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NUMERICAL PREDICTION OF NOISE FROM THE INTERNAL FLOW IN A CENTRIFUGAL BLOWER

机译:离心风机内部流动噪声的数值预测。

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The noise generated from the internal flow in a centrifugal blower was computed by computational aero-acoustics (CAA). The sound sources were obtained by computational fluid dynamics (CFD), using large-eddy simulation (LES) to compute the turbulent flow in the centrifugal blower. The computed sound pressure level (SPL) with sound source from coarse mesh LES is overpredicted, while the computed SPL with sound source from fine mesh LES agrees fairly well with the experimental data. The peak of SPL at blade passing frequency (BPF) of 600 Hz can be somewhat captured by CAA with sound source from fine mesh CFD. However, due to the short computational time, the frequency resolution is not fine in CAA with sound source from fine mesh CFD, which may be the reason of underprediction of the peak value at BPF. Fluid forces acting on the impeller at the plane perpendicular to the axial direction play important role on the predicted SPL at BPF.
机译:离心鼓风机内部流动产生的噪声通过计算航空声学(CAA)进行计算。声源是通过计算流体动力学(CFD),使用大涡流模拟(LES)计算离心鼓风机中的湍流来获得的。用粗网格LES的声源计算出的声压级(SPL)被过高预测,而用细网格LES的声源计算出的声压级与实验数据非常吻合。带有细网CFD声源的CAA可以在600 Hz的叶片通过频率(BPF)处获得SPL的峰值。但是,由于计算时间短,在带有声源来自细网格CFD的CAA中,频率分辨率不佳,这可能是BPF峰值预测不足的原因。在垂直于轴向方向的平面上作用在叶轮上的流体力在BPF的预测SPL中起着重要作用。

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