Subsonic Vortex-Flow Design Study for Slender Wings
- 1 September 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (9) , 611-617
- https://doi.org/10.2514/3.58415
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Load distributions on slender delta wings having vortex flowJournal of Aircraft, 1977
- A three-dimensional solution of flows over wings with leading-edge vortex separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975