Leading-Edge-Vortex Augmentation in Compressible Flow
- 1 April 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (4) , 238-242
- https://doi.org/10.2514/3.58652
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Conceptual Study of Leading-Edge-Vortex Enhancement by BlowingJournal of Aircraft, 1974
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971