Nozzle exit configurations and associated systems and methods are disclosed. An aircraft system in accordance with one embodiment includes a jet engine exhaust nozzle having an internal flow surface and an exit aperture, with the exit aperture having a perimeter that includes multiple projections extending in an aft direction. Aft portions of individual neighboring projections are spaced apart from each other by a gap, and a geometric feature of the multiple can change in a monotonic manner along at least a portion of the perimeter.


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    Titel :

    Jet Engine Nozzle Exit Configurations and Associated Systems and Methods


    Beteiligte:

    Erscheinungsdatum :

    20.08.2013


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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