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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Pressure distribution over airfoil section with flap and tab


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1936


    Size :

    11 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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

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



    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 airfoil with balanced split flap

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