Excitation of Stationary Cross-Flow Instability Modes Using a Plasma Actuator Based on Dielectric Barrier Discharge

A. Ya. Kotvitsky; Котвицкий А. Я.; I. A. Moralev; Моралёв И. А.; M. V. Ustinov; Устинов М. В.; A. A. Abdullaev; Абдуллаев А. А.

doi:10.31857/S004036442306008X

Excitation of Stationary Cross-Flow Instability Modes Using a Plasma Actuator Based on Dielectric Barrier Discharge

Authors: Kotvitsky A.Y.¹, Moralev I.A.¹, Ustinov M.V.², Abdullaev A.A.³
Affiliations:
1. Joint Institute for High Temperatures, Russian Academy of Sciences
2. Central Aerohydrodynamic Institute
3. Moscow Institute of Physics and Technology
Issue: Vol 61, No 6 (2023)
Pages: 830-835
Section: Исследование плазмы
URL: https://modernonco.orscience.ru/0040-3644/article/view/653046
DOI: https://doi.org/10.31857/S004036442306008X
ID: 653046

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Abstract

The article presents the results of studying the stationary mode of cross-flow instability excited by a plasma actuator based on dielectric barrier discharge in a three-dimensional boundary layer on a swept plate with an induced pressure gradient. It is shown that the actuator generates an instability mode of a given wavelength with an initial amplitude of up to 2% of the free-stream velocity, while the signal-to-noise ratio is no greater than 15%. As a result of a parametric study, a family of growth curves of the excited instability mode was obtained as a function of the parameters of the voltage supplying the discharge. It is shown that the initial amplitude of stationary cross-flow vortices generated by the actuator in the studied range of parameters depends quadratically on the overvoltage at the electrodes and linearly on frequency, which coincides with a similar dependence for the actuator thrust.

References

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