Pressure distribution tests of Clark Y airfoil with flap and inset tab measured on both upper and lower surfaces at one chord section; calculations of normal force and pitching moment coefficients of airfoil section and normal force and hinge moment coefficients of flap section with tab, also normal force and hinge moment coefficients of tab section alone; comparisons of theoretical and experimental values. (10c)


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    Titel :

    Pressure distribution over airfoil section with flap and tab


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:


    Erscheinungsdatum :

    1936


    Format / Umfang :

    11 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Pressure distribution over clarke Y-H airfoil section with split flap

    Wenzinger, C.J. | Engineering Index Backfile | 1937



    Pressure distribution over a symmetrical airfoil section with trailing edge flap

    Jacobs, Eastman N. / Pinkerton, Robert M. | TIBKAT | 1930


    Pressure distribution over clarke Y-H airfoil section with split flap

    Wenzinger, C.J. | Engineering Index Backfile | 1937


    Pressure distribution over airfoil with balanced split flap

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