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Uspekhi Fizicheskikh Nauk, 2017, Volume 187, Number 6, Pages 653–666 (Mi ufn5771)  

This article is cited in 9 scientific papers (total in 9 papers)

FROM THE CURRENT LITERATURE

Electrohydrodynamic flow for the active control of gas flows

V. Yu. Khomich, V. A. Yamshchikov

Institute of Problems of Electrophysics, Russian Academy of Sciences, St. Petersburg
Full-text PDF (392 kB) Citations (9)
Abstract: A new approach to producing powerful electrohydrodynamic flows in a gas environment is discussed, in which a barrier discharge distributed over a dielectric surface is used as an intense ion source. Electric discharge systems for active control of gas flows with a high (>15 l s1) volumetric rate are developed and investigated. A highly effective multidischarge actuator system is created to control air flows over aerodynamic surfaces with a significantly higher actuator force and energy characteristics than those in known global analogs.
Keywords: electrohydrodynamic flow, ion beam, barrier discharge, multidischarge actuator.
Received: August 9, 2016
Revised: December 8, 2016
Accepted: January 17, 2017
English version:
Physics–Uspekhi, 2017, Volume 60, Issue 6, Pages 608–620
DOI: https://doi.org/10.3367/UFNe.2017.01.038047
Bibliographic databases:
Document Type: Article
PACS: 52.90.+z
Language: Russian
Citation: V. Yu. Khomich, V. A. Yamshchikov, “Electrohydrodynamic flow for the active control of gas flows”, UFN, 187:6 (2017), 653–666; Phys. Usp., 60:6 (2017), 608–620
Citation in format AMSBIB
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Linking options:
  • https://www.mathnet.ru/eng/ufn5771
  • https://www.mathnet.ru/eng/ufn/v187/i6/p653
  • This publication is cited in the following 9 articles:
    1. Vladislav Yu. Khomich, Vladimir A. Yamshchikov, “Effect of power supply modes of multi-discharge actuator systems on their electric discharge and gas-dynamic characteristics”, Acta Astronautica, 215 (2024), 135  crossref
    2. B. S. Aleshin, V. Yu. Khomich, S. L. Chernyshev, “Development Trends in Plasma Aerodynamics”, Dokl. Phys., 68:1 (2023), 1  crossref
    3. Omar Kahol, Marco Belan, Mattia Pacchiani, Domenico Montenero, “Scaling relations for the geometry of wire-to-airfoil atmospheric ionic thrusters”, Journal of Electrostatics, 123 (2023), 103815  crossref
    4. S. A. Baranov, S. L. Chernyshev, V. Yu. Khomich, A. Ph. Kiselev, A. P. Kuryachii, S. I. Moshkunov, I. E. Rebrov, D. S. Sboev, S. N. Tolkachev, V. A. Yamshchikov, “Experimental cross-flow control in a 3D boundary layer by multi-discharge plasma actuators”, Aerosp. Sci. Technol., 112 (2021), 106643  crossref  isi
    5. V. Yu. Khomich, V. A. Yamshchikov, S. L. Chernyshev, A. P. Kuryachii, “Multi-discharge actuator systems for electrogasdynamic flow control”, Acta Astronaut., 181 (2021), 292–300  crossref  isi
    6. Shaygani A., Adamiak K., 2020 IEEE Industry Applications Society Annual Meeting, IEEE Industry Applications Society Annual Meeting, IEEE, 2020  crossref  isi
    7. H. Xu, Y. He, S. R. H. Barrett, “A dielectric barrier discharge ion source increases thrust and efficiency of electroaerodynamic propulsion”, Appl. Phys. Lett., 114:25 (2019), 254105  crossref  isi
    8. S. V. Nebogatkin, I. E. Rebrov, V. Yu. Khomich, V. A. Yamshchikov, “Optimization of a multidischarge actuator system”, Plasma Phys. Rep., 45:4 (2019), 410–413  crossref  isi
    9. V. Yu. Khomich, I. E. Rebrov, “In-atmosphere electrohydrodynamic propulsion aircraft with wireless supply onboard”, J. Electrost., 95 (2018), 1–12  crossref  isi  scopus
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
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