Full dynamic similarity experiments and predictive modeling of wind turbine aerodynamics across control strategies.

IF 4.8 Q2 MULTIDISCIPLINARY SCIENCES
PNAS nexus Pub Date : 2026-09-07 eCollection Date: 2026-10-01 DOI:10.1093/pnasnexus/pgag303
John W Kurelek, Ilan M L Upfal, Supun Pieris, Kirby S Heck, Alexander Piqué, Marcus Hultmark, Michael F Howland
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Abstract

Wind turbines operate in turbulent atmospheric flow that constantly changes. In field tests, the full impacts of turbine design and operation are difficult to measure because confounding effects from atmospheric flow cannot be controlled. We address the gap in controlled experiments of wind turbines across control settings at dynamic similarity using a unique experimental framework that enables representative study of full-scale wind turbines in a laboratory-sized wind tunnel by pressurizing up to 220 atmospheres. This pressurization enables high-throughput experiments of a scaled wind turbine, at high Reynolds numbers and across yaw-misalignments and tip speed ratios relevant to commercial wind turbines. The results confirm that control strategies currently in use that were designed for turbines operating in ideal conditions without yaw misalignment should be modified, as the tip speed ratio that maximizes power depends on the yaw angle. Critically, the changes in forces and power with misalignment angle strongly depend on the tip speed ratio. We present a Unified Wind Turbine (UWT) model, which accurately predicts the behavior observed in these controlled experiments. The reliability of the UWT model to predict the synergistic effects of yaw misalignment and tip speed ratio enables its use in wind turbine design and wind farm flow control optimization to maximize the energy production and value of wind power systems. The cost-efficient experimental testbed in a pressurized wind tunnel presented herein offers a unique opportunity to study aerodynamics at dynamic similarity with large-scale, commercial turbines without many confounding effects and challenges faced in performing field tests.

跨控制策略的风力机空气动力学全动态相似实验与预测建模。
风力涡轮机在不断变化的湍流大气中运行。在现场试验中,由于大气流动的混杂效应无法控制,因此很难测量涡轮机设计和运行的全部影响。我们使用独特的实验框架解决了风力涡轮机控制实验在动态相似性控制设置中的差距,该实验框架通过加压高达220个大气压,可以在实验室大小的风洞中对全尺寸风力涡轮机进行代表性研究。这种加压使得在高雷诺数下,在与商用风力涡轮机相关的偏航失调和叶尖速比下,对规模风力涡轮机进行高通量实验成为可能。结果证实,目前使用的控制策略是为在没有偏航失调的理想条件下运行的涡轮机设计的,应该进行修改,因为最大功率的叶尖速比取决于偏航角。关键的是,力和功率的变化与不对准角强烈依赖于叶尖速比。我们提出了一个统一的风力发电机(UWT)模型,该模型准确地预测了这些控制实验中观察到的行为。UWT模型预测偏航失调和叶尖速比协同效应的可靠性使其能够用于风力涡轮机设计和风电场流量控制优化,以最大限度地提高风力发电系统的能量产量和价值。本文提出的具有成本效益的加压风洞实验试验台为研究与大型商用涡轮机在动力相似性下的空气动力学提供了独特的机会,而没有许多混淆效应和进行现场试验时面临的挑战。
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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CiteScore
1.80
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0.00%
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