An investigation was made in the N.A.C.A. 7 by 10 foot wind tunnel of the distribution of air pressure over one chord section of a Clark Y-H airfoil with a split flap. The results obtained are given in the form of diagrams showing the chordwise distribution of pressure on both airfoil and flap as plots of calculated aerodynamic coefficients for both airfoil and flap.


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    Title :

    Pressure distribution over a Clark Y-H airfoil section with a split flap


    Contributors:

    Publication date :

    1937-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    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 airfoil with balanced split flap

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