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The Problem of Accounting for Heat Exchange between the Flow and the Flow Part Surfaces When Modeling a Viscous Flow in Low-Flow Stages of a Centrifugal Compressor

机译:在离心式压缩机的低流量级模型时流动与流动部分表面之间的热交换的汇总的问题

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摘要

In this paper, we review the problem of accounting for heat exchange between the flow and the flow part surfaces when creating a calculation model for modeling the workflow process of low-flow stages of a centrifugal compressor using computational fluid dynamics (CFD). The objective selected for this study was a low-flow intermediate type stage with the conditional flow coefficient Փ = 0.008 and the relative width at the impeller exit b2/D2 = 0.0133. We show that, in the case of modeling with widespread adiabatic wall simplification, the calculated temperature in the gaps between the impeller and the stator elements is significantly overestimated. Modeling of the working process in the flow part was carried out with a coupled heat exchanger, as well as with simplified accounting for heat transfer by setting the temperatures of the walls. The gas-dynamic characteristics of the stage were compared with the experimental data, the heat transfer influence on the disks friction coefficient was estimated, and the temperature distributions in the gaps between disks and in the flow part of the stage were analyzed. It is shown that the main principle when modeling the flow in low-flow stage is to ensure correct temperature distribution in the gaps.
机译:在本文中,我们在使用计算流体动力学(CFD)创建用于建模离心压缩机的低流量级的工作流程过程时,审议流动部分表面之间的热交换的问题。为该研究选择的目的是一种低流量中间型阶段,条件流量系数փ= 0.008,叶轮出口处的相对宽度B2 / D2 = 0.0133。我们表明,在用广泛的绝热墙简化建模的情况下,叶轮和定子元件之间的间隙中的计算温度显着高估。通过耦合的热交换器进行流动部分中的工作过程的建模,以及通过设置壁的温度来进行传热的简化算法。将阶段的气体动力学特性与实验数据进行比较,估计了对磁盘摩擦系数的传热影响,并且分析了盘之间的间隙和阶段流动部分之间的温度分布。结果表明,在低流量级模型流动时的主要原理是确保空隙中的正确温度分布。

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