An engine inlet for efficient operation at both design Mach number and off-design Mach numbers with an inlet 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 to an extended position aligned with an off-design Mach number shock wave.


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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 :

    29.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT