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Computational prediction of airfoil dynamic stall PDF

89 Pages·1997·4.68 MB·English
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Preview Computational prediction of airfoil dynamic stall

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Abstract—The term dynamic stall refers to unsteady flow separation occurring on aerodynamic bodies, such as . Dynamic stall events on a NACA-0012 airfoil at low free-stream Mach number [from Ref. (10)] and Reding or to use Theodorsen's flat plate theory, as applied by Tyler and Leish- man.
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