Toward Understanding and Optimizing Separation Control Using Microjets
- 1 November 2009
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 47 (11), 2544-2557
- https://doi.org/10.2514/1.38868
Abstract
No abstract availableThis publication has 34 references indexed in Scilit:
- Design of the Blended Wing Body Subsonic TransportJournal of Aircraft, 2004
- Separation Control in Duct FlowsJournal of Aircraft, 2002
- The control of flow separation by periodic excitationProgress in Aerospace Sciences, 2000
- An experimental investigation of boundary layer ingestion in a diffusing S-duct with and without passive flow controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- 3D subsonic diffuser design and analysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Delay of airfoil stall by periodic excitationJournal of Aircraft, 1996
- Influence of inlet distortion on transonic compressor blade loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Separation Control: ReviewJournal of Fluids Engineering, 1991
- Effect of acoustic excitation on the flow over a low- Re airfoilJournal of Fluid Mechanics, 1987
- Control of turbulent boundary layer flows by soundPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983