Aspects of the disclosure are directed to a nacelle of an aircraft, comprising a surface that is profiled such that during cruise flight operation lines of constant static pressure of a boundary layer around the nacelle (422; 522) in a given region are substantially contained within a plane that is normal to an engine axis.


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    Title :

    OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGESTION ACTIVE LAMINAR FLOW CONTROL


    Additional title:

    OPTIMIERTES GONDELPROFIL UND OPTIMIERTE KAMMERFORM FÜR GRENZSCHICHTAUFNAHMEAKTIVE LAMINARE STRÖMUNGSSTEUERUNG
    PROFIL DE NACELLE OPTIMISÉE ET FORME DE PLÉNUM PERMETTANT LA RÉGULATION DE FLUX INGÉRÉ DE COUCHES LIMITES LAMINAIRES ACTIVES


    Contributors:

    Publication date :

    2021-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT






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