Wake characteristics of a balloon wind turbine and aerodynamic analysis of its balloon using a large eddy simulation and actuator disk model

IF 3.6 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY
Aref Ehteshami, Mostafa Varmazyar
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Abstract

Abstract. In the realm of novel technologies for generating electricity from renewable resources, an emerging category of wind energy converters called airborne wind energy systems (AWESs) has gained prominence. These pioneering systems employ tethered wings or aircraft that operate at higher atmospheric layers, enabling them to harness wind speeds surpassing conventional wind turbines' capabilities. The balloon wind turbine is one type of AWESs that utilizes the buoyancy effect to elevate the turbine to altitudes typically ranging from 400 to 1000 m. In this paper, the wake characteristics and aerodynamics of a balloon wind turbine were numerically investigated for different wind scenarios. Large eddy simulation, along with the actuator disk model, was employed to predict the wake behavior of the turbine. To improve the accuracy of the simulation results, a structured grid was generated and refined by using an algorithm to resolve about 80 % of the local turbulent kinetic energy in the wake. Results contributed to designing an optimized layout of wind farms and stability analysis of such systems. The capabilities of the hybrid large eddy simulation and actuator disk model (LES–ADM) when using the mesh generation algorithm were evaluated against the experimental data on a smaller wind turbine. The assessment revealed a good agreement between numerical and experimental results. While a weakened rotor wake was observed at the distance of 22.5 diameters downstream of the balloon turbine, the balloon wake disappeared at about 0.6 of that distance in all the wind scenarios. Vortices generated by the rotor and balloon started to merge at the tilt angle of 10∘, which intensified the turbulence intensity at 10 diameters downstream of the turbine for the wind speeds of 7 and 10 m s−1. By increasing the tilt angle, the lift force on the wings experienced a sharper increase with respect to that of the whole balloon, which signified a controlling system requirement for balancing such an extra lift force.
气球风力涡轮机的风浪特性以及利用大涡模拟和致动器圆盘模型对其气球进行的空气动力学分析
摘要在利用可再生资源发电的新技术领域,一种被称为机载风能系统(AWES)的新兴风能转换器已崭露头角。这些开创性的系统采用系留机翼或飞机,在较高的大气层运行,使其能够利用超过传统风力涡轮机能力的风速。气球风力涡轮机是 AWES 的一种,它利用浮力效应将涡轮机提升到通常为 400 至 1000 米的高度。本文针对不同的风力情况,对气球风力涡轮机的尾流特性和空气动力学进行了数值研究。采用大涡流模拟和致动器盘模型来预测涡轮机的尾流行为。为了提高模拟结果的准确性,使用一种算法生成并细化了结构化网格,以解析尾流中约 80% 的局部湍流动能。模拟结果有助于设计风电场的优化布局和对此类系统进行稳定性分析。使用网格生成算法时,混合大涡流模拟和致动器盘模型(LES-ADM)的能力根据较小风力涡轮机的实验数据进行了评估。评估结果表明,数值结果与实验结果之间存在良好的一致性。在气球涡轮机下游 22.5 直径处观察到转子尾流减弱,而在所有风力情况下,气球尾流在该距离的 0.6 处消失。在倾斜角为 10∘时,涡轮和气球产生的涡流开始合并,在风速为 7 m s-1 和 10 m s-1 时,涡轮下游 10 直径处的湍流强度增强。随着倾斜角的增大,机翼上的升力相对于整个气球的升力急剧增大,这表明控制系统需要平衡这种额外的升力。
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来源期刊
Wind Energy Science
Wind Energy Science GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY-
CiteScore
6.90
自引率
27.50%
发文量
115
审稿时长
28 weeks
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