Effect of a constant magnetic field on a supersonic flow near a submillimeter pulsed electric discharge

Results of an experimental study of the evolution of a vortex flow formed under the action of a submillimeter arc discharge moving in a constant magnetic field in a supersonic air flow near a flat surface are presented. Owing to the high reproducibility of the discharge parameters and precise synchronization of the equipment, it is possible to study the flow structure in much detail by the methods of particle image velocimetry and Schlieren visualization. It is found that the spatial and temporal characteristics of the generated vortex structures can be effectively controlled by changing the direction of the electromagnetic force arising during the discharge.

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Publication Details

Journal
Thermophysics and Aeromechanics
Published
2026-02-13
DOI
https://doi.org/10.1134/s0869864325020143
Primary Topic
Plasma and Flow Control in Aerodynamics
Type
article
Field-Weighted Citation Impact
0.00
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article

Effect of a constant magnetic field on a supersonic flow near a submillimeter pulsed electric discharge

Yu. V. Gromyko, O. I. Vishnyakov, M. A. Yadrenkin
Thermophysics and Aeromechanics
Plasma and Flow Control in Aerodynamics
article

Effect of a constant magnetic field on a supersonic flow near a submillimeter pulsed electric discharge

Yu. V. Gromyko, O. I. Vishnyakov, M. A. Yadrenkin
article en

Abstract

Results of an experimental study of the evolution of a vortex flow formed under the action of a submillimeter arc discharge moving in a constant magnetic field in a supersonic air flow near a flat surface are presented. Owing to the high reproducibility of the discharge parameters and precise synchronization of the equipment, it is possible to study the flow structure in much detail by the methods of particle image velocimetry and Schlieren visualization. It is found that the spatial and temporal characteristics of the generated vortex structures can be effectively controlled by changing the direction of the electromagnetic force arising during the discharge.

Thermophysics and AeromechanicsVol. 32(2)
Institute of Theoretical and Applied Mechanics (RU)
Openalex Percentile: Top 58%
Plasma and Flow Control in Aerodynamics
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