The aircraft exhaust engine nozzle system includes a fan nozzle to receive a fan flow from a fan disposed adjacent to an engine disposed above an airframe surface of the aircraft, a core nozzle disposed within the fan nozzle and receiving an engine core flow, and a pylon structure connected to the core nozzle and structurally attached with the airframe surface to secure the engine to the aircraft.


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    Titel :

    Aircraft Engine Exhaust Nozzle System for Jet Noise Reduction


    Beteiligte:

    Erscheinungsdatum :

    2014-11-04


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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