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About the suitability of different numerical methods to reproduce model wind turbine measurements in a wind tunnel with a high blockage ratio

机译:关于不同数值方法的适用性在具有高封闭率的风洞中再现模型风力涡轮机测量

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摘要

In the present paper, numerical and experimental investigations of a modelwind turbine with a diameter of 3.0 m are described. The study hasthree objectives. The first one is the provision of validation data. Thesecond one is to estimate the influence of the wind tunnel walls by comparingmeasurements to simulated results with and without wind tunnel walls. Thelast objective is the comparison and evaluation of methods of high fidelity,namely computational fluid dynamics, and medium fidelity, namely lifting-linefree vortex wake. The experiments were carried out in the large wind tunnelof the TU Berlin where a blockage ratio of 40 % occurs. With the lifting-line free vortex wake code QBlade, the turbine was simulated under farfield conditions at the TU Berlin. Unsteady Reynolds-averaged Navier–Stokessimulations of the wind turbine, including wind tunnel walls and under farfield conditions, were performed at the University of Stuttgart with thecomputational fluid dynamics code FLOWer.Comparisons among the experiment, the lifting-line free vortex wake code andthe computational fluid dynamics code include on-blade velocity and angle ofattack. Comparisons of flow fields are drawn between the experiment and thecomputational fluid dynamics code. Bending moments are compared among thesimulations.A good accordance was achieved for the on-blade velocity and the angle ofattack, whereas deviations occur for the flow fields and the bending moments.
机译:在本文中,模型的数值和实验研究描述直径为3.0米的风力涡轮机。这项研究有三个目标。第一个是提供验证数据。这第二个是通过比较来估计风洞墙壁的影响对模拟结果的测量结果,没有风洞墙壁。这最后目标是对高保真方法的比较和评估,即计算流体动力学,中等保真度,即升降线免费涡旋唤醒。实验是在大型风洞中进行的涂布柏林的封闭比例为40%。通过升降线免费涡旋唤醒代码QBLADE,涡轮机在远处模拟涂尔林的现场条件。 unsteady reynolds-perveraged navier-stokes风力涡轮机的模拟,包括风洞墙壁和远处现场条件,在斯图加特大学进行计算流体动力学代码花。实验中的比较,升降线免费涡旋唤醒代码和计算流体动力学码包括叶片速度和角度攻击。在实验和实验之间绘制流场比较计算流体动力学代码。弯曲的时刻在比较模拟。根据刀片速度和角度达到了良好攻击,虽然流场和弯曲时刻发生偏差。

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