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A comprehensive modeling of choked two-phase flow through short-tube orifices with application to alternative refrigerants HFO-1234yf and HFO-1234ze

机译:短管节流阀的cho流两相流综合模型及其在替代制冷剂HFO-1234yf和HFO-1234ze中的应用

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摘要

Due to the evaporating two-phase flow and the choked-flow condition, numerical analysis of flow through short-tube orifices is a complicated procedure. A comprehensive method for analyzing such flows is the two-fluid model, which does not assume equilibrium between phases. However, in all previous applications of this model, two-phase flow calculations at the entrance and vena contracta regions were eliminated. In this investigation, two additional steps were introduced to improve the accuracy of computations: (1) applying a comprehensive two-fluid model, including the effect of various two-phase flow patterns and the metastability of liquid phase; and (2) performing a two-phase analysis of the evaporating flow through the entrance and vena contracta, which involves simulation of this region as a contraction from the up-stream to the throat, and an expansion from the throat to downstream. Results showed more compatibility with experimental data in comparison with those of previous investigations for predicting the critical flow condition of common refriger antsHFC-134a, HCFC-22, and HFC-410a through short-tube orifices. In addition, the developed numerical scheme was utilized in order to develop selection charts for short-tube orifices based on the common refrigerant HFC-134a and the alternative newly released hydrofluoroolefin refrigerants HFO-1234yf and HFO-1234ze. (C) 2016 Elsevier Ltd and IIR. All rights reserved.
机译:由于蒸发的两相流和节流条件,通过短管孔流的数值分析是一个复杂的过程。用于分析此类流动的一种综合方法是双流体模型,该模型不假定相之间是平衡的。但是,在该模型的所有先前应用中,都消除了入口和腔静脉收缩区域的两相流计算。在这项研究中,引入了两个额外的步骤来提高计算的准确性:(1)应用综合的两流体模型,包括各种两相流模式的影响和液相的亚稳性; (2)对通过入口和腔静脉收缩的蒸发流进行两阶段分析,其中包括模拟该区域从上游到喉部的收缩以及从喉部到下游的膨胀。结果表明,与通过短管孔预测普通制冷剂HFC-134a,HCFC-22和HFC-410a的临界流动条件的先前研究相比,与实验数据的兼容性更高。另外,利用开发的数值方案来开发基于普通制冷剂HFC-134a和新近发布的替代氢氟烯烃制冷剂HFO-1234yf和HFO-1234ze的短管孔选择表。 (C)2016 Elsevier Ltd和IIR。版权所有。

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