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

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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Bibliographic Details
Main Authors: Irina V. Mursenkova, Igor E. Ivanov, Yugan Liao, Igor A. Kryukov
Format: Article
Language:English
Published: MDPI AG 2022-03-01
Series:Energies
Subjects:
nanosecond surface sliding discharge
plasma actuator
supersonic flow
oblique shock wave
high-speed shadowgraphy
numerical simulation
Online Access:https://www.mdpi.com/1996-1073/15/6/2189

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https://www.mdpi.com/1996-1073/15/6/2189

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