Please use this identifier to cite or link to this item:
|Title:||Effects of AC Dielectric Barrier Discharge plasma actuator location on flow separation and airfoil performance||Authors:||Bouremel, Y.
|Keywords:||Dielectric barrier discharge plasma
Particle image velocimetry
|Issue Date:||2013||Citation:||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|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Oct 16, 2020
WEB OF SCIENCETM
checked on Oct 9, 2020
checked on Oct 10, 2020
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.