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Development of the method of an electrohydrodynamic force effect on a boundary layer for active control of aerodynamic flows

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Abstract

The results of investigations on the possibility of an electrohydrodynamic force effect on a gas flow implemented with the help of a barrier discharge are presented. A new method of controlling the laminar flow around a base with suppression of instabilities of the incoming flow due to electrohydrodynamic force action on the boundary layer near the forward edge of a swept wing is proposed. An efficient multidischarge actuator system is developed and created for active control of aerodynamic flows with induced-air-flow characteristics exceeding the world analogues.

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Authors and Affiliations

  1. National Research Centre “Institute named after Zhukovskii,”, Zhukovskii, Moscow oblast, Russia

    B. S. Aleshin

  2. Institute of Electrophysics and Electroenergetics, Russian Academy of Sciences, St. Petersburg, 191186, Russia

    V. Yu. Khomich

  3. Central Aerohydrodynamic Institute, Zhukovskii, Moscow region, 140160, Russia

    S. L. Chernyshev

Authors
  1. B. S. Aleshin
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  2. V. Yu. Khomich
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  3. S. L. Chernyshev
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Corresponding author

Correspondence to V. Yu. Khomich.

Additional information

Original Russian Text © B.S. Aleshin, V.Yu. Khomich, S.L. Chernyshev, 2016, published in Doklady Akademii Nauk, 2016, Vol. 471, No. 6, pp. 662–664.

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Aleshin, B.S., Khomich, V.Y. & Chernyshev, S.L. Development of the method of an electrohydrodynamic force effect on a boundary layer for active control of aerodynamic flows. Dokl. Phys. 61, 601–603 (2016). https://doi.org/10.1134/S1028335816120107

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  • DOI: https://doi.org/10.1134/S1028335816120107

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