Experimental and Numerical Studies on Aerodynamic Control of NACA 4418 Airfoil with a Rotating Cylinder
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Link
http://link.springer.com/article/10.1007/s42417-019-00085-5/fulltext.html
Reference22 articles.
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2. Al-Garni AZ, Al-Garni AM, Ahmed SA, Sahin AZ (2000) Flow control for an airfoil with leading-edge rotation: an experimental study. J Aircr 37:617–622. https://doi.org/10.2514/2.2673
3. Amitay M, Smith DR, Kibens V, Parekh DE, Glezer A (2001) Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators. AIAA J 39:361–370. https://doi.org/10.2514/2.1323
4. Badr H, Dennis S, Young P (1989) Steady and unsteady flow past a rotating circular cylinder at low Reynolds numbers. Comput Fluids 17:579–609. https://doi.org/10.1016/0045-7930(89)90030-3
5. Brooks JD (1963) The effect of a rotating cylinder at the leading and trailing edges of a hydrofoil. Naval Ordnance Test Station, China Lake
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