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In this work, wind tunnel measurements and a CFD simulation of flow separation on the NACA 64-418 airfoil are presented. The comparison of the results allows a deeper insight into the physics of the occurring flow phenomena.
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This page is a summary of: Experimental and Numerical Investigation of Stall on the NACA 64(3) – 418 Airfoil, AIAA Journal, December 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061922.
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