Sweep Effect on Parameters Governing Control of Separation by Periodic Excitation
- 1 May 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 35 (3) , 510-512
- https://doi.org/10.2514/2.2332
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Delay of airfoil stall by periodic excitationJournal of Aircraft, 1996
- Forcing level effects of internal acoustic excitation on the improvement of airfoil performanceJournal of Aircraft, 1992
- Flow structures behind a vertically oscillating fence immersed in a flat-plate turbulent boundary layerExperiments in Fluids, 1991
- Aerodynamic Characteristics of an Unsteady Separated FlowAIAA Journal, 1979