Aerodynamic Performance of a Notional Perching MAV Design
Author:
Affiliation:
1. U.S. Air Force Research Laboratory
2. University of Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-63
Reference13 articles.
1. Mechanization and Control Concepts for Biologically Inspired Micro Air Vehicles
2. Design and Optimization of a Biologically Inspired Flapping Mechanism for Flapping Wing Micro Air Vehicles
3. Longitudinal Dynamics of a Perching Aircraft
4. Optimization of Perching Maneuvers Through Vehicle Morphing
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4. Effect of Aspect Ratio and Leading and Trailing Edge Form on the Flow Around an Impulsively Pitching Flat Plate;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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