Unsteady, separated flow behind an oscillating, two-dimensional spoiler
- 1 May 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (5) , 845-852
- https://doi.org/10.2514/3.25128
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Analysis and control of unsteady separated flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- An LDA Study of the Backward-Facing Step Flow, Including the Effects of Velocity BiasJournal of Fluids Engineering, 1988
- Investigation of unsteady subsonic spoiler and flap aerodynamicsJournal of Aircraft, 1987
- Unsteady separated flows driven by periodic leading edge deformationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Forced unsteady vortex flows driven by pitching airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Control of Separated Flows Using Forced UnsteadinessPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Control of unsteady separated flow structures on airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Aerodynamic characteristics of a two-dimensional moving spoiler in subsonic and transonic flowJournal of Aircraft, 1984
- Forced vortices near a wallPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Aerodynamic Characteristics of an Unsteady Separated FlowAIAA Journal, 1979