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Jukes, T., Segawa, T. and Furutani, H. (2012) Active Flow Separation Control on a NACA 4418 Using DBD Vortex Generators and FBG Sensors. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2012-1139.

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.