何娇, 金鑫, 谢双义, 刘龙, 曹乐. 基于不同CFD建模复杂度的垂直轴风力机气动性能分析[J]. 太阳能学报, 2021, 42(12): 150-156. DOI: 10.19912/j.0254-0096.tynxb.2019-1420
引用本文: 何娇, 金鑫, 谢双义, 刘龙, 曹乐. 基于不同CFD建模复杂度的垂直轴风力机气动性能分析[J]. 太阳能学报, 2021, 42(12): 150-156. DOI: 10.19912/j.0254-0096.tynxb.2019-1420
He Jiao, Jin Xin, Xie Shuangyi, Liu Long, Cao Le. AERODYNAMIC PERFORMANCE ANALYSIS OF VERTICAL AXIS WIND TURBINES BASED ON DIFFERENT CFD MODELING COMPLEXITIES[J]. Acta Energiae Solaris Sinica, 2021, 42(12): 150-156. DOI: 10.19912/j.0254-0096.tynxb.2019-1420
Citation: He Jiao, Jin Xin, Xie Shuangyi, Liu Long, Cao Le. AERODYNAMIC PERFORMANCE ANALYSIS OF VERTICAL AXIS WIND TURBINES BASED ON DIFFERENT CFD MODELING COMPLEXITIES[J]. Acta Energiae Solaris Sinica, 2021, 42(12): 150-156. DOI: 10.19912/j.0254-0096.tynxb.2019-1420

基于不同CFD建模复杂度的垂直轴风力机气动性能分析

AERODYNAMIC PERFORMANCE ANALYSIS OF VERTICAL AXIS WIND TURBINES BASED ON DIFFERENT CFD MODELING COMPLEXITIES

  • 摘要: 通过将计算流体力学(CFD)与实验结果比较,研究2D URANS、2.5D URANS、2.5D LES和3D URANS CFD建模技术在风力机气动性能分析中的准确性和可行性。与SST k-ω方法相比,LES模型可更准确地模拟垂直轴风力机在动态失速工况下的气动性能。2.5D LES模拟结果的显著改善表明:叶尖涡的忽略可能不是2D URANS和2.5D URANS过高预测功率输出的主要原因,而可能是由其方程存在的内部缺陷导致的。考虑到模型的计算精度和计算成本,2.5D LES可被认为是研究风力机气动性能的一种有效方法,特别适用于垂直轴风力机启动工况的仿真。

     

    Abstract: Computational fluid dynamics(CFD)is an effective method to study the aerodynamic performance of vertical axis wind turbines(VAWTs). At present,the two-dimensional(2 D)Unsteady Reynolds Average Navier Stokes(URANS)method has been widely used to analyze the aerodynamic performance of VAWTs,but its accuracy is limited. In this paper,the accuracy and feasibility of the 2 D URANS,2.5 D URANS,2.5 D LES and 3 D URANS CFD modeling techniques are studied for wind turbine aerodynamic performance analyses by comparing with the experimental results. Compared with the SST k-ω method,the LES method can provide more accurate results under the dynamic stall conditions. The significant improvement of the 2.5 D LES simulation results show that the neglect of blade tip vortices may not be the main reason for the excessive prediction power of both 2 D and 2.5 D URANS,but may be due to the internal defects of the equation. Considering the calculation accuracy and cost of both 2.5 D LES and 3 D URANS models,2.5 D LES can be regarded as an effective method to study the aerodynamic performance of VAWTs,especially for the start-up condition of VAWTs.

     

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