Control of Actuation System Based Smart Material Actuators in a Morphing Wing Experimental Model
Author:
Affiliation:
1. University of Québec
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4918
Reference47 articles.
1. Active Control of Separation on a Wing with Oscillating Camber
2. 3Sobieczky, H., Geissler, W., and Hannemann, M. "Expansion shoulder bump for wing section viscous/wave drag control", FLOWCONIUTAMSymposiumon Mechanicsof Passiveand ActiveFlow Control,1998,Gottingen,Germany.
3. Active flow control based on transonic design concepts
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