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Comparison of Turbulence Models for Single Sphere Simulation Study Under Supercritical Fluid Condition

机译:超临界流体条件下单球仿真研究湍流模型的比较

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摘要

In this paper, the comparison of turbulence models for fluid flow past single sphere under supercritical conditions is reported. Firstly, Dixon et al.’s models [1], which are under non-supercritical conditions, were used as benchmarks to validate the simulated results. Two turbulence models namely RNG k-ε and SST k-ω models parameters were fine-tuned accordingly in order to obtain almost comparable results generated by Dixon et al.’s models [1]. The simulation works were then extended to simulate flow of supercritical carbon dioxide. The second part of this paper, therefore, presents a comparative study of the turbulence models i. e. standard k-ε, RNG k-ε, realizable k-ε and SST k-ω models. This study emphasises on the predictions and evaluations of the velocity profiles at different flow regimes namely recirculation, recovery and near-wake. Simulations were carried out to determine the velocity profiles at subcritical and supercritical conditions by varying Reynolds numbers (2000 and 20,000), pressures (65 and 80 bar) and temperatures (283.15 and 308.15K). Simulation results indicate that the predicted results are consistent with the literature data. Interesting flow features were identified for all the simulations. The results of this study also reveal that the SST k-ω turbulence model was able to better capture the flow characteristics near-wake of the sphere.
机译:本文报道了超临界条件下流体流动流体流动湍流模型的比较。首先,Dixon等人。在非超临界条件下的模型[1]用作基准,以验证模拟结果。两个湍流模型即RNG K-ε和SST k-ω模型参数相应地进行了微调,以便获得Dixon等人生成的几乎可比较的结果。的型号[1]。然后扩展了模拟作品以模拟超临界二氧化碳流。因此,本文的第二部分呈现了对湍流模型I的比较研究。 e。标准k-ε,rng k-ε,可实现的k-ε和SST k-Ω模型。该研究强调了不同流动制度的速度谱的预测和评价,即再循环,恢复和近尾。进行仿真以通过不同的雷诺数(2000和20,000),压力(65和80巴)和温度(283.15和308.15K)来确定亚临界和超临界条件下的速度谱。仿真结果表明预测结果与文献数据一致。所有模拟都识别有趣的流量功能。该研究的结果还揭示了SSTK-ω湍流模型能够更好地捕获球体靠近尾部的流动特性。

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