Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma

By J. Roth, Daniel M. Sherman, Stephen Wilkinson. 2000

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Airflow control by non-thermal plasma actuators (2007, methodology): “Figure 14 shows the first three configurations tested by Roth et al and presented for the first time for airflow control in 1998 [29,30] at the AIAA conference and 25th ICOPS, and published in a journal in 2000 [68].”
Development and characterization of plasma actuators for high-speed jet control (2004, background): “Engineering applications of the plasmaassisted flow control mainly focus on viscous drag reduction and control of boundary layer separation in subsonic flows (Roth et al. 2000; Corke and Matlis 2000; Artana et al. 2001; Leonov et al. 2001; Post and Corke 2003), shock wave”
Diagnostics for characterisation of plasma actuators (2015, background): “Roth et al (1998–2000) [4, 33] Pitot tube 4.”
Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator (2008, background): “[3–5] and functions as a plasma actuator, is composed of two electrodes and a dielectric plate in between them; one of the electrodes is exposed to ambient gas and the other is encapsulated.”
High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “Early examples of plasma actuators as flow control devices demonstrated their potential for boundary layer and leading edge airfoil separation control applications (Roth et al. 2000; Post and Corke 2004).”