Supersonic commercial transport aircraft (SCT) are known for their short travel times and also for their low-speed noise. This paper focuses on the aerodynamic design of low-drag SCT high-lift systems contributing significant low-speed noise reductions by enabling steeper climbing. The high-lift system design - relying on separated flow- and validation work at DLR will be reported.


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    Titel :

    Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft


    Beteiligte:
    Herrmann, U. (Autor:in)


    Erscheinungsdatum :

    2006


    Format / Umfang :

    8 Seiten





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






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    SUPERSONIC INTERFERENCE LIFT

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