Experiments on supercritical flow instability in two vertical parallel channels

I. Singh, V. Chatoorgoon
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引用次数: 1

Abstract

Very limited experimental data on supercritical flow instability is present in the literature. To enrich this limited database and to further the understanding of supercritical flow instability, an experimental study was conducted using two vertical parallel channels with supercritical CO2. A total of 7 experimental cases were performed with a system pressure range of 8.25 – 9.1MPa and inlet temperatures 0.5 – 10.05 °C. The channel inlet temperature and system pressure were held constant and the input power was increased gradually until mass flow oscillations commenced. The distribution of mass flow rate in the channels with input power increase was examined. Initially, at low input power, the flow rate in the channels was almost equal, with an increase in input power, it got distributed in channels and become asymmetric, and with the further input power increase, it started oscillating 180 °out-of-phase. The results for seven experimental cases are presented and these would be useful for code validation purposes.
两个垂直平行通道内超临界流动不稳定性实验
文献中关于超临界流动不稳定性的实验数据非常有限。为了丰富这个有限的数据库,并进一步了解超临界流动的不稳定性,使用两个垂直平行通道进行了超临界CO2的实验研究。共进行了7个实验,系统压力范围为8.25 ~ 9.1MPa,进口温度为0.5 ~ 10.05℃。通道入口温度和系统压力保持不变,输入功率逐渐增加,直到质量流量振荡开始。研究了质量流率随输入功率增大的分布规律。最初,在低输入功率时,通道内的流量基本相等,随着输入功率的增加,流量在通道内分布,变得不对称,随着输入功率的进一步增加,流量开始180°的反相振荡。给出了七个实验案例的结果,这些结果将对代码验证有用。
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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