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INFLUENCE OF DESIGN PARAMETERS ON THE UNSTEADY FLOW IN A CENTRIFUGAL FAN

机译:设计参数对离心式风扇非定常流动的影响

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The aim of this study is to evaluate the influence of design parameters on the unsteady flow in a forward-curved centrifugal fan and their impact on the aeroacoustic behavior. To do so, numerical and experimental study has been carried out on four centrifugal impellers designed with various geometrical parameters. The same volute casing has been used to study these fans. The effects on the unsteady flow behavior related to irregular blade spacing, blade number and radial distance between the impeller periphery and the volute tongue have been studied. The numerical simulations of the unsteady flow have been carried out using Computational Fluid Dynamics tools (CFD) based on Unsteady Reynolds Averaged Navier Stokes approach (URANS). The sliding mesh technique has been applied at the interfaces between the rotating and stationary zones in order to model the blades' motion relative to the volute casing. The study is focused on the unsteadiness induced by the aerodynamic interaction between the volute and the rotating impeller blades. In order to predict the acoustic pressure at far field, the unsteady flow variables provided by the CFD calculations (pressure and velocity fluctuations acquired upon the surfaces of the rotating blades) have been used as inputs in the Ffowcs Williams-Hawkings equations (FW-H). Using this model, the acoustic pressure has been computed at the fan exit duct. The experimental part of this work concerns measurement of aerodynamic performance of the fans using a test bench built according to ISO 5801 [1] standard. In addition to this, pressure microphones have been flush-mounted on the volute tongue surface in order to measure the wall pressure fluctuations. The sound pressure level (SPL) measurements have been carried out in an anechoic room in order to remove undesired noise reflections. Finally, the numerical results have been compared with the experimental measurements and a correlation between the wall pressure fluctuations and the far field noise signals has been found.
机译:本研究的目的是评估设计参数对前向离心风扇的不稳定流动的影响及其对流动性行为的影响。为此,在具有各种几何参数的四个离心叶轮上进行了数值和实验研究。相同的蜗壳壳已经用于研究这些风扇。研究了对叶轮周边和蜗壳之间的不规则叶片间距,叶片数和径向距离相关的不稳定流动的影响。非定常流量的数值模拟已经使用基于不稳定的Reynolds的计算流体动力学工具(CFD)进行了平均的Navier Stokes方法(Urans)。滑动网格技术已经应用于旋转和固定区域之间的界面,以便相对于蜗壳壳体模拟叶片运动。该研究专注于由蜗壳和旋转叶轮叶片之间的空气动力学相互作用引起的不稳定性。为了预测远场的声压,由CFD计算提供的不稳定流量(在旋转刀片的表面上获取的压力和速度波动)已被用作FFOWS Williams-Hawkings方程中的输入(FW-H. )。使用该模型,在风扇出口管道上计算了声压。这项工作的实验部分涉及使用根据ISO 5801 [1]标准的测试台的风扇的空气动力学性能。除此之外,压力麦克风已经嵌入蜗壳舌面上,以测量壁压波动。在一个空中空间中已经执行声压水平(SPL)测量,以消除不期望的噪声反射。最后,已经将数值结果与实验测量结果进行了比较,并且已经找到了壁压波动与远场噪声信号之间的相关性。

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