Laminar Boundary-Layer Response to Spanwise Periodic Forcing by Dielectric-Barrier-Discharge Plasma-Actuator Arrays
Author:
Affiliation:
1. Institute for Aerospace Studies, University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053207
Reference51 articles.
1. High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator
2. Characterization of Surface Plasma-Induced Wall Flows Through Velocity and Temperature Measurements
3. Experimental damping of boundary-layer oscillations using DBD plasma actuators
4. Local stability effects of plasma actuation on a zero pressure gradient boundary layer
5. Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma
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