基于深度平均薄膜模型的落波膜预测及其在航空发动机轴承室中的应用

K. Singh, A. Nicoli, R. Jefferson-Loveday, S. Ambrose, P. Paleo Cageao, K. Johnson, S. Mouvanal, J. Cao, A. Jacobs
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引用次数: 1

摘要

在本研究中,采用深度平均薄膜模型,即欧拉薄膜模型(ETFM),研究了在上游强制激励下波浪状薄膜的演化过程。由于控制方程的深度平均,可以在壁面法线方向上采用粗网格。因此,与完全解析薄膜相比,该模型计算效率高,因此对工业模拟非常有利。在下降波状膜的情况下,膜厚和膜速度是紧密耦合的。为了提高模型的精度和鲁棒性,采用了同时求解深度平均连续性方程和动量方程的耦合求解器,并对表面张力项的曲率进行了平滑处理。实现的模型为显式和隐式时间公式提供了稳定的解决方案。通过与实验结果和高保真VOF仿真的比较,对新实现的ETFM模型的性能进行了评价。新实现的模型在预测自由表面膜分布方面是可靠的。与高保真VOF模拟相比,它的计算成本要低150到415倍。将该模型成功地应用于某典型航空发动机轴承室进气道波纹膜的预测。该模型能够捕获静态刀片(轴承室入口的一部分)前表面的关键流动物理,并且与刀片上油流的实验可视化非常吻合。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Predictions of Falling Wavy Films Based on the Depth Averaged Thin Film Model and Its Application to Aeroengine Bearing Chamber
In the present study, the evolution of a falling wavy film with upstream forced excitation is investigated using the depth averaged thin film model, known as Eulerian Thin Film Model (ETFM). Because of the depth averaging of the governing equations, coarse grids can be used in the wall normal direction. Consequently, this model is computationally efficient when compared to fully resolving thin films and hence highly advantageous for industrial simulations. In the case of a falling wavy film, film thickness and film velocity are closely coupled. A coupled solver that solves the depth averaged continuity and momentum equations simultaneously has been implemented with the provision to apply smoothing to the curvature of surface tension term to improve the accuracy and robustness of the model. The implemented model provides a stable solution for explicit as well as implicit temporal formulations. The performance of the newly implemented ETFM model is evaluated by comparing numerical results with experimental measurements and high-fidelity VOF simulations. The newly implemented model is found to be reliable in predicting free surface film profiles. It is 150 to 415 times computationally cheaper when compared to high-fidelity VOF simulations. The implemented and validated model is successfully used to predict a wavy film on the inlet of a representative aeroengine bearing chamber. The model is able to capture key flow physics on the front face of a static insert, which forms part of the bearing chamber inlet, and agrees well with experimental visualization of oil flow on the insert.
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