The NACA CYH airfoil section is described and its aerodynamic characteristics are given as tested in the NACA variable density wind tunnel at twenty atmosphere pressure. This section has a low drag, a high maximum lift, and a small travel of center of pressure.


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    Title :

    The NACA CYH Airfoil Section


    Contributors:

    Publication date :

    1926-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



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