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The Performance Test of Three Different Horizontal Axis Wind Turbine (HAWT) Blade Shapes Using Experimental and Numerical Methods

机译:使用实验和数值方法对三种不同水平轴风力涡轮机叶片形状的性能测试

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Three different horizontal axis wind turbine (HAWT) blade geometries with the same diameter of 0.72 m using the same NACA4418 airfoil profile have been investigated both experimentally and numerically. The first is an optimum (OPT) blade shape, obtained using improved blade element momentum (BEM) theory. A detailed description of the blade geometry is also given. The second is an untapered and optimum twist (UOT) blade with the same twist distributions as the OPT blade. The third blade is untapered and untwisted (UUT). Wind tunnel experiments were used to measure the power coefficients of these blades, and the results indicate that both the OPT and UOT blades perform with the same maximum power coefficient, Cp = 0.428, but it is located at different tip speed ratio, λ = 4.92 for the OPT blade and λ = 4.32 for the UOT blade. The UUT blade has a maximum power coefficient of Cp = 0.210 at λ = 3.86. After the tests, numerical simulations were performed using a full three-dimensional computational fluid dynamics (CFD) method using the k-ω SST turbulence model. It has been found that CFD predictions reproduce the most accurate model power coefficients. The good agreement between the measured and computed power coefficients of the three models strongly suggest that accurate predictions of HAWT blade performance at full-scale conditions are also possible using the CFD method.
机译:已经通过实验和数值研究了三种具有相同直径0.72 m,使用相同NACA4418翼型轮廓的不同水平轴风力涡轮机(HAWT)叶片几何形状。第一种是使用改进的叶片元素动量(BEM)理论获得的最佳(OPT)叶片形状。还给出了叶片几何形状的详细描述。第二个是没有锥度的最佳扭曲(UOT)刀片,其扭曲分布与OPT刀片相同。第三刀片不带锥度且不扭曲(UUT)。使用风洞实验测量了这些叶片的功率系数,结果表明,OPT和UOT叶片的性能均具有相同的最大功率系数C p = 0.428,但其位于尖端速度比不同,对于OPT刀片,λ= 4.92,对于UOT刀片,λ= 4.32。在λ= 3.86时,UUT刀片的最大功率系数为C p = 0.210。测试后,使用k-ωSST湍流模型,使用完整的三维计算流体动力学(CFD)方法进行了数值模拟。已经发现,CFD预测可再现最准确的模型功率系数。三种模型的实测功率系数和计算出的功率系数之间的良好一致性有力地表明,使用CFD方法还可以在满量程条件下准确预测HAWT叶片的性能。

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