Augmentation of Vortex Lift by Spanwise Blowing
- 1 September 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (9), 727-732
- https://doi.org/10.2514/3.58703
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Leading-edge-vortex augmentation in compressible flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A Conceptual Study of Leading-Edge-Vortex Enhancement by BlowingJournal of Aircraft, 1974
- Lift and control augmentation by spanwise blowing over trailing edge flaps and control surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Lift augmentation by lateral blowing over a lifting surfacePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low SpeedsJournal of the Aeronautical Sciences, 1955