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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    Titel :

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


    Beteiligte:


    Erscheinungsdatum :

    1987-12-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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

    W. G. Sewall / R. J. McGhee / D. E. Hahne et al. | NTIS | 1987



    Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil

    Ferris, James C. / Mcghee, Robert J. / Barnwell, Richard W. | NTRS | 1987