Wind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-thick airfoil designed for general aviation applications. The results were compared with NACA 12 percent-thick sections and with the 17 percent-thick NASA airfoil. The tests were conducted ovar a Mach number range from 0.10 to 0.35. Chord Reynolds numbers varied from about 2,000,000 to 9,000,000.


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    Titel :

    Low-speed aerodynamic characteristics of a 13-percent-thick airfoil section designed for general aviation applications


    Beteiligte:
    Mcghee, R. J. (Autor:in) / Beasley, W. D. (Autor:in) / Somers, D. M. (Autor:in)

    Erscheinungsdatum :

    1975-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :