The feasibility of two candidate leading-edge flow laminarization systems applicable to airline service was tested using representative airline operational conditions with respect to air traffic, weather, and airport insect infestation. One of the systems involved a perforated Ti alloy suction surface with about 1 million 0.0025-in. diameter holes drilled by electron beam, as well as a Krueger-type flap that offered protective shielding against insect impingement; the other supplied surface suction through a slotted Ti alloy skin with 27 spanwise slots on the upper and lower surface.


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    Titel :

    Laminar flow control leading edge systems in simulated airline service


    Beteiligte:
    Wagner, R. D. (Autor:in) / Maddalon, D. V. (Autor:in) / Fisher, D. F. (Autor:in)

    Kongress:

    ICAS Congress ; 1988 ; Jerusalem, Israel


    Erscheinungsdatum :

    1988-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Laminar Flow Control Leading Edge Systems in Simulated Airline Service

    R. D. Wagner / D. V. Maddalon / D. F. Fisher | NTIS | 1988


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    WAGNER, R. D. / MADDALON, D. V. / FISHER, D. F. | AIAA | 1990


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