Email this article Thrust-Energy Characteristics of Plasma Actuators at Various Pressures
- Authors: Bocharnikov V.M.1, Trifanov I.V.1,2, Golub V.V.1
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Affiliations:
- Joint Institute for High Temperatures, Russian Academy of Sciences
- Moscow Institute of Physics and Technology (State University)
- Issue: Vol 45, No 1 (2019)
- Pages: 31-33
- Section: Article
- URL: https://bakhtiniada.ru/1063-7850/article/view/208185
- DOI: https://doi.org/10.1134/S1063785019010206
- ID: 208185
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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.
About the authors
V. M. Bocharnikov
Joint Institute for High Temperatures, Russian Academy of Sciences
Author for correspondence.
Email: vova.m.bocha@gmail.com
Russian Federation, Moscow, 127412
I. V. Trifanov
Joint Institute for High Temperatures, Russian Academy of Sciences; Moscow Institute of Physics and Technology (State University)
Email: vova.m.bocha@gmail.com
Russian Federation, Moscow, 127412; Dolgoprudnyi, Moscow oblast, 141700
V. V. Golub
Joint Institute for High Temperatures, Russian Academy of Sciences
Email: vova.m.bocha@gmail.com
Russian Federation, Moscow, 127412
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