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Aerodynamic and Aeroacoustic Study of the Interaction between a 2D Wind Turbine Airfoil and a Cylinder Wake using PIV and Farfield Microphones

机译:利用PIV和Farfield麦克风对2D风力涡轮机翼型和圆柱尾流之间的相互作用进行空气动力学和空气声学研究

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This paper investigates the aerodynamic and aeroacoustic characteristics of a 2D airfoil specially designed for wind turbine applications using PIV and a far field microphone array. The experiments were carried out in Syracuse University's Anechoic Wind Tunnel, both with and without large scale unsteadiness in the freestream generated by an upstream 2D cylinder. The results from both PIV measurements and surface pressure measurements show that the upstream cylinder created highly unsteady aerodynamic loading on the airfoil model. We also observed much higher lift fluctuation at high angle of attack due to the unsteady boundary separation on the airfoil suction surface. In the meantime, the far-field acoustic signals indicate that the large scale unsteadiness in the freestream generated higher noise especially at the lower frequency band.
机译:本文研究了专门为使用PIV和远场麦克风阵列的风力涡轮机应用设计的2D翼型的空气动力学和空气声学特性。实验是在锡拉丘兹大学(Syracuse University)的消声风洞中进行的,无论上游是否存在由上游2D圆柱产生的自由流中的大规模不稳定的情况。 PIV测量和表面压力测量的结果均表明,上游气缸在翼型模型上产生了非常不稳定的气动载荷。我们还观察到,由于翼型吸力表面上的不稳定边界分离,在高迎角下的升力波动要大得多。同时,远场声信号表明自由流中的大规模不稳定性会产生较高的噪声,尤其是在较低频段。

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