Effects of vortex separation on the lift distribution on bodies of elliptic cross section
- 1 November 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 6 (6) , 537-543
- https://doi.org/10.2514/3.44102
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- REAL FLOW OVER A BODY OF REVOLUTION AT ANGLE OF ATTACKPublished by Defense Technical Information Center (DTIC) ,1963
- Theory of the vortex breakdown phenomenonJournal of Fluid Mechanics, 1962