Aerodynamic Multi-Parameter Optimization of NACA0012 Airfoil Using Suction/Blowing Jet Technique
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/s13369-016-2259-3.pdf
Reference25 articles.
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3. Wild, J.: Mach-, Reynolds-and Sweep effects on active flow separation control effectivity on a 2-element airfoil wing. In: King, R. (ed.) Active Flow and Combustion Control 2014, pp. 87–100. Springer, Berlin (2015)
4. Seifert, A.; Pack, L.G.: Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions. AIAA paper 2000–2542 (2000)
5. Seifert, A.; Pack, L.G.: Active flow separation control on wall-mounted hump at high Reynolds numbers. AIAA J. 40(7), 1363–1372 (2002)
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