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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    Title :

    Jet engine nozzle exit configurations and associated systems and methods


    Contributors:

    Publication date :

    2011-06-28


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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