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    Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft

    Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft


    Abstract This paper carries out a modeling method of ducted propulsion system of vertical take-off and landing aircraft. On axial flow condition, the model of ducted propulsion system, based momentum theory, is established and verified. Based on the non-dimensional definition of open propeller, the non-dimensional method, applied to the ducted blades, is proposed. The research shows that the ducted propulsion system model and the ducted blade non-dimensional method are reasonable and effective, for high performance aircraft configuration design with tilting duct-fan propulsion system.

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    Titel :

    Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft

    Beteiligte:
    Chang, Min (Autor:in) / Zhou, Weixiang (Autor:in) / Peng, Bo (Autor:in) / Bai, Junqiang (Autor:in)
    Erschienen in:

    The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018) ; 2 ; 1222-1230

    Lecture Notes in Electrical Engineering ; 459 , 2

    Erscheinungsdatum :

    2019-01-01

    Format / Umfang :

    9 pages

    ISBN :

    978-981-13-3304-0 , 978-981-13-3305-7

    ISSN :

    1876-1100 , 1876-1119

    DOI :

    https://doi.org/10.1007/978-981-13-3305-7_96

    Medientyp :

    Aufsatz/Kapitel (Buch)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Schlagwörter :

    Vertical take-off and landing aircraft , Ducted propulsion system , Modeling method , Non-dimensional method , Momentum theory Engineering , Aerospace Technology and Astronautics , Fluid- and Aerodynamics , Theoretical and Applied Mechanics , Control and Systems Theory

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