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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Jet Engine Nozzle Exit Configurations and Associated Systems and Methods


    Contributors:

    Publication date :

    2013-08-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    JET ENGINE NOZZLE EXIT CONFIGURATIONS AND ASSOCIATED SYSTEMS AND METHODS

    MENGLE VINOD G | European Patent Office | 2018

    Free access

    JET ENGINE NOZZLE EXIT CONFIGURATIONS AND ASSOCIATED SYSTEMS AND METHODS

    MENGLE VINOD G | European Patent Office | 2016

    Free access

    JET ENGINE NOZZLE EXIT CONFIGURATIONS AND ASSOCIATED SYSTEMS AND METHODS

    MENGLE VINOD G | European Patent Office | 2018

    Free access

    Non-intrusive Space Shuttle Main Engine nozzle exit diagnostics

    SHIRLEY, JOHN / BOEDEKER, LAURENCE | AIAA | 1988