ELIMINATION OF THE CROSS-FLOW INSTABILITY ON THE SWEPT WING BOUNDARY LAYER BY MEANS OF DIELECTRIC BARRIER DISCHARGE

Maxim Vladimirovich  Ustinov

doi:10.1615/TsAGISciJ.2016016392

TsAGI Science Journal

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Mitherausgeber: Ivan Vladimirovich Egorov (open in a new tab)

International Executive Editorial Advisors: M. de Gliniasty (open in a new tab) C.W. Kauffman (open in a new tab) Jurgen Quest (open in a new tab) Gu Songfen (open in a new tab) Shinji Suzuki (open in a new tab)

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ISSN Druckformat: 1948-2590

ISSN Online: 1948-2604

ELIMINATION OF THE CROSS-FLOW INSTABILITY ON THE SWEPT WING BOUNDARY LAYER BY MEANS OF DIELECTRIC BARRIER DISCHARGE

Volumen 46, Ausgabe 8, 2015, pp. 715-732

DOI: 10.1615/TsAGISciJ.2016016392

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Maxim Vladimirovich Ustinov
Central Aerohydrodynamic Institute (TsAGI), Zhukovsky str. 1, Zhukovsky, 140180, Russia

ABSTRAKT

Control of the laminar-turbulent transition caused by the cross-flow instability of the boundary layer on a swept wing by means of a dielectric barrier discharge is investigated. The practically important case of discharge on a large number of closely located electrodes is considered. The distance between the electrodes is assumed to be comparable with the boundary layer thickness. Unlike previous studies based on the solution to boundary layer equations, Navier-Stokes equations are applied to describe the discharge effect on the flow.

SCHLÜSSELWÖRTER: laminar-turbulent transition, swept wing, dielectric barrier discharge

REFERENZIERT VON

Baranov Sergey A., Chernyshev Sergey L., Khomich Vladislav Yu., Kiselev Andrey Ph., Kuryachii Aleksandr P., Moshkunov Sergey I., Rebrov Igor E., Sboev Dmitry S., Tolkachev Stepan N., Yamshchikov Vladimir A., Experimental cross-flow control in a 3D boundary layer by multi-discharge plasma actuators, Aerospace Science and Technology, 112, 2021. Crossref
Baranov S. A., Kiselev A. F., Kuryachii A. P., Sboev D. S., Tolkachev S. N., Chernyshev S. L., Control of Cross-Flow in a Three-Dimensional Boundary Layer Using a Multidischarge Actuator System, Fluid Dynamics, 56, 1, 2021. Crossref

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