Vortex breakdown control by delta wing geometry
- 1 July 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 32 (4) , 832-838
- https://doi.org/10.2514/3.46798
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Symmetry breaking in vortex flows on conical bodiesAIAA Journal, 1992
- Effect of tunnel walls on vortex breakdown location over delta wingsAIAA Journal, 1992
- Visualization measurements of vortex flowsJournal of Aircraft, 1991
- Water-Tunnel Studies of Leading-Edge VorticesJournal of Aircraft, 1982
- Vortex breakdown on slender sharp-edged wingsJournal of Aircraft, 1971
- Some Experiments with Vortex BreakdownJournal of the Royal Aeronautical Society, 1964