Abstract
The paper describes a study of a distributed electric propulsion system impact on the aerodynamic performance of an aircraft wing. A semi-empirical method and CFD calculation method for prop blown wing influence on take-off and landing characteristic were considered and compared. Results of these methods are compared. Optimal location of a prop with leading edge of an airfoil in terms of maximize lift coefficient was obtained through the CFD method.
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CITATION STYLE
Vlasov, A. V., Varyukhin, A. N., Brailko, I. A., Lebedev, A. O., Zakharchenko, V. S., & Ovdienko, M. A. (2021). Modelling of aerodynamical interaction of the wing and propellers of a distributed propulsion system. In Journal of Physics: Conference Series (Vol. 1891). IOP Publishing Ltd. https://doi.org/10.1088/1742-6596/1891/1/012012
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