Experimental Small-Amplitude Self-Sustained Pitch–Heave Oscillations at Transitional Reynolds Numbers
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Royal Military College of Canada, Kingston, Ontario K7K 7B4, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052541
Reference21 articles.
1. MuellerT. J. “Low Reynolds Number Vehicles,” AGARD AG-288, 1985.
2. Control of low-speed airfoil aerodynamics
3. Vortex shedding and shear-layer instability of wing at low-Reynolds numbers
4. Progress in Astronautics and Aeronautics;Lutz T. H.,2001
5. Influence of surface flow on aerodynamic loads of a cantilever wing
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