Wing design for minimum drag with practical constraints
- 1 November 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (11) , 879-886
- https://doi.org/10.2514/3.45058
Abstract
No abstract availableKeywords
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- Approximate solution of minimum induced drag of wings with given structural weightJournal of Aircraft, 1975