Numerical investigation of trailing edge flow in centrifugal pump impellers

O. Litfin, A. Delgado
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引用次数: 1

Abstract

In the fields of aerodynamics and turbomachinery trailing edge flows are of great interest as they can substantially affect performance, vibration and sound emission. The present paper discusses the trailing edge and wake flow in centrifugal pump impellers. In the first part of the study the effect of the trailing edge flow on the performance of equiangular impeller blades was investigated by means of 2D steady RANS simulations for a wide range of blade angles and flow coefficients. The effect was quantified by the slip coefficient as a measure for the overall trailing edge flow deflection from the theoretical, inviscid flow through an impeller with an infinite number of blades. For the typical cut-off or knuckle-type trailing edge configuration an attached and a separated flow regime could be identified, mainly depending on the blade angle. Consequently, in the second part of the study, detached-eddy simulations were carried out, revealing the flow structures of the different trailing edge flow regimes in greater detail.
离心泵叶轮尾缘流动的数值研究
在空气动力学和涡轮机械领域中,尾缘流动对性能、振动和声发射有很大的影响,因此引起了人们的极大兴趣。本文讨论了离心泵叶轮的尾缘和尾流。在研究的第一部分中,采用二维定常RANS模拟方法,研究了尾缘流动对等角叶轮叶片性能的影响。这种效应是通过滑移系数来量化的,滑移系数是通过具有无限叶片的叶轮的理论无粘流动的整体尾缘流动偏转的度量。对于典型的截止型或转节型尾缘结构,可以识别出附着型和分离型的流型,这主要取决于叶片角度。因此,在研究的第二部分,进行了分离涡模拟,更详细地揭示了不同后缘流动形式的流动结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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