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An improved second-order dynamic stall model for wind turbine airfoils

机译:一种改进的风力涡轮机翼型动态失速模型

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摘要

Robust and accurate dynamic stall modeling remains one of the most difficult tasks in wind turbine load calculations despite its long research effort in the past. In the present paper, a new second-order dynamic stall model is developed with the main aim to model the higher harmonics of the vortex shedding while retaining its robustness for various flow conditions and airfoils. Comprehensive investigations and tests are performed at various flow conditions. The occurring physical characteristics for each case are discussed and evaluated in the present studies. The improved model is also tested on four different airfoils with different relative thicknesses. The validation against measurement data demonstrates that the improved model is able to reproduce the dynamic polar accurately without airfoil-specific parameter calibration for each investigated flow condition and airfoil. This can deliver further benefits to industrial applications where experimental/reference data for calibrating the model are not always available.
机译:尽管过去的研究努力,稳健和准确的动态摊位卷尺仍然是风力涡轮机负荷计算中最困难的任务之一。在本文中,开发了一种新的二阶动态失速模型,主要旨在模拟涡流脱落的更高谐波,同时保留其各种流动条件和翼型的鲁棒性。在各种流动条件下进行综合调查和测试。在本研究中讨论和评估每种情况的发生的物理特性。改进的模型也在四种不同的翼型中测试,具有不同的相对厚度。针对测量数据的验证表明,改进的模型能够精确地再现动态极性,而无需针对每个研究的流动条件和翼型的翼型特定的参数校准。这可以为工业应用提供进一步的好处,其中用于校准模型的实验/参考数据并不总是可用的。

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