The potential of laminar flow nacelles for reducing installed engine/nacelle drag was studied. The purpose was twofold: to experimentally verify a method for designing laminar flow nacelles and to determine the effect of installation on the extent of laminar flow on the nacelle and on the nacelle pressure distributions. The results of the isolated nacelle tests illustrated that laminar flow could be maintained over the desired length. Installing the nacelles on wing/pylon did not alter the extent of laminar flow occurring on the nacelles. The results illustrated that a significant drag reduction was achieved with this laminar flow design. Further drag reduction could be obtained with proper nacelle location and pylon contouring.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Natural Laminar Flow Nacelle for Transport Aircraft


    Beteiligte:
    M. Lamb (Autor:in) / W. K. Abeyounis (Autor:in) / J. C. Patterson (Autor:in) / R. J. Re (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hybrid Laminar Flow Nacelle Design

    Lecordix, J. L. / Mullender, A. / Lecossais, E. et al. | British Library Conference Proceedings | 1996


    Hybrid Laminar Flow Nacelle Design

    Lecordix, J. L. / Mullender, A. / Lecossais, E. et al. | British Library Online Contents | 1996


    Natural laminar flow flight experiments on a turbine engine nacelle fairing

    OBARA, C. / HASTINGS, E. / SCHOENSTER, J. et al. | AIAA | 1986


    NACELLE INLET ASSEMBLY THAT PROMOTES LAMINAR FLOW

    RUST CHARLES WILLIAM | Europäisches Patentamt | 2024

    Freier Zugriff

    Development of an active laminar flow nacelle

    MOUNT, J. / MILLMAN, V. | AIAA | 1985