Interaction of Synthetic Jet Propulsion with Wing Aerodynamics at Low Reynolds Numbers
Author:
Affiliation:
1. University of Bath
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-93
Reference21 articles.
1. Energy requirements for the flight of micro air vehicles
2. Charmichael, B. H. "Low Reynolds Number Airfoil Survey", NASA Contractor Report 165803, Volume I, 1981.
3. Aerodynamic lift at Reynolds numbers below 7 x 10 exp 4
4. Wind tunnel tests of wings at Reynolds numbers below 70 000
5. Aerodynamics and Propulsion of Synthetic Jet Based Micro Air Vehicles
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1. Analysis of Low Speed Flow over an Adaptive Airfoil with Oscillating Camber;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
2. Interaction of Synthetic Jet Propulsion with Airfoil Aerodynamics at Low Reynolds Numbers;AIAA Journal;2006-08
3. Characterization of Zero Mass Flux Flow Control for Separation Control of an Adaptive Airfoil;3rd AIAA Flow Control Conference;2006-06-05
4. Comparison Between Zero Mass Flux Flow Control Methods for Low Speed Airfoil Separation Control;35th AIAA Fluid Dynamics Conference and Exhibit;2005-06-06
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