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Feng, L.H., Jukes, T.N., Choi, K.-S. and Wang, J.J. (2012) Flow Control over a NACA 0012 Airfoil Using Dielectric- Barrier-Discharge Plasma Actuator with a Gurney Flap. Experiments in Fluids, 52, 1533-1546. http://dx.doi.org/10.1007/s00348-012-1263-y

has been cited by the following article:

• TITLE: Plasma Virtual Actuators for Flow Control

  AUTHORS: Kwing-So Choi, Timothy N. Jukes, Richard D. Whalley, Lihao Feng, Jinjun Wang, Takayuki Matsunuma, Takehiko Segawa

  KEYWORDS: Flow Control, DBD Plasma, Actuators, Aerodynamics, Drag Reduction, Turbulence

  JOURNAL NAME: Journal of Flow Control, Measurement & Visualization, Vol.3 No.1, January 15, 2015

  ABSTRACT: Dielectric-barrier-discharge (DBD) plasma actuators are all-electric devices with no moving parts. They are made of a simple construction, consisting only of a pair of electrodes sandwiching a dielectric sheet. When AC voltage is applied, air surrounding the upper electrode is ionized, which is attracted towards the charged dielectric surface to form a wall jet. Control of flow over land and air vehicles as well as rotational machinery can be carried out using this jet flow on demand. Here we review recent developments in plasma virtual actuators for flow control that can replace conventional actuators for better aerodynamic performance.