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EFFECT OF TURBULENCE DAMPING IN VOF SIMULATION OF AN AERO-ENGINE BEARING CHAMBER

机译:湍流阻尼在航空发动机轴承腔室VOF模拟中的作用

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In aero-engine bearing chambers, the modelling of shear-driven oil films with the Volume of Fluid method poses significant challenges linked with the need to accurately capture the gas-liquid interaction at the free surface. Typically, the modelling of the latter relies on a dedicated scalable source term, which is activated locally at the interface between the phases. Our latest published work focused on the application of a popular term of this kind known as turbulence damping, and raised some questions on the suitability of the choice of a high value for its scaling factor. In this paper, a lower turbulence damping factor value is proposed. The new results are evaluated against both the reference bearing chamber experimental data and the previously published numerical data. The results highlight that a transition from shear-driven to gravity-driven flow conditions takes place once the damping factor value is decreased. Considering the impact this may have on the accuracy of the numerical predictions, a strategy is proposed towards a better-informed choice of the turbulence damping factor, in particular when the expected flow conditions are unknown.
机译:在航空发动机轴承室中,使用“流体体积”方法对剪切驱动的油膜进行建模提出了与精确捕获自由表面上的气液相互作用的需求相关的重大挑战。通常,后者的建模依赖于专用的可伸缩源术语,该术语在阶段之间的接口处本地激活。我们最新发表的工作着眼于这种流行术语,即湍流阻尼的应用,并提出了对其比例系数选择高值是否合适的问题。本文提出了一种较低的湍流阻尼系数值。对照参考轴承室实验数据和先前发布的数值数据对新结果进行了评估。结果表明,一旦减小阻尼系数值,就会发生从剪切驱动流向重力驱动流的过渡。考虑到这可能对数值预测的准确性产生影响,因此提出了一种策略,以更明智地选择湍流阻尼因子,特别是在预期流动条件未知的情况下。

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