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A computational investigation of 3-D flow separation in a vaneless diffuser

机译:无叶片扩压器中3-D流动分离的计算研究

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Computational analyses based on the momentum integral (MI) method and a turbulent flow simulation with the low Reynolds-number turbulence model (LRN k-epsilon) were conducted to investigate the 3-D alternating flow separation in a vaneless diffuser at small flow rates. The obtianed numerical results show that the LRN k-epsilon calculation works well in reproducing the reverse flow in the vaneless diffuser, while the MI-method behaves relatively poor although it captures the overall flow pattern correctly. It is clarified that a small gradient in the inlet tangential velocity distribution with respect to diffuser depth is the key factor, which dominates the reverse flow in the vaneless diffuser at small flow rates, as demonstrated in the experiment. And suppression of flow separation could be achieved by an increase in inflow turbulence or by a wall treatment with locally increasing the surface roughness of hub wall where the reverse flow occurs. Comparison indicates agreements in velocity distributions within 3-D boundary layer between the LRN k-epsilon calculation and the experiment are satisfactory.
机译:进行了基于动量积分(MI)方法的计算分析和低雷诺数湍流模型(LRNk-ε)的湍流模拟,以研究小流量无叶扩压器中的3-D交替流分离。强迫的数值结果表明,LRNk-ε计算可很好地再现无叶扩压器中的逆流,而MI方法虽然可正确地捕获总体流型,但其性能相对较差。可以看出,相对于扩压器深度,进口切向速度分布中的小梯度是关键因素,如实验所示,它在小流量下主导了无叶扩压器中的逆流。并且可以通过增加流入湍流或通过在局部地增加发生逆流的轮毂壁的表面粗糙度的壁处理来实现对流分离的抑制。比较表明LRNk-ε计算和实验之间在3-D边界层内的速度分布一致。

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