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This article is cited in 1 scientific paper (total in 1 paper)
Thrust-energy characteristics of plasma actuators at various pressures
V. M. Bocharnikova, I. V. Trifanovab, V. V. Goluba a Joint Institute for High Temperatures, Russian Academy of Sciences, Moscow
b Moscow Institute of Physics and Technology (State University), Dolgoprudny, Moscow region
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.
Received: 15.10.2018
Citation:
V. M. Bocharnikov, I. V. Trifanov, V. V. Golub, “Thrust-energy characteristics of plasma actuators at various pressures”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 45:2 (2019), 33–35; Tech. Phys. Lett., 45:1 (2019), 31–33
Linking options:
https://www.mathnet.ru/eng/pjtf5565 https://www.mathnet.ru/eng/pjtf/v45/i2/p33
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Abstract page: | 59 | Full-text PDF : | 11 |
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