An investigation was conducted in the Langley low turbulence pressure tunnel to determine the low-speed, two dimensional characteristics of a 9.3 percent-thick supercritical airfoil. The airfoil was tested at Reynolds numbers (based on chord) from 2.9 million to 16.8 million, at Mach numbers from 0.10 to 0.36, and at geometric angles of attack from -8 degrees to 14 degrees.


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    Title :

    Low-Speed Aerodynamic Characteristics of a 9.3-Percent-Thick Supercritical Airfoil Section


    Contributors:
    K. W. Noonan (author) / R. J. Mcghee (author)

    Publication date :

    1982


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English