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Study of Aerodynamic Performance and Power Output for Residential-Scale Wind Turbines

机译:住宅尺度风力涡轮机空气动力性能和功率输出研究

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This study presents the rotor blade airfoil analysis of residential-scale wind turbines. On this track, four new airfoils (GOE447, GOE446, NACA 6412, and NACA 64(3)-618) characterized by their high lift-to-drag ratios (161.3, 148.7, 142.7, and 136.3, respectively). These new airfoils are used to generate an entire 7 m long blades for three-bladed rotor horizontal axis wind turbine models tested numerically at low, medium, and rated wind speeds of 7.5, 10, and 12.5 m/s, respectively, with a design tip speed ratio of 7. The criterion to judge each model's performance is power output. Thus, the blades of the model that produce the highest power are selected to undergo a tip modification (winglet) and leading-edge modification (tubercles), seeking power improvement. It is found that the GOE 447 airfoil outperformed the other three airfoils at all tested wind speeds. Thus, it is opted for adding winglets and tubercles. At 12.5 m/s, winglet design produced 5% more power, while tubercles produced 5.5% more power than the GOE 447 baseline design. Furthermore, the computational domain is divided into two regions: rotating (the disc that encloses the rotor) and stationary (the rest of the flow domain). Meanwhile, the numerical model is validated against the experimental velocity measurements. Since Reynolds-averaged Navier-Stokes with k-ω shear stress transport turbulence model can capture the laminar-to-turbulent boundary layer transition, it is used in the 18 simulations of the current work. However, large eddy simulation (LES) can deal successfully with the various scale eddies resulting from the rotor blades and its interactions with the surrounding flow. Thus, the LES was used in the six simulations done at the rated wind speed. LES power output calculation is 7.9% to 11.9% higher than the RANS power output calculation.
机译:本研究介绍了居民级风力涡轮机的转子叶片翼型分析。在该轨道上,四种新的翼型(GOE447,GOE446,NACA 6412和NACA 64(3)-618),其特征在于它们的高升力比率(分别为161.3,148.7,142.7和136.3)。这些新的翼型用于为三刃转子水平轴风力涡轮机模型产生整个7米长的叶片,分别在低,介质和额定的风速下进行数值在7.5,10和12.5米/秒,设计尖端速度比为7.判断每个模型性能的标准是电源输出。因此,选择产生最高功率的模型的刀片被选择以进行尖端修改(小翼)和前缘修改(结节),寻求功率改进。发现GOE 447翼型在所有测试的风速下表现出其他三个翼型。因此,选择添加小翼和结节。在12.5米/秒,小翼设计的功率增加了5%,而结节产生的功率比GoE 447基线设计更多。此外,计算结构域被分成两个区域:旋转(封闭转子的盘)和静止(流动域的其余部分)。同时,根据实验速度测量验证数值模型。由于Reynolds平均Navier-Stokes具有K-Ω剪切应力传输湍流模型,因此可以捕获层流 - 湍流边界层过渡,它用于当前工作的18模拟中。然而,大型涡流模拟(LES)可以成功地处理由转子叶片的各种刻度漩涡及其与周围流动的相互作用。因此,在以额定风速完成的六种模拟中使用LES。 LES电源输出计算比RAN电源输出计算高7.9%至11.9%。

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