Aircraft aerodynamics in a disturbed atmosphere
Автор: Vyshinsky V.V., Zoan K.T.
Журнал: Труды Московского физико-технического института @trudy-mipt
Рубрика: Механика
Статья в выпуске: 2 (50) т.13, 2021 года.
Бесплатный доступ
An engineering method is proposed for assessing the aerodynamic effect of a disturbed atmosphere on an aircraft. As a source of vortex structures, vortex wind wakes arising when the atmospheric boundary layer flows around the landscape or superstructures of a moving aircraft carrier, vortex wakes behind aircraft, etc. can be considered. The article deals with the situation of a light transport aircraft getting into a vortex wake behind an aircraft Su-27.
Coherent vortex structures in the atmosphere, flight safety, boundary-value problems, reynolds-averaged navier-stokes equations, subsonic vortex flows, boundary element method, discrete vortex method, panel methods
Короткий адрес: https://sciup.org/142231003
IDR: 142231003 | DOI: 10.53815/20726759_2021_13_2_40
