Wind tunnel tests were conducted to evaluate a natural laminar flow airfoil designed for the high speed jet aircraft in general aviation. The airfoil, designated as the High Speed Natural Laminar Flow (HSNLF)(1)-0213, was tested in two dimensional wind tunnels to investigate the performance of the basic airfoil shape. A three dimensional wing designed with this airfoil and a high lift flap system is also being evaluated with a full size, half span model.


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    Title :

    Wind Tunnel Results of the High-Speed NLF(Natural Flow Control)(1)-0213 Airfoil


    Contributors:
    W. G. Sewall (author) / R. J. McGhee (author) / D. E. Hahne (author) / F. L. Jordan (author)

    Publication date :

    1987


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Wind tunnel results of the high-speed NLF(1)-0213 airfoil

    Sewall, William G. / Mcghee, Robert J. / Hahne, David E. et al. | NTRS | 1987



    Wind tunnel results for a high-speed, natural laminar-flow airfoil designed for general aviation aircraft

    Sewall, William G. / Mcghee, Robert J. / Viken, Jeffery K. et al. | NTRS | 1985