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Experimental measurement and CFD simulation on the hydrodynamics of an internal-loop airlift reactor

机译:内环空运反应堆流体动力学的实验测量和CFD仿真

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This paper concerns with the experimental measurement and computational fluid dynamics simulation on local hydrodynamics of a gas-liquid internal-loop airlift reactor. The aim of this work is to study the sensitivity of the drag models and the significance of considering the lift force on the predictive accuracy of the simulation. The experimental analysis was carried out using laser Doppler anemometry at three different heights (i.e. Y = 0.20 m, 0.30 m and 0.38 m) across the riser and downcomerat volumetric flow rate of 0.30 m3/h to provide validation for the simulation results. A transient three-dimensional gasliquid internal-loop airlift reactor was carried out using FLUENT 16.2 by implementing the two-fluid model approach. The Eulerian-Eulerian multiphase and standard κ-ε dispersed turbulence model wereemployed in this study. Results suggest that the spherical drag model performed poorly and that the drag model governed by Rayleigh-Taylor shows promising accuracy in the prediction of overall mean axial liquid velocity. On the other hand, the consideration of lift model shows slightly improvement in accuracy. These findings may serve as a guidance for future scale-up and design of airlift reactor studies
机译:本文涉及对燃气液内环空运反应器的局部流体动力学的实验测量和计算流体动力学模拟。这项工作的目的是研究阻力模型的敏感性以及考虑提升力对模拟预测精度的重要性。在三种不同高度(即y = 0.20m,0.30m和0.38m)上使用激光多普勒式风皮测量法进行实验分析,并在提升管和下变量体积流速为0.30m 3 / h以提供仿真结果的验证。通过实施双流体模型方法,使用流畅的16.2进行瞬时三维气体内环空气梯子。本研究中播种了欧拉欧洲多相和标准κ-ε分散湍流模型。结果表明,球形阻力模型表现不佳,并且瑞利泰勒管辖的阻力模型在总体平均轴向液体速度的预测中显示了有希望的准确性。另一方面,考虑升力模型的准确性略微提高。这些调查结果可以作为未来扩大和设计空运反应堆研究的指导

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