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Aerodynamic optimization of wind turbine rotors using a blade element momentum method with corrections for wake rotation and expansion
Author(s) -
Døssing Mads,
Madsen Helge Aa.,
Bak Christian
Publication year - 2012
Publication title -
wind energy
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.743
H-Index - 92
eISSN - 1099-1824
pISSN - 1095-4244
DOI - 10.1002/we.487
Subject(s) - wake , aerodynamics , turbine , mechanics , rotation (mathematics) , aerodynamic force , momentum (technical analysis) , tip speed ratio , rotor (electric) , blade pitch , blade element momentum theory , physics , blade element theory , turbine blade , structural engineering , engineering , mechanical engineering , mathematics , geometry , finance , economics
ABSTRACT The blade element momentum (BEM) method is widely used for calculating the quasi‐steady aerodynamics of horizontal axis wind turbines. Recently, the BEM method has been expanded to include corrections for wake expansion and the pressure due to wake rotation ( BEM cor ), and more accurate solutions can now be obtained in the blade root and tip sections. It is expected that this will lead to small changes in optimum blade designs. In this work,BEM corhas been implemented, and the spanwise load distribution has been optimized to find the highest possible power production. For comparison, optimizations have been carried out using BEM as well. Validation ofBEM corshows good agreement with the flow calculated using an advanced actuator disk method. The maximum power was found at a tip speed ratio of 7 usingBEM cor , and this is lower than the optimum tip speed ratio of 8 found for BEM. The difference is primarily caused by the positive effect of wake rotation, which locally causes the efficiency to exceed the Betz limit. Wake expansion has a negative effect, which is most important at high tip speed ratios. It was further found that by usingBEM cor , it is possible to obtain a 5% reduction in flap bending moment when compared with BEM. In short,BEM corallows fast aerodynamic calculations and optimizations with a much higher degree of accuracy than the traditional BEM model. Copyright © 2011 John Wiley & Sons, Ltd.

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