Fluid–Structure Interactions and Unsteady Kinematics of a Low-Reynolds-Number Rotor
Author:
Affiliation:
1. ISAE-Supaero, University of Toulouse, 31055 Toulouse, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference33 articles.
1. Report No. 496, general theory of aerodynamic instability and the mechanism of flutter
2. GreenbergJ. M. “Airfoil in Sinusoidal Motion in Pulsating Stream,” NACA TN 1329, 1947.
3. Theoretical and experimental study of a piezoelectric flapping wing rotor for micro aerial vehicle
4. Aerodynamic Analysis of a Flapping Rotary Wing at a Low Reynolds Number
5. Aerodynamic Power Efficiency Comparison of Various Micro-Air-Vehicle Layouts in Hovering Flight
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