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Effect of Inflow Turbulence on Noise in Low Speed Centrifugal Fans - A Frequency Domain Approach

机译:流入湍流对低速离心风机噪声的影响 - 一种频域方法

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High axial velocities and low radial velocities at the inlet section of the impeller have been found to cause a separation region over approximately one-third of the impeller width. TIx high turbulent intensities in this region are a strong function of the axial distance into the inlet and circumferential position. The two fluctuating velocity components a’ and v’ are always partially correlated but the extent of coherency varies with location. This partial conelation indicates that the two components are interacting and collectively form a complex source region. The broadband energy levels in the velocity power slwctra are higher in the separation region than regions further into the inlet, by two orders of magnitude, showing higher levels of turbulent energy. The partial coherence functions between the fluctuating velocity components and SPL have been found to be very low at all the locations due to the interactions of the turbulent fluctuations with one blade passage not being correlated with the interactions of other blade passages. In fact, the radiated SPL is a cumulative effect of turbulence in many such passages. Farther, low coherency is also doe to the fact that the separation region is a complex, interactive source region instead of several independent warces of noise. The coherent input power spectrum calculated at a particular location in the fan inlet yields a measure. of the energy in the velocity fluctuations that affects the SPL. Therefore, locations having higher turbulence arc shown to be sources of broadband noise. These results imply that the broadband noise could be reduced If the size and strength of the separation region could be reduced, the turbulence in the inlet decreased, and the flow through the scroll and cat-off made more uniform. It was, therefore, logical to consider the use of a suitable flow turning device or an inlet guide vane (IGV) to direct the flow smoothly through the impeller blades. The performance of the IGV has been evaluated in another paper by Vadari et al. 161.
机译:已经发现叶轮的入口部分处的高轴向速度和低径向速度,以使分离区域在大约三分之一的叶轮宽度上。该区域的Tix高湍流强度是轴向距离进入入口和圆周位置的强功能。两个波动速度分量A'和V'始终是相关的,但是一致性的程度随位置而变化。这种部分锥形表明,两个组分是相互作用的并且共同形成复杂的源区。分离区域的速度功率SLWCTRA中的宽带能量水平高于进一步进入入口的区域,其数量级较高,显示出更高水平的湍流能量。由于湍流波动的相互作用与一个刀片通道与其他叶片通道的相互作用相关的湍流波动的相互作用,已经发现波动速度分量和拼接之间的部分相干功能在所有位置处非常低。实际上,辐射的SPL是许多这种通道中的湍流的累积效果。更远,低相干性也是将分离区域是复合的交互源区域而不是几种独立的噪声的噪声。在风扇入口处的特定位置计算的相干输入功率谱产生措施。影响SPL的速度波动中的能量。因此,具有更高的湍流弧的位置被示出为宽带噪声的源。这些结果意味着如果可以减小分离区域的尺寸和强度,则可以减小宽带噪声,入口中的湍流减小,并且流过涡旋和尖端的流动使得更均匀。因此,考虑使用合适的流量转动装置或入口导向叶片(IGV)是逻辑的,以平稳地穿过叶轮叶片。通过Vadari等人在另一篇论文中评估了IGV的性能。 161。

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