研究湍流混合层空气动力特性的脱离涡模拟

Trung Dung Nguyen
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引用次数: 0

摘要

湍流混合层是航空工程中经常出现和应用的一种现象。用数值方法研究混合层湍流适合国内条件。大多数研究采用两种数值模拟方法,包括直接数值模拟 DNS 和大涡模拟 LES,而采用分离涡模拟 DES 的研究很少。在本文中,作者使用不断演化的雷诺平均纳维-斯托克斯模拟 RANS 和分离涡模拟 DES 数值模拟方法,提出了一种可以研究湍流相互作用气动特性的数值模拟模型。RANS 用于评估网格的独立性。利用选定的网格,进行了 DES-2D 模型和 DES-3D 模型的计算。用 Matlab 代码处理速度场数据,结果表明平均流动行为与实验结果密切相关,而湍流动能仍有较大误差。POD 和 Q 准则分析表明,在相互作用区域存在一些大的相干结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
DETACHED EDDY SIMULATIONS IN THE STUDY OF AERODYNAMIC CHARACTERISTICS OF THE TURBULENT MIXING LAYER
The turbulent mixing layer is a phenomenon that occurs and has many applications in aeronautical engineering. The study of mixing layer turbulence by the numerical method is suitable under domestic conditions. Two numerical simulation methods are used in most studies including, direct numerical simulation DNS and large eddy simulation LES, while there are very few studies using detached eddy simulation DES. In this article, the authors use numerical simulation methods evolving Reynolds average Navier-Stokes simulation RANS and detached eddy simulation DES to propose a numerical simulation model that allows to study of the aerodynamic characteristics of the turbulent flow interaction. RANS is used to evaluate grid independence. With the selected mesh, two models counting the DES-2D model and the DES-3D model are conducted. Processing velocity field data with Matlab code, the results show that the average flow behavior has closely followed the experimental results, while the turbulent kinetic energy still has a large error. POD and Q-criterion analysis has shown some large coherent structures in the interaction region.
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