile | 1941