Biplane and Tail Effects in Flapping Flight
Author:
Affiliation:
1. Faculty of Aerospace Engineering, Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052007
Reference25 articles.
1. Flow Visualization and Force Measurements on a Hovering Flapping-Wing MAV 'DelFly II'
2. Titanium-alloy MEMS wing technology for a micro aerial vehicle application
3. Flapping Wing Aerodynamics: Progress and Challenges
4. Recent progress in flapping wing aerodynamics and aeroelasticity
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