The aerodynamic performance of a modern, high-tip-speed, three-bladed windmill rated at lOkW at 30 mph was studied by three methods. First, the results of field tests of the actual device with both a resistive and a battery-charging electric load are reported. Second, the predictions of a simple blade-element analysis are presented and compared with the field data. Aerodynamic blade section coefficients of an actual blade section were measured in a wind tunnel and used as input in the analysis. Third, wind tunnel test results for a 1 5th scale model are given. Reynolds number simulation from model to prototype is considered in detail. The results of all three efforts are compared, and good agreement is shown. Nomenclature C = mean chord CL -coefficient of lift CD = coefficient of drag Re — Reynolds number V —velocity c = local chord q = dynamic pressure in centimeters of water r = local radius x = tip-speed ratio (QR/ K) a = angle of attack Q = angular velocity A = scaling factor v = kinematic viscosity
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