首页> 外文期刊>Journal of Energy Resources Technology >Wind Turbine Aerodynamic Modeling in Icing Condition: Three-Dimensional RANS-CFD Versus Blade Element Momentum Method
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Wind Turbine Aerodynamic Modeling in Icing Condition: Three-Dimensional RANS-CFD Versus Blade Element Momentum Method

机译:风力涡轮机空气动力学建模在结冰状态下:三维RANS-CFD与刀片元素动量法

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Icing limits the performance of wind turbines in cold climates. The prediction of the aerodynamic performance losses and their distribution due to ice accretion is essential. Blade element momentum (BEM) is the basis of blade structural studies. The accuracy and limitations of this method in icing condition are assessed in the present study. To this purpose, a computational study on the aerodynamic performance of the full-scale NREL 5MW rotor is performed. Three-dimensional (3D) steady Reynolds-averaged Navier-Stokes (RANS) simulations are performed for both clean and iced blade, as well as BEM calculations using two-dimensional (2D) computational fluid dynamics (CFD) sectional airfoil data. The total power calculated by the BEM method is in close agreement with the 3D CFD results for the clean blade. There is a 4% deviation, while it is underestimated by 28% for the iced one. The load distribution along the clean blade span differs between both methods. Load loss due to the ice, predicted by 3D CFD, is 32% in extracted power and the main loss occurs at the regions where the ice horn height exceeds 8% of the chord length.
机译:结冰限制了风力涡轮机在寒冷气候中的性能。预测气动性能损失及其由于冰含量的分布至关重要。刀片元素动量(BEM)是叶片结构研究的基础。在本研究中评估了该方法在糖霜条件下的准确性和限制。为此目的,执行对全尺寸NREL 5MW转子的空气动力学性能的计算研究。对于清洁和冰的刀片,对三维(3D)稳定的雷诺平均天瓦(RANS)模拟,以及使用二维(2D)计算流体动力学(CFD)截面翼型数据的BEM计算。 BEM方法计算的总功率与清洁刀片的3D CFD结果密切一致。偏离偏差4%,而冰的偏差是28%的低估。沿着清洁刀片跨度的负载分布在两种方法之间都不同。由于3D CFD预测的冰引起的负载损失,提取功率的32%,并且在冰角高度超过弦长的8%的区域发生主损失。

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