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Thrust-Energy Characteristics of Plasma Actuators at Various Pressures

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Abstract

We have studied the pressure dependences of the long thrust and specific power thrust of synthetic jets generated by dielectric barrier discharge of a symmetric actuator at reduced pressures. Decreasing pressure leads to increase in the length of the plasma sheet. The thrust of synthetic jets reaches a maximum at a certain pressure dependent on the actuator geometry.

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Authors and Affiliations

  1. Joint Institute for High Temperatures, Russian Academy of Sciences, 127412, Moscow, Russia

    V. M. Bocharnikov, I. V. Trifanov & V. V. Golub

  2. Moscow Institute of Physics and Technology (State University), 141700, Dolgoprudnyi, Moscow oblast, Russia

    I. V. Trifanov

Authors
  1. V. M. Bocharnikov
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  2. I. V. Trifanov
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  3. V. V. Golub
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Corresponding author

Correspondence to V. M. Bocharnikov.

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Translated by P. Pozdeev

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Bocharnikov, V.M., Trifanov, I.V. & Golub, V.V. Thrust-Energy Characteristics of Plasma Actuators at Various Pressures. Tech. Phys. Lett. 45, 31–33 (2019). https://doi.org/10.1134/S1063785019010206

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  • DOI: https://doi.org/10.1134/S1063785019010206

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