Investigation of Airfoil Boundary Layer and Wake Development at Low Reynolds Numbers
Author:
Affiliation:
1. University of Toronto
2. Ryerson University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2551
Reference15 articles.
1. Low-Reynolds-Number Airfoils
2. Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds Numbers
3. AERODYNAMICS OF SMALL VEHICLES
4. Effect of acoustic excitation on stalled flows over an airfoil
5. Effect of Acoustic Excitation on Airfoil Performance at Low Reynolds Numbers
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1. An experimental study of the turbulence quantities in the boundary layer and near-wake of an airfoil placed at upstream of a 90° bend;Experimental Thermal and Fluid Science;2010-11
2. Aerodynamics of a NACA4412 Airfoil in Ground Effect;AIAA Journal;2007-01
3. Coherent structures in an airfoil boundary layer and wake at low Reynolds numbers;Physics of Fluids;2006-04
4. Experiments on the Aerodynamics of a Cambered Airfoil in Ground Effect;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
5. Airfoil Performance at Low Reynolds Numbers in the Presence of Periodic Disturbances;Journal of Fluids Engineering;2005-10-10
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