Aerodynamic Optimization and Analysis of Low Reynolds Number Propeller with Gurney Flap for Ultra-High-Altitude Unmanned Aerial Vehicle

Ultra-high-altitude unmanned aerial vehicles have created a high demand for the performance of propellers under low Reynolds numbers, while the efficiency of such propellers by the existing design framework has reached a bottleneck. This paper explores the possibility of extending the Gurney flap on...

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Principais autores:	Yuan Yao, Dongli Ma, Liang Zhang, Xiaopeng Yang, Yayun Yu
Formato:	Artigo
Idioma:	Inglês
Publicado em:	MDPI AG 2022-03-01
coleção:	Applied Sciences
Assuntos:	low Reynolds number propeller gurney flap aerodynamic optimization wind tunnel test ultra-high-altitude unmanned aerial vehicle
Acesso em linha:	https://www.mdpi.com/2076-3417/12/6/3195
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