A Numerical Optimization Study on Winglets
Author:
Affiliation:
1. University of Toronto
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2173
Reference33 articles.
1. DRAG DUE TO LIFT: Concepts for Prediction and Reduction
2. Theoretical considerations in the aerodynamic effectiveness of winglets
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