The potential application of hybrid laminar flow control (HLFC) to the external surface of an advanced, high bypass ratio turbofan engine nacelle with a wetted area that approaches 15 percent of the wing total wetted area of future commercial transports is presented. A pressure distribution compatible with HLFC is specified and the corresponding nacelle geometry is computed employing a predictor/corrector design technique. Performance evaluations on an advanced twin-engine transport configuration are discussed to determine potential benefits in terms of reduced fuel consumption.


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    Titel :

    Hybrid laminar flow control applied to advanced turbofan engine nacelles


    Beteiligte:

    Kongress:

    SAE, Aerospace Atlantic Conference ; 1992 ; Dayton, OH, United States


    Erscheinungsdatum :

    1992-04-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Hybrid Laminar Flow Control Applied to Advanced Turbofan Engine Nacelles

    Collier, F. S. / Arcara, P. C. / Wie, Y. S. | SAE Technical Papers | 1992


    Application of Laminar Flow Control to High-Bypass-Ratio Turbofan Engine Nacelles

    Collier, F. S. / Wagner, R. D. / Wie, Y. S. | SAE Technical Papers | 1991


    Application of laminar flow control to high-bypass-ratio turbofan engine nacelles

    Wie, Y.S. / Collier, F.S. jun. / Wagner, R.D. | Tema Archiv | 1991


    Hybrid laminar flow technology for aero-engine nacelles

    Mullender, A.J. / Poll, D.I.A. | Tema Archiv | 1995


    Hybrid Laminar Flow Technology for Aero-Engine Nacelles

    Mullender, A. J. / Poll, D. I. A. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995