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气-水鼓泡塔的计算流体动力学模拟:罗聚并参数和破碎核的影响

CFD Simulations of an Air-Water Bubble Column: Effect of Luo Coalescence Parameter and Breakup Kernels.

作者信息

Syed Alizeb Hussain, Boulet Micael, Melchiori Tommaso, Lavoie Jean-Michel

机构信息

Industrial Research Chair on Cellulosic Ethanol and Biocommodities, University of SherbrookeSherbrooke, QC, Canada.

EnerkemSherbrooke, QC, Canada.

出版信息

Front Chem. 2017 Sep 21;5:68. doi: 10.3389/fchem.2017.00068. eCollection 2017.

DOI:10.3389/fchem.2017.00068
PMID:28983480
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC5613131/
Abstract

In this work, CFD simulations of an air-water bubbling column were performed and validated with experimental data. The superficial gas velocities used for the experiments were 0.019 and 0.038 m/s and were considered as an homogeneous regime. The former involves simpler physics when compared to a heterogeneous regime where the superficial velocities are higher. In order to simulate the system, a population balance model (PBM) was solved numerically using a discrete method and a closure kernels involving the Luo coalescence model as well as two different breakup models: Luo's and Lehr's. For the multi-phase calculations, an eulerian framework was selected and the interphase momentum transfer included drag, lift, wall lubrication, and turbulent dispersion terms. A sensitivity analysis was performed on a Luo coalescence kernel by changing the coalescence parameter () from 1.1 to 0.1 and results showed that the radial profiles of gas holdup and axial liquid velocity were significantly affected by such parameter. From the simulation results, the main conclusions were: (a) A combination of the Luo coalescence and Luo breakup kernels (Luo-Luo) combined with a decreasing value of improves the gas holdup profiles as compared to empirical values. However, at the lowest value of investigated in this work, the axial liquid velocity deteriorates with regards to experimental data when using a superficial gas velocity of 0.019 m/s. (b) A combination of the Luo coalescence and Lehr breakup models (Luo-Lehr) was shown to improve the gas holdup values with experimental data when compared to the Luo-Luo kernels. However, as decreases, the Luo-Lehr models underestimate the axial liquid velocity profiles with regards to empirical values. (c) A first and second order numerical schemes allowed predicting similar radial profiles of gas holdup and axial liquid velocity. (d) The mesh sensitivity results show that a 3 mm mesh size can be considered as reasonable for simulating experimental data. (e) The inclusion of wall lubrication parameter was found to be significant, although only when using finer meshing. In addition, it allows an improvement of the axial liquid velocity at the core of the bubble column.

摘要

在这项工作中,对气-水鼓泡塔进行了计算流体动力学(CFD)模拟,并与实验数据进行了验证。实验中使用的表观气速为0.019和0.038 m/s,被视为均相流型。与表观气速较高的非均相流型相比,前者涉及更简单的物理过程。为了模拟该系统,使用离散方法对种群平衡模型(PBM)进行了数值求解,并采用了包含Luo聚并模型以及两种不同破碎模型(Luo模型和Lehr模型)的封闭核。对于多相计算,选择了欧拉框架,相间动量传递包括曳力、升力、壁面润滑和湍流扩散项。通过将聚并参数()从1.1更改为0.1,对Luo聚并核进行了敏感性分析,结果表明,该参数对气体持液率和轴向液体速度的径向分布有显著影响。从模拟结果得出的主要结论如下:(a)与经验值相比,Luo聚并核和Luo破碎核(Luo-Luo)的组合以及逐渐减小的 值改善了气体持液率分布。然而,在本工作中研究的最低 值下,当表观气速为0.019 m/s时,轴向液体速度相对于实验数据有所恶化。(b)与Luo-Luo核相比,Luo聚并模型和Lehr破碎模型(Luo-Lehr)的组合在与实验数据比较时提高了气体持液率值。然而,随着 值的减小,Luo-Lehr模型相对于经验值低估了轴向液体速度分布。(c)一阶和二阶数值格式能够预测相似的气体持液率和轴向液体速度径向分布。(d)网格敏感性结果表明,3 mm的网格尺寸对于模拟实验数据可以认为是合理的。(e)发现壁面润滑参数的纳入是显著的,尽管仅在使用更精细的网格划分时如此。此外,它可以改善鼓泡塔核心处的轴向液体速度。

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