Circulation Control as a Roll Effector for Unmanned Combat Aerial Vehicles
Author:
Affiliation:
1. University of Liverpool, Liverpool, England L69 3GH, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033642
Reference30 articles.
1. Circulation Control for High Lift and Drag Generation on STOL Aircraft
2. Design of the Circulation Control Wing STOL Demonstrator Aircraft
3. Flight Performance of a Circulation Controlled STOL Aircraft
4. Circulation controlled STOL wing optimization
5. A Wind Tunnel Model to Explore Unsteady Circulation Control for General Aviation Applications
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