Aero-Propulsive Interactions between UAV Wing and Distributed Propellers Due to Their Relative Position

The purpose of this paper is the evaluation of the aero-propulsive effects on a UAV wing model with distributed propulsion. An array of three propellers is placed ahead of the leading edge of a rectangular wing with flap. The investigation was performed with high-fidelity numerical analyses to provi...

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Hlavní autoři: Danilo Ciliberti, Pierluigi Della Vecchia, Vincenzo Orticalco, Fabrizio Nicolosi
Médium: Článek
Jazyk:English
Vydáno: MDPI AG 2023-01-01
Edice:Drones
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On-line přístup:https://www.mdpi.com/2504-446X/7/1/49