Load distributions on slender delta wings having vortex flow
- 1 July 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (7) , 699-702
- https://doi.org/10.2514/3.44616
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A three-dimensional solution of flows over wings with leading-edge vortex separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- A theory of the flow past a slender delta wing with leading edge separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959
- Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low SpeedsJournal of the Aeronautical Sciences, 1955