Abstract
The present paper describes a method to calculate velocity profiles in the boundary layer of a rotating blade. A differential approach is used to solve the laminar boundary layer equations. The effects of tip speed ratio, dimensionless radial position r/R and angle of attack have been analyzed. The test airfoils used in the simulations are NACA 63-215 and S809. The resulting velocity profiles in the chordwise and spanwise directions are mapped and stored in a Database according to the boundary layer parameters. © 2007 IOP Publishing Ltd.
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CITATION STYLE
Martínez H, G. G., Sørensen, J. N., & Shen, W. Z. (2007). 3D boundary layer study on a rotating wind turbine blade. In Journal of Physics: Conference Series (Vol. 75). Institute of Physics Publishing. https://doi.org/10.1088/1742-6596/75/1/012032
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