Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma

By J. Roth. 2003

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Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, background): “In Roth (2003), they propose a variety of electrode arrangements for DBDs in series, some of them producing normal wall jet when others promote flow acceleration in one or two directions.”
Active control of a Mach 0.9 jet for noise mitigation using plasma actuators (2007, background): “Note that the nature of a hightemperature, localized arc discharge is completely different from low-temperature, low-current, diffuse glow discharges used in previous low-speed flow control work [49,50].”
Experimental study of a DBD surface discharge for the active control of subsonic airflow (2008, result): “To the best of our knowledge, only Roth et al [8, 9] have recently performed measurements to estimate the power lost in the dielectric.”
Strategies for control of transitional and turbulent flows using plasma-based actuators (2006, background): “Experiments have shown the potential of DBD actuators for the control of boundary-layer separation on both external and internal flows (Corke et al. 2002, List et al. 2003, Post and Corke 2003, Roth 2003, Post and Corke 2004).”
Scaling Effects of an Aerodynamic Plasma Actuator (2007, background): “It is important to note that the SDBD plasmaactuator design has a self-limiting property and therefore is stable even at atmospheric pressures.”