Parameters affecting dynamic stall control by oscillatory excitation
- 28 June 1999
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Some factors affecting stall control with particular emphasis on dynamic stallPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Sweep Effect on Parameters Governing Control of Separation by Periodic ExcitationJournal of Aircraft, 1998
- Effects of Periodic Excitation on Turbulent Flow Separation from a FlapAIAA Journal, 1998
- Suppression of dynamic-stall vortices over pitching airfoils by leading-edge suctionAIAA Journal, 1994
- The delay of turbulent boundary layer separation by oscillatory active controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- The delay of turbulent boundary layer separation by oscillatory active controlPhysics of Fluids A: Fluid Dynamics, 1989
- Toward dynamic separation without dynamic stallExperiments in Fluids, 1988
- Progress in analysis and prediction of dynamic stallJournal of Aircraft, 1988
- The effect of a leading-edge slat on the dynamic stall of an oscillating airfoilPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Unsteady AirfoilsAnnual Review of Fluid Mechanics, 1982