椭圆钝体气动特性有效预测的深度学习技术

W. M. U. Weerasekara, H. M. C. D. B. Gunarathna, W. A. K. P. Wanigasooriya, T. P. Miyanawala
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引用次数: 0

摘要

由于钝体的流动行为难以预测,特别是在高雷诺数下,预测钝体的气动力仍然是一项具有挑战性的任务。用实验方法来确定空气动力系数既昂贵又费时。同时,根据流动特性的复杂性,使用数值技术也需要相当大的计算成本和时间。研究的重点是开发一种有效的深度学习技术来预测给定展弦比和给定流动条件下作用在椭圆钝体上的气动力系数。采用精确的全阶模型,对从涡旋碎裂开始到亚临界区域边缘的流动条件下,几种展弦比的阻力系数和升力系数进行了采集。指定区域将提供瞬态流动行为,因此升力系数将以均方根值表示,阻力系数以平均值表示。随着流动特性和涡流粉碎频率的变化,需要选择合适的湍流模型、优化的流域离散化和时间步长来获得准确的结果。流动模拟主要采用非定常Reynolds average Navier-Stokes Equations (URANS)模型和Detached Eddy simulations (DES)模型。通过与现有实验结果的比较,探讨了在特定流型中使用不同湍流模型的有效性。在较低的雷诺数下,特定物体的气动力系数只取决于雷诺数。但是在一定的雷诺数之后,气动力除了依赖于雷诺数之外,还依赖于马赫数。因此,对于较高的雷诺数,记录相同雷诺数的多个马赫数的气动力系数,并将其馈入神经网络。随着机器学习和神经网络建模的发展,许多领域已经培育并创造了有效和高效的技术来简化复杂的功能和活动。我们的目标是通过创建一个深度神经网络工具来预测给定宽高比下椭圆钝体的阻力和升力系数,并使其精度达到可接受的水平,从而减轻计算流体动力学领域的复杂性。研究人员开发了深度神经网络工具来预测各种流动状况,并取得了足够的精度和令人满意的计算成本降低。在我们提出的深度学习神经网络中,我们选择将输入作为几何设置和具有经过验证的阻力和升力系数的流动条件来建模网络。该模型将通过对输入执行卷积操作将必要的流特征提取到过滤器中。我们的主要目标是创建一个深度学习的神经网络工具,在可接受的精度范围内预测目标值,同时最小化计算成本。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Deep Learning Techniques for Effective Prediction of Aerodynamic Properties of Elliptical Bluff Bodies
Predicting aerodynamic forces on bluff bodies remains to be a challenging task due to the unpredictable flow behavior, specifically at higher Reynolds numbers. Experimental approaches to determine aerodynamic coefficients could be costly and time consuming. In the meantime, use of numerical techniques could also require a considerable computational cost and time depending on complexity of the flow behavior. The research focusses on developing an effective deep learning technique to predict aerodynamic force coefficients acting on elliptical bluff bodies for a given aspect ratio and given flow condition. Collecting data for drag and lift coefficients of several aspect ratios for flow conditions starting from onset of vortex shredding to verge of subcritical region is conducted by an accurate full order model. The specified region will provide a transient flow behavior and thus lift coefficient will be represented in terms of root mean square value and drag coefficient in terms of a mean value. With variations in flow behavior and vortex shredding frequencies, it requires to select an appropriate turbulence model, optimum discretization of fluid domain and time step to obtain an accurate result. Flow simulations are conducted primarily using Unsteady Reynolds Averaged Navier-Stokes Equations (URANS) model and Detached Eddy Simulations (DES) model. Effectiveness in using different turbulence models for specified flow regimes are also explored in comparison to available experimental results. At lower Reynolds numbers, aerodynamic force coefficients for a specified body will only depend on Reynolds number. But after a certain specific Reynolds number, aerodynamic forces are dependent on the Mach number in addition to Reynolds number. Therefore, for higher Reynolds numbers, aerodynamic force coefficients are recorded for multiple Mach numbers with same Reynolds number and will be fed to the neural network. With the development of the machine learning and neural network modelling, many of the fields have nourished and created effective and efficient technologies to ease complex functions and activities. Our goal is to ease the complexity in the computational fluid dynamic field with a deep neural network tool created to predict drag and lift coefficient of elliptical bluff bodies for a given aspect ratio with an acceptable accuracy level. Researchers have developed deep neural network tools to predict various flow conditions and have succeeded with sufficient accuracy and a satisfying reduction of computational cost. In our proposed deep learning neural network, we have chosen to model the network with inputs as the geometry setup and the flow conditions with validated drag and lift coefficients. The model will extract the necessary flow features into filters with the convolution operation performed on the inputs. Our main directive is to create a deep learned neural network tool to predict the target values within an acceptable range of accuracy while minimizing the computation cost.
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