Experimental and Numerical Investigation of a Surface Sliding Discharge in a Supersonic Flow with an Oblique Shock Wave

This study presents an experimental and numerical investigation on a surface sliding discharge in a supersonic airflow in the presence of an oblique shock wave. In experiments, flow Mach numbers were 1.20–1.68 in the shock tube combined with the discharge chamber. A single high-voltage 25 kV pulse s...

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Hauptverfasser:	Irina V. Mursenkova, Igor E. Ivanov, Yugan Liao, Igor A. Kryukov
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	MDPI AG 2022-03-01
Schriftenreihe:	Energies
Schlagworte:	nanosecond surface sliding discharge plasma actuator supersonic flow oblique shock wave high-speed shadowgraphy numerical simulation
Online-Zugang:	https://www.mdpi.com/1996-1073/15/6/2189
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