SUPERSONIC CARET INLET SYSTEM LEADING EDGE SLAT FOR IMPROVED INLET PERFORMANCE AT OFF-DESIGN FLIGHT An engine inlet for efficient operation at both design Mach number and off-design Mach numbers with an inlet (10) having a caret configuration with rotatably extending effective leading edges on the inlet from a retracted position aligned with a nominal Mach number shock wave (36) to an extended position aligned with an off-design Mach number shock wave (36'). ------ 10 FIG.lIA --- -- ----4--- --v -~ -- ---- FIG.l1B


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    Titel :

    Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions


    Beteiligte:
    HUYNH THUY (Autor:in)

    Erscheinungsdatum :

    27.02.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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