Connection between leading-edge sweep, vortex lift, and vortex strength for delta wings
- 1 May 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 27 (5) , 473-475
- https://doi.org/10.2514/3.25305
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Similarity for high-angle-of-attack subsonic/transonic slender-body aerodynamicsJournal of Aircraft, 1989
- Three-dimensional hypersonic gas flow past slender bodies at high angles of attackJournal of Applied Mathematics and Mechanics, 1960