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Trailing-Edge Noise Measurements of Wind Turbine Airfoils in Open and Closed Test Section Wind Tunnels

机译:开放式和闭合试验段风力涡轮机翼型的后缘噪声测量风隧道

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This paper describes two-dimensional trailing edge noise measurements in open and closed test section wind tunnels. The investigations are related to the EU-funded project SIROCCO, which aims to find quiet airfoils for wind turbines without a decrease in aerodynamic performance. Trailing edge noise measurements were performed in the open jet of the Aeroacoustic Wind Tunnel Braunschweig (AWB) using a phased microphone array. In addition, the trailing edge noise of the same models was measured in the closed section of the Laminar Wind Tunnel Stuttgart (LWT), using the new Coherent Particle Velocity (CPV) method. This method is based on the cross correlation of two hot-wire signals. The experimental results obtained in the two wind tunnels could be quantitatively compared after application of appropriate wind tunnel corrections. The sound pressure frequency spectra are basically parallel in the range of sufficient measurement accuracy. The total sound pressure levels vs. lift coefficient show a more or less constant offset of about 2 dB between AWB and LWT. Given the totally different measurement principles this can be regarded as a very good agreement.
机译:本文介绍了开放式和闭合试验段风隧道中的二维后缘噪声测量。调查与欧盟资助的项目西罗科有关,旨在为风力涡轮机找到安静的翼型,而不会降低空气动力学性能。使用相控麦克风阵列在空气声隧道Braunschweig(AWB)的开口射流中进行后缘噪声测量。另外,使用新的相干粒子速度(CPV)方法,在层状风洞斯图加特(LWT)的封闭部分中测量相同型号的后缘噪声。该方法基于两个热线信号的互相关。在施加适当的风隧道校正之后,可以定量比较两个风隧道中获得的实验结果。声压频谱基本上在足够的测量精度范围内平行。总声压水平与升力系数在AWB和LWT之间显示出约2 dB的或多或少恒定的偏移。鉴于完全不同的测量原则,这可以被视为一个非常愉快的一致性。

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