Development of disturbances generated by an electric discharge in the shock wave / boundary layer interaction zone

The paper presents the results of experimental study of disturbances generated by an electric discharge. Observations are carried out in the zone of interaction of a shock wave and a boundary layer (the incident shock wave has the Mach number M = 1.43). Experiments were carried out in a supersonic w...

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Veröffentlicht in:	Thermophysics and aeromechanics 2023-07, Vol.30 (4), p.673-681
Hauptverfasser:	Vishnyakov, O. I., Polivanov, P. A., Sidorenko, A. A., Budovsky, A. D.
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary layer interaction Broadband Disturbances Electric discharges Flow velocity Fluid flow Hot wire method Mach number Physics Physics and Astronomy Reynolds number Shear layers Shock wave interaction Supersonic wind tunnels Thermodynamics
Online-Zugang:	Volltext
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