Determination of Optimal Geometry for an Empty Concentrator Augmented Wind Turbine

C. Shonhiwa, G. Makaka, P. Mukumba, Ngwarai Shambira
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Abstract

Aims: To determine the optimal concentrator geometrical parameters of an empty concentrator augmented wind turbine (CAWT), which are used to design and install CAWTs. Place and Duration of Study: Physics Department, University of Fort Hare, South Africa between March 2023, and October 2023. Methodology: The study used the concentrator length (L) to concentrator outlet diameter ratio (Lr) and the difference between inlet and outlet radii to concentrator outlet diameter ratio (Rr) to investigate the effect of concentrator geometry on wind velocity augmentation and air dynamics to determine the optimum concentrator geometrical parameters using computational fluid dynamics modelling. The modelled concentrators’ geometry was created in SolidWorks, prepared for meshing in SpaceClaim, meshed, and analysed in Fluent to solve the Reynolds-averaged Navier-Stokes equations, and validated by primary experimental results. To make the concentrators, six equally spaced Lr were used in the range 0.1 \(\le\) Lr \(\le\) 0.6  and thirteen equally spaced Rr in the range 0.025 \(\le\) Rr  \(\le\) 0.325 . The concentrators’ performance was investigated in terms of velocity augmentation ratio (Vr) and concentrator efficiency (\(\eta\)c). Results: It was observed that the variation in Vr was influenced by the change in both Lr and Rr. The Vr and \(\eta\)c   increased with an increase in Lr to a maximum at optimum Lr  and decreased thereafter. The optimum Vr was obtained at Lr = 0.4 and Rr  = 0.1 with a maximum velocity at the concentrator outlet. It was also shown that the energy losses due to friction negatively impact velocity augmentation more than energy losses due to a large concentrator tilt angle at high Lr . Conclusion: When constructing a CAWT, the turbine rotor should be placed at any distance between the concentrator outlet and 0.5L  behind the concentrator, and the blade tips of the turbine in a CAWT system should be at least 10% smaller than the concentrator outlet radius, for the whole rotor to receive wind with augmented velocity.
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确定空聚光器增强型风力涡轮机的最佳几何形状
目的: 确定空聚光器增强风力涡轮机(CAWT)的最佳聚光器几何参数,用于设计和安装 CAWT。研究地点和时间:南非黑尔堡大学物理系,2023 年 3 月至 2023 年 10 月。研究方法:该研究使用聚光器长度(L)与聚光器出口直径之比(Lr)以及入口和出口半径之差与聚光器出口直径之比(Rr)来研究聚光器几何形状对风速增强和空气动力学的影响,从而利用计算流体动力学建模确定最佳聚光器几何参数。聚光器的几何模型在 SolidWorks 中创建,在 SpaceClaim 中准备网格划分,在 Fluent 中进行网格划分和分析,以求解雷诺平均纳维-斯托克斯方程,并通过主要实验结果进行验证。为了制作聚光器,使用了六个等间距的 Lr,范围为 0.1 \(\le\) Lr \(\le\) 0.6,十三个等间距的 Rr,范围为 0.025 \(\le\) Rr \(\le\) 0.325。根据速度增强比(Vr)和浓缩器效率(\(\eta\)c)对浓缩器的性能进行了研究。结果:观察到 Vr 的变化受 Lr 和 Rr 变化的影响。Vr和\(\eta\)c随着Lr的增大而增大,在最佳Lr时达到最大值,随后减小。最佳 Vr 值出现在 Lr = 0.4 和 Rr = 0.1 时,聚能器出口处的速度最大。研究还表明,在高 Lr 条件下,摩擦造成的能量损失对速度提升的负面影响大于浓缩器倾斜角过大造成的能量损失。结论:在建造 CAWT 时,涡轮机转子应放置在聚光器出口与聚光器后方 0.5L 之间的任意距离,并且 CAWT 系统中的涡轮机叶尖应至少比聚光器出口半径小 10%,这样整个转子才能以增强的速度接收风。
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