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- W2212384698 abstract "The unsteady behaviour of aerofoils has application to fixed wing aircraft encountering gusts or wind sheer, super-manoeuvrable aircraft with articulated wings, helicopters and wind turbines as well as the marine use of hydrofoils. The aerodynamic characteristics of an unsteady aerofoil deviates substantially from the steady flow case. Many such devices will have aerofoils working at relative velocities low enough to introduce a Reynolds Number dependence. Aerofoils typically undergo a rapid degradation in performance at Reynolds numbers below approximately 1x10{6}. The paper introduces the experimental facility now running at the University of Melbourne designed to study the effect of Reynolds Number on an aerofoil in the unsteady condition. The apparatus described allows full flow visualisation and directly measures the lift, drag and pitching moment at 400Hz with Strouhal Numbers of up to 1.2 at a Reynolds Number of 1x10{6}. The configuration for phase linked heave (flap-wise) and surge (chord-wise) periodic motions will be described in detail with respect to previous work in the field. The current experimental program for Reynolds numbers from 1x10{6} down to 2.5x10{6} will also be described herein." @default.
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- W2212384698 date "1995-01-01" @default.
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- W2212384698 title "Experimental Investigation of the Unsteady Aerodynamics of a Symmetric Aerofoil at Low Reynolds Numbers" @default.
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