Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (4), 193-199
- https://doi.org/10.2514/3.44254
Abstract
No abstract availableKeywords
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- Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low SpeedsJournal of the Aeronautical Sciences, 1955
- The lift of a delta wing at supersonic speedsQuarterly of Applied Mathematics, 1946