Sweep Effect on Parameters Governing Control of Separation by Periodic Excitation
Author:
Affiliation:
1. Tel-Aviv University, Ramat-Aviv 69978, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2332
Reference5 articles.
1. Forcing level effects of internal acoustic excitation on the improvement of airfoil performance
2. Aerodynamic Characteristics of an Unsteady Separated Flow
3. Flow structures behind a vertically oscillating fence immersed in a flat-plate turbulent boundary layer
4. Delay of airfoil stall by periodic excitation
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