Open-Loop Flow-Control Investigation for Airfoils at Low Reynolds Numbers
Author:
Affiliation:
1. Department of Aerospace and Mechanical Engineering, University of Arizona, Tucson, Arizona 85721
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051860
Reference48 articles.
1. 1/5 Scale Model of Aeromot 200S SuperXimango for Scaled Flight Research
2. Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds Numbers
3. Laminar separation bubble characteristics on an airfoil at low Reynolds numbers
4. Aerodynamic performance and flow structure studies of a low Reynoldsnumber airfoil
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2. Effect of Airfoil Concavity on Wind Turbine Blade Performances;Shock and Vibration;2019-07-22
3. Control of low Reynolds number flow around an airfoil using periodic surface morphing: A numerical study;Journal of Fluids and Structures;2018-01
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