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EXPERIMENTAL AND NUMERICAL INVESTIGATION OF THE UNSTEADY FLOW FIELD AND TONE GENERATION IN AN ISOLATED CENTRIFUGAL FAN IMPELLER

机译:分离式离心风机叶轮内非定常流场和音调产生的实验和数值研究

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In spite of low circumferential Mach number the sound of iso-lated centrifugal fan impellers is sometimes dominated by distinctive tones at blade passing frequency (BPF) and integer multiples. This paper reports on an experimental and numerical investigation in-tended to unveil the tone generating mechanism. The sound spectra from three impellers operating at a large range of speed were meas-ured and decomposed into Strouhal and Helmholtz number dependent functions. This led to the preliminary conclusion that the BPF related tones are exclusively flow-induced. Based on hot-wire and blade pressure fluctuation measurements and a subsequent correlation analysis, coherent flow structures different from the one associated with the principal azimuthal flow pattern due to the blades were de-tected. Eventually, numerical three-dimensional unsteady flow simu-lation and experimental flow visualization revealed an inlet vortex. It takes on a helical form, with the vortex core slowly varying its posi-tion with respect to the impeller center. As the blades cut through that quasi-stationary helical vortex they encounter blade force fluctuations producing the BPF tones. The slow spin of the vortex core and the slow variation of vortex strength were identified as the reason for the amplitude modulation of the BPF tone.
机译:尽管马赫数较低,但隔离离心式风机叶轮的声音有时仍以叶片通过频率(BPF)和整数倍的独特音调占主导地位。本文报道了旨在揭示音调产生机理的实验和数值研究。测量了三个以大速度运行的叶轮的声谱,并将其分解为斯特劳哈尔和亥姆霍兹数依赖函数。这导致了一个初步结论,即与BPF相关的音调是完全由流量引起的。基于热线和叶片压力波动测量值以及随后的相关性分析,检测到与叶片引起的与主要方位流模式相关的相干流动结构不同的相干流动结构。最终,数值三维非稳态流动模拟和实验流动可视化揭示了入口涡流。它呈螺旋形,涡旋芯相对于叶轮中心的位置缓慢变化。当叶片穿过准静态螺旋涡旋时,它们会遇到叶片力波动,从而产生BPF音调。涡旋核的缓慢自旋和涡旋强度的缓慢变化被确定为BPF音调幅度的原因。

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