High-Performance Wings with Significant Leading Edge Thrust at Supersonic Speeds
- 1 June 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (6) , 419-422
- https://doi.org/10.2514/3.57919
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Numerical method of estimating and optimizing supersonic aerodynamic characteristics of arbitrary planform wingsJournal of Aircraft, 1965