Improving Aircraft Endurance Through Turbulent Separation Control by Pulsed Blowing
Author:
Affiliation:
1. University of Naples Federico II, 80125 Naples, Italy
2. Italian Center for Aerospace Research, 81043 Capua, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.33268
Reference14 articles.
1. Airfoils with boundary layer suction, design and off-design cases
2. Delay of airfoil stall by periodic excitation
3. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation
4. Tinapp, F., and Nitsche, W. "Separation Control on High Lift Configuration by Periodic Excitation," 12DGLR-Fach-Symposium der AG STAB,Noteson Numerical Fluid Mechanics, Vol.77, Springer-Verlag, Berlin,Nov. 2000, pp.42-49.
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