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WIND TURBINE AIRFOIL DESIGN METHOD BY NCGA AND AIRFOIL USING THE METHOD
WIND TURBINE AIRFOIL DESIGN METHOD BY NCGA AND AIRFOIL USING THE METHOD
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机译:基于NCGA的风轮机翼型设计方法及采用该方法的翼型
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摘要
PURPOSE: A rotor blade airfoil design method for a wind turbine using genetic algorithm and an airfoil by the same are provided to optimize the airfoil profile of a rotor blade, thereby ensuring good blade efficiency. CONSTITUTION: A rotor blade airfoil design method for a wind turbine using genetic algorithm comprises the steps of: creating an airfoil profile using an optimization method(S2), calculating an objective function(S5), applying genetic algorithm(S6), drawing a candidate airfoil profile group optimized through the genetic algorithm(S7), and selecting the optimum profile from the candidate group(S8).
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