Control of Flow Separation and Transition Point over an Aerofoil at Low Re Number using Simultaneous Blowing and Suction
Author:
Affiliation:
1. University of Erciyes
2. TOBB University of Economics and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3672
Reference36 articles.
1. Low-Reynolds-number airfoil design for the M.I.T. Daedalus prototype- A case study
2. Numerical Study of Blowing and Suction Control Mechanism on NACA0012 Airfoil
3. Huang L., 2004, "Optimization of Blowing and Suction Control on NACA0012 Aerofoil Using Genetic AlgorithmwithDiversityControl", PhD. Thesis,UniversityofKentucky,Lexington,Kentucky,USA.
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