推力缩放 IEA 15 兆瓦风力涡轮机模型的空气动力特性:利用 PIV 数据的实验启示

E. Fritz, André F. P. Ribeiro, K. Boorsma, Carlos Ferreira
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引用次数: 1

摘要

摘要本研究介绍了三叶水平轴风力涡轮机的风洞试验结果。该风机模型是 IEA 15 兆瓦参考风机的缩小版,保留了沿叶片的非尺寸推力分布。使用粒子图像测速仪捕捉了叶片周围多个径向位置的流场。除这些流场外,该综合数据集还包含边界环流的跨度分布、流入条件以及从速度场推导出的叶片力。因此,这三个叶片的空气动力学特性得到了全面描述。研究表明,沿跨度测得的升力系数与叶片设计中所用机翼的升力极值非常吻合,从而验证了实验方法。这项研究为验证模拟最先进风力涡轮机的低保真到高保真数值模型提供了宝贵的公共实验数据集。此外,本文还确定了新开发的风力涡轮机模型的气动特性,为今后使用该模型进行风洞实验奠定了基础。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Aerodynamic characterisation of a thrust-scaled IEA 15 MW wind turbine model: experimental insights using PIV data
Abstract. This study presents results from a wind tunnel experiment on a three-bladed horizontal axis wind turbine. The model turbine is a scaled-down version of the IEA 15 MW reference wind turbine, preserving the non-dimensional thrust distribution along the blade. Flow fields were captured around the blade at multiple radial locations using particle image velocimetry. In addition to these flow fields, this comprehensive dataset contains spanwise distributions of bound circulation, inflow conditions and blade forces derived from the velocity field. As such, the three blades' aerodynamics are fully characterised. It is demonstrated that the lift coefficient measured along the span agrees well with the lift polar of the airfoil used in the blade design, thereby validating the experimental approach. This research provides a valuable public experimental dataset for validating low- to high-fidelity numerical models simulating state-of-the-art wind turbines. Furthermore, this article establishes the aerodynamic properties of the newly developed model wind turbine, creating a baseline for future wind tunnel experiments using this model.
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