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    WIND TUNNEL RESULTS FOR A HIGH SPEED, NATURAL LAMINAR FLOW AIRFOIL DESIGNED FOR GENERAL AVIATION AIRCRAFT

    Subjects
    Laminar Flow
    Links
    http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19880004696.pdf
    Record Type
    TECHPAP
    Corporate Author
    NASA Langley Research Center, Hampton, VA
    Author
    Sewall, William G
    Notes
    IM - 649034287
    Description
    IM - 649034287
    Publication Date
    2022
    Collection
    EVL Archive
    • Email Address[email protected]

     

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