Predictions of the effect of wing camber and thickness on airfoil self-noise
20th AIAA/CEAS Aeroacoustics Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Airfoil Thickness, Camber and Reynolds Number on Plunging Airfoil Propulsion
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|Thickness and camber effects in slender wing theory
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