Active Control of Cylinder Flow With and Without a Splitter Plate Using Piezoelectric Actuators
Author:
Affiliation:
1. Tel -Aviv University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3070
Reference32 articles.
1. Longitudinal curvature effects in turbulent boundary layers
2. Effects of sound on separated flows
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