Characterization of a Direct-Current Glow Discharge Plasma Actuator in Low-Pressure Supersonic Flow

An experimental study of a direct-current, nonequilibrium glow plasma discharge in the presence of a Mach 2.85 supersonic flow is presented. The discharge is generated with pinlike electrodes flush-mounted on a plane surface with sustaining currents between 25 to 300 mA. In the presence of a superso...

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Veröffentlicht in:	AIAA journal 2007-07, Vol.45 (7), p.1596-1605
Hauptverfasser:	Shin, Jichul, Narayanaswamy, V, Raja, Laxminarayan L, Clemens, Noel T
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Air flow Exact sciences and technology Experiments Flow control Fluid dynamics Fundamental areas of phenomenology (including applications) Instrumentation for fluid dynamics Physics Plasma Studies
Online-Zugang:	Volltext
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