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.
Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft
The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018) ; 2 ; 1222-1230
Lecture Notes in Electrical Engineering ; 459 , 2
2019-01-01
9 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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