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This article is cited in 5 scientific papers (total in 5 papers)
A multidischarge actuator system for power electrohydrodynamic action on the boundary layer of aerohydrodynamic surfaces
B. S. Aleshina, A. P. Kuryachiia, I. E. Rebrovb, V. Yu. Khomichb, S. L. Chernysheva, V. A. Yamshchikovb a Central Aerohydrodynamic Institute, Zhukovsky
b Institute of Problems of Electrophysics of the Russian Academy of Sciences, St. Petersburg
Abstract:
We present the results of a study of a new multidischarge actuator system designed for active gas flow control on the basis of a three-electrode circuit with a shielding electrode, in which the role of an accelerating electrode is played by the solid equipotential sheath surface of the wing. The main parameters of the multidischarge actuator system and classical scheme of electrodes are compared–namely, the induced air flow velocity, average integral volume force, average consumed power, and energy efficiency coefficient calculated per unit length of the external electrode.
Received: 11.08.2016
Citation:
B. S. Aleshin, A. P. Kuryachii, I. E. Rebrov, V. Yu. Khomich, S. L. Chernyshev, V. A. Yamshchikov, “A multidischarge actuator system for power electrohydrodynamic action on the boundary layer of aerohydrodynamic surfaces”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 43:1 (2017), 45–52; Tech. Phys. Lett., 43:1 (2017), 64–66
Linking options:
https://www.mathnet.ru/eng/pjtf6030 https://www.mathnet.ru/eng/pjtf/v43/i1/p45
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