A rotorcraft is provided and includes a fuselage. The fuselage includes drag generating portions, a main rotor assembly and an auxiliary propulsor having an expected propulsion efficiency. The auxiliary propulsor is disposed to ingest boundary layer flows and in wake regions associated with the drag generating portions and is provided with a corresponding increase in the expected propulsion efficiency thereof.


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    Titel :

    ROTORCRAFT CONFIGURATION AND METHOD OF ROTORCRAFT DESIGN


    Beteiligte:
    MOFFITT BLAKE ALMY (Autor:in) / WAKE BRIAN E (Autor:in) / LORBER PETER F (Autor:in)

    Erscheinungsdatum :

    2017-10-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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