Delta Wing Flow Control Using Dielectric Barrier Discharge Actuators
Author:
Affiliation:
1. Technical University of Berlin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4277
Reference17 articles.
1. Delta Wing Stall and Roll Control Using Segmented Piezoelectric Fluidic Actuators
2. Guy Y., Morrow J. A. and McLaughlin T.E "Velocity measurements on a delta wing with periodic blowing and suction", AIAA paper 2000-0550.
3. Siegel S. G., Mclaughlin T. E. and Morrow J. A. "PIV Measurements on a Delta Wing with Periodic Blowing and Suction", AIAA paper 2001-2436.
4. Siegel S. G., Mclaughlin T. E. and Albertson J. A. "Partial Leading Edge Forcing of a Delta Wing At High Angles of Attack", AIAA paper 2002-3268.
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1. Aerodynamic performance enhancement of a flying wing using nanosecond pulsed DBD plasma actuator;Chinese Journal of Aeronautics;2015-04
2. Gurney Flaps on Slender and Nonslender Delta Wings;Journal of Aircraft;2010-03
3. Airflow Reattachment Along a NACA 0015 Airfoil by Surfaces Dielectric Barrier Discharge Actuator: Time-Resolved Particle Image Velocimetry Investigation;4th Flow Control Conference;2008-06-15
4. Delta-Wing Flow Control Using Dielectric Barrier Discharge Actuators;AIAA Journal;2008-06
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