Investigation carried out in NACA 7-ft by 10-ft wind tunnel; results obtained given in form of diagrams showing chordwise distribution of pressure on both airfoil and flap and as plots of calculated aerodynamic coefficients for both airfoil and flap.


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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1937


    Size :

    5 pages


    Remarks:

    6 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :