Enhancing aerodynamic performance of vertical axis wind turbines using bionic airfoils inspired by swordfish tail

IF 1.9 3区 工程技术 Q3 MECHANICS
Hui Song, Zhou Ye, Ying Wang, Chun Li
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Abstract

In this work, a pioneering approach is proposed to enhance the efficacy of vertical axis wind turbines within the aerodynamic field. This innovative method involves integrating a bionic airfoil, inspired by the tail fin of a swordfish, along the trailing edge of the airfoil. To evaluate the impact of these biomimetic airfoils on wind turbine functionality, applications such as numerical simulations facilitated by computational fluid dynamics (CFD) and design of experiments (DOE) were employed. The primary objective of this study is to mitigate the flow separation phenomenon that occurs when wind turbines operate at low tip speed ratios (TSR < 4). The results indicate that the addition of the bionic tail delays the angle at which the peak torque appears, and enhances positive torque generation effectively within the phase angle range of 60° to 150°, suggesting successful suppression of the flow separation phenomenon. The presence of the tail also postpones the occurrence of dynamic stall, particularly near the trailing edge of the airfoil, and reduces losses associated with the expansion and shedding of dynamic stall vortices. As the tip speed ratio increases, the average power coefficient of the bionic airfoil exhibits a positive trend. Notably, at a tip speed ratio of 2.63, a significant increase in the average power coefficient of approximately 17% was observed. The analysis of the downstream wake of the wind turbine reveals that the bionic tail enhances the speed loss in the wake. This indicates that the blades can generate greater lift at a lower tip speed ratio, allowing the vertical axis wind turbine to operate effectively at low wind speeds, particularly in urban areas with significant development potential.

剑鱼尾仿生翼型提升垂直轴风力涡轮机气动性能
在这项工作中,提出了一种开创性的方法来提高垂直轴风力发电机在空气动力领域的效率。这种创新的方法包括整合仿生翼型,灵感来自剑鱼的尾鳍,沿着翼型的后缘。为了评估这些仿生翼型对风力涡轮机功能的影响,研究人员采用了计算流体动力学(CFD)和实验设计(DOE)等方法进行数值模拟。本研究的主要目的是减轻风力涡轮机在低叶尖速比下运行时发生的流动分离现象(TSR < 4)。结果表明:仿生尾的加入延迟了扭矩峰值出现的角度,并在相位角60°~ 150°范围内有效增强了正扭矩的产生,成功抑制了流动分离现象;尾翼的存在也推迟了动态失速的发生,特别是在翼型的后缘附近,并减少了与动态失速旋涡的膨胀和脱落相关的损失。随着叶尖速比的增大,仿生翼型的平均功率系数呈增大趋势。值得注意的是,在叶尖速比为2.63时,平均功率系数显著提高了约17%。对风力机下游尾迹的分析表明,仿生尾迹增大了尾迹中的速度损失。这表明叶片可以在较低的叶尖速比下产生更大的升力,使垂直轴风力涡轮机能够在低风速下有效运行,特别是在具有重大发展潜力的城市地区。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Meccanica
Meccanica 物理-力学
CiteScore
4.70
自引率
3.70%
发文量
151
审稿时长
7 months
期刊介绍: Meccanica focuses on the methodological framework shared by mechanical scientists when addressing theoretical or applied problems. Original papers address various aspects of mechanical and mathematical modeling, of solution, as well as of analysis of system behavior. The journal explores fundamental and applications issues in established areas of mechanics research as well as in emerging fields; contemporary research on general mechanics, solid and structural mechanics, fluid mechanics, and mechanics of machines; interdisciplinary fields between mechanics and other mathematical and engineering sciences; interaction of mechanics with dynamical systems, advanced materials, control and computation; electromechanics; biomechanics. Articles include full length papers; topical overviews; brief notes; discussions and comments on published papers; book reviews; and an international calendar of conferences. Meccanica, the official journal of the Italian Association of Theoretical and Applied Mechanics, was established in 1966.
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