Open AccessInfluence of propeller diameter mounted at wingtip of high aspect ratio wing on aerodynamic performance
Author(s) -
O. N. Vinogradov,
Aleksandr Vyacheslavovich Kornushenko,
Olga V. Pavlenko,
Albert Vasilievich Petrov,
E A Pigusov,
Trinh Thang Ngoc
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1959/1/012051
Subject(s) - propeller , advance ratio , wing , lift coefficient , aerodynamics , thrust , lift (data mining) , mach number , reynolds number , aerospace engineering , angle of attack , wing configuration , wing loading , wing twist , lift to drag ratio , wingtip vortices , aerodynamic force , airfoil , mechanics , marine engineering , engineering , physics , blade pitch , computer science , vortex , turbulence , horseshoe vortex , vorticity , turbine , data mining
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 = 0·3-10 6 . Three aircraft configurations were considered: without propellers, with running two-bladed propellers with diameters of 0.22 m and 0.33 m. Numerical studies showed that the installed propeller introduces significant non-linearity into the lift curves and propeller thrust coefficient versus angle of attack curves. The propeller slipstream velocity field changes depending on the propeller advance ratio and the flow velocity, thus influencing the pressure distribution on the wing and the aircraft aerodynamic performance.