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Numerical studies of side slip effect on stability of airplane with propeller and the high aspect ratio wing
Pavlenko O.V.
1,2, Pigusov Е.А.1,2, Santhosh А.S.2, Trinh Thang Ngoc2
1Central Aerohydrodynamic Institute named after Prof.N.E.Zhukovsky, Zhukovsky, Russia
2Moscow Institute of Physics and Technology, Dolgoprudny, Moscow oblast, Russia
2Moscow Institute of Physics and Technology, Dolgoprudny, Moscow oblast, Russia
Email: olga.v.pavlenko@yandex.ru
The results of numerical studies of effect of the slip angle (crosswind) on the on stability of airplane with propeller and the high aspect ratio wing are presented. Increase the slip angle from 0 to 20o are change aerodynamic and moments characteristics of airplane due to the deterioration of the power plant and the asymmetric blowing by the pulling propellers. Numerical studies were carried out using the numerical code for the Reynolds-averaged Navier-Stokes equations. Keywords: pulling propeller, high aspect ratio wing, slip angle, moments characteristics, CFD methods.
- O.V. Pavlenko, E.A. Pigusov, A. Santosh, M.G. Reslan. Vestnik Moskovskogo aviatsionnogo in-ta, 30 (1), 23 (2023)
- O.N. Vinogradov, A.V. Kornushenko, O.V. Pavlenko, A.V. Petrov, E.A. Pigusov, Trinh Thang Ngoc. J. Physics: Conf. Series, ISCM 2021, IOP Publishing, 1959, 012051 (2021). DOI: 10.1088/1742-6596/1959/1/012051
- T.-H. Shih, W.W. Liou, A. Shabbir, J. Zhu. Computers Fluids, 24 (3), 227 (1995)
- O.V. Pavlenko, E.A. Pigusov, M.G. Reslan, A. Santosh. Pis'ma v ZhTF, 49 (24), 22 (2023).(in Russian)
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Дата начала обработки статистических данных - 27 января 2016 г.