Potential of Articulated Split Wingtips for Morphing-Based Control of a Flying Wing
Author:
Affiliation:
1. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4443
Reference25 articles.
1. The Wright Brothers: First Aeronautical Engineers and Test Pilots
2. Aerodynamic and Aeroelastic Characteristics of Wings with Conformal Control Surfaces for Morphing Aircraft
3. Flexible Composite Wing with Internal Actuation for Roll Maneuver
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