4.6 Article

Assessment of the impact of bubble size modelling in CFD simulations of alternative bubble column configurations operating in the heterogeneous regime

期刊

CHEMICAL ENGINEERING SCIENCE
卷 186, 期 -, 页码 88-101

出版社

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.ces.2018.04.025

关键词

CFD; Single bubble size models; MUSIG; Bubble column; Airlift column; Churn turbulent flow

资金

  1. East China University of Science and Technology
  2. ARC Training Centre for the Australian Food Processing Industry in the 21st Century [IC140100026]

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Modelling bubble columns operating in the churn turbulent flow regime is a considerable challenge due to their complex and transient behaviour. A key modelling decision is how best to model the bubble size distribution, with a range of approaches existing from the relatively simple option of using a single, representative bubble size to more complex population balance approaches. In this comparative study, we have examined various approaches (i.e. constant and variable single bubble size models, dual bubble size models, and both homogeneous and inhomogeneous MUSIG models). Model predictions were compared with experimental data from three different configurations of a pilot-scale column (0.39 m in diameter and 2 m in height) operated at industrially relevant superficial gas velocities of 0.16 and 0.25 m s(-1). The single bubble size models gave reasonable agreement with experimental data for the 'symmetrical' configuration, with the variable bubble size model having the major advantage of providing acceptable predictions of the mean bubble size (without this having to be provided as a model input). Implementation of multiple bubble size models did not lead to any substantial improvement in the modelling fit with the experimental data, leading to the inescapable conclusion that the standard bubble breakup and coalescence kernels proposed in the literature do not adequately describe bubble transformations taking place under heterogeneous operating conditions. (C) 2018 Elsevier Ltd. All rights reserved.

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