Unsteady flow phenomena over delta wings at high angle of attack
- 1 February 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (2) , 225-231
- https://doi.org/10.2514/3.11976
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- On the viscous modes of instability of a trailing line vortexJournal of Fluid Mechanics, 1991
- Vortex shedding over delta wingsAIAA Journal, 1990
- Vortex breakdown as a fundamental element of vortex dynamicsFluid Dynamics Research, 1988
- Vortex breakdown and its control on delta wingsFluid Dynamics Research, 1988
- Visualization and wake surveys of vortical flow over a delta wingAIAA Journal, 1988
- Experiments on vortex stabilityPhysics of Fluids, 1976
- The stability of a trailing line vortex. Part 1. Inviscid theoryJournal of Fluid Mechanics, 1974
- Vortex breakdown on slender sharp-edged wingsJournal of Aircraft, 1971
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968
- Observations of oscillatory motion in certain swirling flowsJournal of Fluid Mechanics, 1965