Mechanisms and Responses of a Dielectric Barrier Plasma Actuator: Geometric Effects
By C. Enloe, Thomas McLaughlin, R. Vandyken, K. Kachner, E. Jumper, Thomas C. Corke, Martiqua L. Post, O. Haddad. 2004
573 citations recorded by the source corpus.
View Paper: https://www.semanticscholar.org/paper/62aba3b66d3b6ec158f8ed8a456af38705cf2a8b
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Citations in the corpus
- High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “This appears consistent with modeling results that show the highest force density associated with such devices is near the edge of the exposed electrode (Enloe et al. 2004b; Corke et al. 2007).”
- Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator (2008, background): “8; that is, the thrust increases with the electric power consumption linearly, as previously reported [28].”
- Development and use of localized arc filament plasma actuators for high-speed flow control (2007, background): “Although EHD plasma actuators can be quite energy efficient (with actuator power budget of a few tens of Watts [11]), further ion density increase in the glow discharge plasma is severely limited by ionization instability development.”
- Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, methodology): “8 shows the electrical power consumption versus applied voltage for two different frequencies with a thin dielectric (Enloe et al. 2004a).”