Flow Structures Around a Flapping-Wing Micro Air Vehicle Performing a Clap-and-Peel Motion
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055146
Reference42 articles.
1. CarmichaelB. “Low Reynolds Number Airfoil Survey,” NASA TR NASA-CR-165803-VOL-1, 1981.
2. Design, Analysis and Hover Performance of a Rotary Wing Micro Air Vehicle
3. Challenges Facing Future Micro-Air-Vehicle Development
4. Hover Performance of a Micro Air Vehicle: Rotors at Low Reynolds Number
5. Small Rotor Design Optimization Using Blade Element Momentum Theory and Hover Tests
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