Low Speed Design and Analysis of Wing/Winglet Combinations Including Viscous Effects
Author:
Affiliation:
1. University of California, Davis, Davis, California 95616
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.15349
Reference10 articles.
1. Aerodynamic design and analysis of winglets
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