Unsteady aerodynamics of a pitching-flapping-perturbed revolving wing at low Reynolds number
Author:
Affiliation:
1. School of Transportation Science and Engineering, Beihang University, Beijing 100191, China
2. Department of Mechanical and Nuclear Engineering, Pennsylvania State University, University Park, Pennsylvania 16801, USA
Funder
National Science Foundation
National Natural Science Foundation of China
Army Research Office
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/am-pdf/10.1063/1.5024925
Reference42 articles.
1. Challenges Facing Future Micro-Air-Vehicle Development
2. Flying like a fly
3. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
4. Aerodynamics of Low Reynolds Number Flyers
5. Aerodynamic Power Efficiency Comparison of Various Micro-Air-Vehicle Layouts in Hovering Flight
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