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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    Titel :

    The NACA CYH Airfoil Section


    Beteiligte:

    Erscheinungsdatum :

    01.06.1926


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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