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

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 Navi...

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Bibliographic Details
Published in:Technical physics letters 2018-08, Vol.44 (8), p.687-690
Main Authors: Voevodin, A. V., Kornyakov, A. A., Petrov, D. A., Petrov, A. S., Sudakov, G. G.
Format: Article
Language:English
Subjects:
Actuators
Boundary layer
Boundary layer control
BOUNDARY LAYERS
Classical and Continuum Physics
Computational fluid dynamics
COMPUTERIZED SIMULATION
CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY
CONTROL SYSTEMS
Ejection
EQUATIONS
Gas jets
NAVIER-STOKES EQUATIONS
Physics
Physics and Astronomy
Reynolds averaged Navier-Stokes method
REYNOLDS NUMBER
SURFACES
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Summary: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.
ISSN:1063-7850
1090-6533
DOI:10.1134/S106378501808014X