Effect of leading-edge vortex flaps on aerodynamic performance of delta wings
- 1 September 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (9) , 796-798
- https://doi.org/10.2514/3.44734
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Analytical investigation of aerodynamic characteristics of highly swept wings with separated flowJournal of Aircraft, 1980
- Assessment of airframe noiseJournal of Aircraft, 1979