Experimental Study of Drag-Reduction Devices on a Flatback Airfoil
Author:
Affiliation:
1. National Technical University of Athens, 157 80 Athens, Greece
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054901
Reference28 articles.
1. Experimental Analysis of Thick Blunt Trailing-Edge Wind Turbine Airfoils
2. BakerJ. P.Van DamC.GilbertB. L. “Flatback Airfoil Wind Tunnel Experiment,” Sandia National Lab. Rept. SAND2008-2008, Albuquerque, NM, 2008.
3. Base Drag and Thick Trailing Edges
4. A Method for Reducing the Base Drag of Wings with Blunt Trailing Edge
5. Control of Flow Over a Bluff Body
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