Lift efficient composite flexible wing for rolling manuever without ailerons
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
2. Ohio State Univ., Columbus
3. Dayton, Univ., OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1333
Reference16 articles.
1. Optimization of Flexible Wing Without Ailerons for Rolling Maneuver
2. Adaptive/conformal wing design for future aircraft
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2. Influence of anisotropic piezoelectric actuators on wing aerodynamic forces;Science in China Series E: Technological Sciences;2008-04-20
3. Improvement of Aircraft Rolling Power by Use of Piezoelectric Actuators;Chinese Journal of Aeronautics;2004-05
4. Morphing Inflatable Wing Development for Compact Package Unmanned Aerial Vehicles;45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;2004-04-19
5. Roll Maneuver Control of UCAV Wing Using Anisotropic Piezoelectric Actuators;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22
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