Please use this identifier to cite or link to this item: https://doi.org/10.1016/j.proeng.2013.12.026
Title: Effects of AC Dielectric Barrier Discharge plasma actuator location on flow separation and airfoil performance
Authors: Bouremel, Y. 
Li, J.M. 
Zhao, Z.
Debiasi, M. 
Keywords: Dielectric barrier discharge plasma
Drag coefficient
Lift coefficient
Particle image velocimetry
Separation point
Vorticity
Issue Date: 2013
Source: Bouremel, Y., Li, J.M., Zhao, Z., Debiasi, M. (2013). Effects of AC Dielectric Barrier Discharge plasma actuator location on flow separation and airfoil performance. Procedia Engineering 67 : 270-278. ScholarBank@NUS Repository. https://doi.org/10.1016/j.proeng.2013.12.026
Abstract: The goal of this work is to characterize the effect of Dielectric Barrier Discharge (DBD) plasma actuator on the lift and drag coefficients generated by the flow around a NACA 4415 airfoil model using force-balance and Particle Image Velocimetry (PIV) measurements. DBD actuators are mounted at the leading edge, at 30% and 60% of the chord length. The effect of actuation on the airfoil lift and drag at these different locations are studied. It is found that for increasing angles of attack, the actuators need to be located closer to the leading edge and in front of the separation area to produce the best lift or drag coefficient improvements. If located within the flow separation zone, their effects on the airfoil lift and drag coefficients are limited. © 2013 The Authors. Published by Elsevier Ltd.
Source Title: Procedia Engineering
URI: http://scholarbank.nus.edu.sg/handle/10635/116067
ISSN: 18777058
DOI: 10.1016/j.proeng.2013.12.026
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