Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-1188
Reference25 articles.
1. Spanwise variations in profile drag for airfoils at low Reynolds numbers
2. Correlation of Theory to Wind-Tunnel Data at Reynolds Numbers below 500,000
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