Modification of the Flow Structure over a UAV Wing for Roll Control
Author:
Affiliation:
1. University of Notre Dame
2. Orbital Research Inc
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-884
Reference13 articles.
1. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
2. Plasma Flaps and Plasma Slats: An Application of Weakly-Ionized Plasma Actuators
3. 4Moeller, E.B. And Rediniotis, O. K. "Hingeless Flow Control Over a Delta Wing Platform", AIAA Paper No. 2000-117.
4. Active Flow Control on the Stingray Uninhabited Air Vehicle: Transient Behaviour
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