Title: Подъёмная сила аэродинамического профиля с интерцептором
Other Titles: Lift of the airfoil with spoiler
Authors: Редькина, К.В.
Фролов, В.А.
Issue Date: 2012
Publisher: СГАУ
Citation: Редькина, К. В. Подъёмная сила аэродинамического профиля с интерцептором = Lift of the airfoil with spoiler / К. В. Редькина, В. А. Фролов // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 333-334.
Abstract: A model of a stationary vortex for the potential circulation flow around airfoil-spoiler combination has been proposed. The solution is obtained for the flow of incompressible ideal fluid. The Complex Variable Function Theory is applied. For the simulation of the recirculation area, a stationary vortex is used, the location of which is found by minimizing a velocity function. Dependence of the lift on the angle of attack, relative length of the spoiler and its angle of deflection is obtained.
URI: http://repo.ssau.ru/jspui/handle/123456789/20411
Appears in Collections:Самолетостроение России. Проблемы и перспективы

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