Closed-Loop Stall Control on a Morphing Airfoil Using Hot-Film Sensors and DBD Actuators
Author:
Affiliation:
1. U.S. Air Force Research Laboratory
2. The Boeing Company
3. FlexSys Inc
4. Tao of Systems Integration
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-547
Reference31 articles.
1. Quest for Efficient Transonic Cruise
2. Flight Testing of Mission Adaptive Compliant Wing
3. Unsteady Aerodynamic Observable for Gust Load Alleviation and Flutter Suppression
4. Ground/Flight Correlation of Aerodynamic Loads with Structural Response
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