Transient structure of vortex breakdown on a delta wing
- 1 January 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (1) , 6-12
- https://doi.org/10.2514/3.12325
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- Onset of vortex breakdown above a pitching delta wingAIAA Journal, 1994
- Instantaneous structure of vortex breakdown on a delta wing via particle image velocimetryAIAA Journal, 1993
- Experimental study of vortex flows over delta wings in wing-rock motionJournal of Aircraft, 1992
- Axisymmetric vortex breakdown Part 2. Physical mechanismsJournal of Fluid Mechanics, 1990
- Leading-edge vortices due to low Reynolds number flow past a pitching delta wingAIAA Journal, 1990
- Vortex dynamics on a pitching delta wingJournal of Aircraft, 1990
- Vortex breakdown: Observations and explanationsProgress in Aerospace Sciences, 1988
- The Structure of Vortex BreakdownAnnual Review of Fluid Mechanics, 1978
- Vortex BreakdownAnnual Review of Fluid Mechanics, 1972
- On stationary and travelling vortex breakdownsJournal of Fluid Mechanics, 1971