The role of effective angle of attack in hovering pitching-flapping-perturbed revolving wings at low Reynolds number
Author:
Affiliation:
1. College of Sciences, Northeastern University, Shenyang 110819, People’s Republic of China
2. School of Transportation Science and Engineering, Beihang University, Beijing 100191, People’s Republic of China
Funder
China Postdoctoral Science Foundation
National Natural Science Foundation of China
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/pdf/10.1063/1.5130959
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4. Design and stable flight of a 21 g insect-like tailless flapping wing micro air vehicle with angular rates feedback control
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