Discovery of a Physically Interpretable Data-Driven Wind-Turbine Wake Model

IF 2.4 3区 工程技术 Q3 MECHANICS
Kherlen Jigjid, Ali Eidi, Nguyen Anh Khoa Doan, Richard P. Dwight
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Abstract

This study presents a compact data-driven Reynolds-averaged Navier-Stokes (RANS) model for wind turbine wake prediction, built as an enhancement of the standard \(k\)-\(\varepsilon\) formulation. Several candidate models were discovered using the symbolic regression framework Sparse Regression of Turbulent Stress Anisotropy (SpaRTA), trained on a single Large Eddy Simulation (LES) dataset of a standalone wind turbine. The leading model was selected by prioritizing simplicity while maintaining reasonable accuracy, resulting in a novel linear eddy viscosity model. This selected leading model reduces eddy viscosity in high-shear regions—particularly in the wake—to limit turbulence mixing and delay wake recovery. This addresses a common shortcoming of the standard \(k\)-\(\varepsilon\) model, which tends to overpredict mixing, leading to unrealistically fast wake recovery. Moreover, the formulation of the leading model closely resembles that of the established \(k\)-\(\varepsilon\)-\(f_P\) model. Consistent with this resemblance, the leading and \(k\)-\(\varepsilon\)-\(f_P\) models show nearly identical performance in predicting velocity fields and power output, but they differ in their predictions of turbulent kinetic energy. In addition, the generalization capability of the leading model was assessed using three unseen six-turbine configurations with varying spacing and alignment. Despite being trained solely on a standalone turbine case, the model produced results comparable to LES data. These findings demonstrate that data-driven methods can yield interpretable, physically consistent RANS models that are competitive with traditional modeling approaches while maintaining simplicity and achieving generalizability.

物理上可解释的数据驱动的风力涡轮机尾流模型的发现
本研究提出了一个紧凑的数据驱动的雷诺平均纳维-斯托克斯(RANS)模型,用于风力涡轮机尾流预测,作为标准\(k\) - \(\varepsilon\)公式的增强。使用符号回归框架湍流应力各向异性稀疏回归(SpaRTA)发现了几个候选模型,并在一个独立风力涡轮机的大涡模拟(LES)数据集上进行了训练。在保持合理精度的同时,优先考虑简单性,选择了领先的模型,形成了一种新颖的线性涡旋粘度模型。这种选择的领先模型减少了高剪切区域的涡流粘度-特别是在尾流中-以限制湍流混合和延迟尾流恢复。这解决了标准\(k\) - \(\varepsilon\)模型的一个共同缺点,即倾向于过度预测混合,导致不现实的快速尾迹恢复。此外,主导模型的公式与已建立的\(k\) - \(\varepsilon\) - \(f_P\)模型非常相似。与这种相似性相一致的是,领先模型和\(k\) - \(\varepsilon\) - \(f_P\)模型在预测速度场和功率输出方面表现出几乎相同的性能,但它们在预测湍流动能方面有所不同。此外,采用三种不可见的具有不同间距和对准的六涡轮配置评估了领先模型的泛化能力。尽管只在一个独立的涡轮箱上进行了训练,但该模型产生的结果与LES数据相当。这些发现表明,数据驱动的方法可以产生可解释的、物理上一致的RANS模型,与传统的建模方法竞争,同时保持简单性和通用性。
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来源期刊
Flow, Turbulence and Combustion
Flow, Turbulence and Combustion 工程技术-力学
CiteScore
5.70
自引率
8.30%
发文量
72
审稿时长
2 months
期刊介绍: Flow, Turbulence and Combustion provides a global forum for the publication of original and innovative research results that contribute to the solution of fundamental and applied problems encountered in single-phase, multi-phase and reacting flows, in both idealized and real systems. The scope of coverage encompasses topics in fluid dynamics, scalar transport, multi-physics interactions and flow control. From time to time the journal publishes Special or Theme Issues featuring invited articles. Contributions may report research that falls within the broad spectrum of analytical, computational and experimental methods. This includes research conducted in academia, industry and a variety of environmental and geophysical sectors. Turbulence, transition and associated phenomena are expected to play a significant role in the majority of studies reported, although non-turbulent flows, typical of those in micro-devices, would be regarded as falling within the scope covered. The emphasis is on originality, timeliness, quality and thematic fit, as exemplified by the title of the journal and the qualifications described above. Relevance to real-world problems and industrial applications are regarded as strengths.
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