An inlet for a propulsion system has an upper wall and a lower wall and a throat extending between the upper wall and the lower wall. The lower wall has a bump edge located immediately after the throat.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Blended Wing Body Boundary Layer Ingesting Inlet Design Integration


    Beteiligte:

    Erscheinungsdatum :

    2016-05-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Boundary-Layer-Ingesting Inlet Flow Control

    Owens, L.R. | Online Contents | 2008


    Boundary-Layer-Ingesting Inlet Flow Control

    Owens, Lewis / Allan, Brian / Gorton, Susan | AIAA | 2006


    Design Exploration for Vortex Generators on Boundary-Layer-Ingesting Inlet

    Lee, B.J. / Kumano, T. / Liou, M.-S. et al. | British Library Conference Proceedings | 2010


    Fan Response to Boundary-Layer Ingesting Inlet Distortions

    Giuliani, James E | Online Contents | 2016


    Fan Response to Boundary-Layer Ingesting Inlet Distortions

    Giuliani, James E. / Chen, Jen-Ping | AIAA | 2016