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This article is cited in 4 scientific papers (total in 4 papers)
Improving the lift properties of a wing in takeoff and landing by means of a boundary layer control system using ejector-type actuators
A. V. Voevodin, A. A. Kornyakov, D. A. Petrov, A. S. Petrov, G. G. Sudakov Central Aerohydrodynamic Institute
Abstract:
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.
Received: 11.12.2017 Revised: 16.04.2018
Citation:
A. V. Voevodin, A. A. Kornyakov, D. A. Petrov, A. S. Petrov, G. G. Sudakov, “Improving the lift properties of a wing in takeoff and landing by means of a boundary layer control system using ejector-type actuators”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 44:15 (2018), 71–79; Tech. Phys. Lett., 44:8 (2018), 687–690
Linking options:
https://www.mathnet.ru/eng/pjtf5738 https://www.mathnet.ru/eng/pjtf/v44/i15/p71
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Abstract page: | 32 | Full-text PDF : | 6 |
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