Accuracy assessment of Beddoes-Leishman and IAG dynamic stall models for wind turbine applications

O. S. Mohamed, P. F. Melani, G. Bangga, Navid Aryan, Luca Greco, A. Bianchini
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Abstract

The study presents a systematic comparison between two of the most-credited dynamic stall models for wind turbine applications: the original Beddoes-Leishman (BL) model and the newly-developed IAG. The scope of such comparison, supported by experimental data, is to shed new light on the actual suitability of current dynamic stall models for their integration into modern wind turbine simulation codes, and on the best practices to calibrate them. Two different strategies are followed for the calibration of the BL model: 1) standard one, compliant with common practices found in the literature; 2) a physics-oriented one, focusing on the constants defining the dynamic stall onset as well as on the parameters governing the duration of the vortex shedding process. The IAG model, initially developed based on the first-order BL formulation and recently improved by reducing the number of constants and removing compressibility effects, is applied instead in its standard form only. The two models are compared across a range of oscillation mean angles, amplitudes, and reduced frequencies. Results demonstrate that the original BL model, although with a challenging calibration process, when properly tuned, can provide a very good description of aerodynamic unsteady loads. While showing consistent results, the IAG formulation appears to be more robust, as it employs fewer constants and extracts most of the needed information directly from the input polar data. The comparison between the calibrated BL and IAG models highlights critical modelling aspects, the computation of drag and determination of the stall onset above all, offering valuable insights for the future development of dynamic stall formulations.
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风力涡轮机应用中 Beddoes-Leishman 和 IAG 动态失速模型的精度评估
本研究系统地比较了风力涡轮机应用中两个最受认可的动态失速模型:最初的贝多斯-莱西曼(Beddoes-Leishman,BL)模型和新开发的 IAG。在实验数据的支持下,这种比较的目的是揭示当前动态失速模型与现代风力涡轮机仿真代码整合的实际适用性,以及校准这些模型的最佳实践。在校准 BL 模型时采用了两种不同的策略:1) 标准策略,符合文献中的常见做法;2) 物理导向策略,重点关注定义动态失速起始点的常数以及涡流脱落过程持续时间的参数。IAG 模型最初是基于一阶 BL 公式开发的,最近通过减少常数数量和消除可压缩性效应进行了改进,现在仅以其标准形式应用。在一系列振荡平均角、振幅和降低频率范围内对这两个模型进行了比较。结果表明,原始的 BL 模型虽然校准过程具有挑战性,但如果调整得当,可以很好地描述空气动力非稳态载荷。在显示一致结果的同时,IAG 公式似乎更加稳健,因为它采用了更少的常数,并直接从输入的极地数据中提取了大部分所需的信息。经过校准的 BL 模型和 IAG 模型之间的比较突出了建模的关键方面,尤其是阻力的计算和失速起始点的确定,为今后动态失速公式的开发提供了宝贵的启示。
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