Effect of Endplates on Two-Dimensional Airfoil Testing at Low Reynolds Number
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana 46556
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2872
Reference15 articles.
1. Low Reynolds number aerodynamics of low aspect-ratio wings
2. The Secondary Flow About Struts and Airfoils
3. An Investigation of Strut-Wall Intersection Losses
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