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EXPERIMENTAL AND NUMERICAL ANALYSIS OF R744 EJECTORS OPERATED IN PART LOAD

机译:R744喷射器在部分载荷下的实验与数值分析

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This paper presents an experimental and a numerical investigation of R744 ejectors. For different operatingrnconditions, several experimental tests were carried out. The experimental results show a strong correlationrnbetween the mass entrainment ratio and pressure lift. The achieved ejector efficiencies reach from 22% to 33%rnfor the pressure lifts between 3.5 bar and 9 bar. The experimental data was used to validate the numericalrnsimulations. For a detailed investigation, three cases were chosen. To perform the simulations, thernhomogeneous equilibrium model (HEM) and the k-ε RNG turbulence model were used. The contour plots ofrnMach number, turbulent kinetic energy and pressure as well as plots along the flow path reveal the flow patternrndetails. The approach of a sectional and cumulative increase in entropy rate was used to investigate local andrnglobal flow irreversibilities. The results show that the diffuser section contributes little to the overall increasernin entropy rate with values from 10.12% up to 28.73% and that the diverging part of the motive nozzlerncontributes a considerable amount more with values from 33.3% up to 37.77%. It can be concluded thatrnchanges in turbulence along the mixer and diffuser are the main reason for the different efficiencies.
机译:本文介绍了R744喷射器的实验和数值研究。针对不同的运行条件,进行了几次实验测试。实验结果表明,质量夹带率与升压之间存在很强的相关性。对于3.5 bar至9 bar的压力提升,实现的喷射器效率达到22%至33%rn。实验数据用于验证数值模拟。为了进行详细调查,选择了三个案例。为了执行模拟,使用了均质平衡模型(HEM)和k-εRNG湍流模型。马赫数,湍动能和压力等高线图以及沿流路的图揭示了流型细节。使用熵的分段和累积增加的方法来研究局部和全局流动的不可逆性。结果表明,扩散段对总熵率的贡献很小,从10.12%到28.73%不等,动力喷嘴的发散部分贡献更大,从33.3%到37.77%。可以得出结论,沿着混合器和扩散器的湍流变化是效率不同的主要原因。

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