Improving the Lift Properties of a Wing in Takeoff and Landing by Means of a Boundary Layer Control System Using Ejector-Type Actuators


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A device making it possible to control of the flow past a wing at low flight speeds is proposed. The device comprises an ejector-type actuator that simultaneous sucks the boundary layer on the upper surface and blows a gas jet in the vicinity of the trailing edge. Based on the Reynolds-averaged Navier–Stokes equations, a mathematical model of an ejector-type actuator is developed and experimental studies are carried out.

作者简介

A. Voevodin

Central Aerodynamic Institute

Email: daniel.petrov@tsagi.ru
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180

A. Kornyakov

Central Aerodynamic Institute

Email: daniel.petrov@tsagi.ru
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180

D. Petrov

Central Aerodynamic Institute

编辑信件的主要联系方式.
Email: daniel.petrov@tsagi.ru
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180

A. Petrov

Central Aerodynamic Institute

Email: daniel.petrov@tsagi.ru
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180

G. Sudakov

Central Aerodynamic Institute

Email: daniel.petrov@tsagi.ru
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180

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