Minimizing Induced Drag with Wing Twist, Computational-Fluid-Dynamics Validation
- 1 March 2006
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 43 (2) , 437-444
- https://doi.org/10.2514/1.15089
Abstract
No abstract availableKeywords
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