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Abstract

This paper describes a three-dimensional analysis of the laminar boundary layer that develops on the blades of an horizontalaxis wind turbine. The main aim was to investigate a fundamental phenomenon: the effect of rotation on the blade boundary layer of a wind turbine in conjunction with the widely observed phenomenon of stall-delay. The separation position in retarded flows with pressure gradients is calculated and compared for the rotation and non-rotation cases. It is concluded that the stall is linearly postponed due to the Coriolis force and the separation point is delayed as a result of increasing rotation speed or decreasing blade spanwise position. (© 2004 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)