Active Flow Separation Control on a NACA 0015 Wing using Fluidic Actuators
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2364
Reference21 articles.
1. Active Flow Separation Control on Wall-Mounted Hump at High Reynolds Numbers
2. Oscillatory Control of Separation at High Reynolds Numbers
3. The control of flow separation by periodic excitation
4. Influence of Finite Span and Sweep on Active Flow Control Efficacy
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