Influence of propeller diameter mounted at wingtip of high aspect ratio wing on aerodynamic performance

In this paper, the propeller diameter effect on cruising characteristics of a solar-powered aircraft with a high aspect ratio wing is considered. Numerical studies were performed using a program based on the Reynolds-averaged Navier-Stokes equations for Mach numbers M=0.145 and Reynolds numbers Re =...

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Veröffentlicht in:	Journal of physics. Conference series 2021-07, Vol.1959 (1), p.12051
Hauptverfasser:	Vinogradov, O N, Kornushenko, A V, Pavlenko, O V, Petrov, A V, Pigusov, E A, Ngoc, Trinh Thang
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Aircraft configurations Aircraft performance Angle of attack Computational fluid dynamics Flow velocity Fluid flow High aspect ratio Numerical analysis Pressure distribution Propeller slipstreams Reynolds averaged Navier-Stokes method Reynolds number Slender wings Slipstreams Solar powered aircraft Stress concentration Velocity distribution Wing tips
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