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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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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.

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Authors and Affiliations

  1. Central Aerodynamic Institute, Zhukovsky, Moscow oblast, 140180, Russia

    A. V. Voevodin, A. A. Kornyakov, D. A. Petrov, A. S. Petrov & G. G. Sudakov

Authors
  1. A. V. Voevodin
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  2. A. A. Kornyakov
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  3. D. A. Petrov
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  4. A. S. Petrov
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  5. G. G. Sudakov
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Corresponding author

Correspondence to D. A. Petrov.

Additional information

Original Russian Text © A.V. Voevodin, A.A. Kornyakov, D.A. Petrov, A.S. Petrov, G.G. Sudakov, 2018, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2018, Vol. 44, No. 15, pp. 71–79.

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Voevodin, A.V., Kornyakov, A.A., Petrov, D.A. et al. Improving the Lift Properties of a Wing in Takeoff and Landing by Means of a Boundary Layer Control System Using Ejector-Type Actuators. Tech. Phys. Lett. 44, 687–690 (2018). https://doi.org/10.1134/S106378501808014X

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  • DOI: https://doi.org/10.1134/S106378501808014X

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