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Wall-Modelled Large-Eddy Simulation of a hot Jet-In-Cross-Flow with turbulent inflow generation

机译:具有湍流流入的热流横流的壁式大涡模拟

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摘要

Hot jets-in-cross-flow are frequently encountered in aeronautics and the accurate estimation of the wall temperature in the jet wake is crucial during the early design of a new aircraft. However, common two-equation RANS models fail at estimating the wall temperature in the jet wake. The use of Large-Eddy Simulation, which seems to be a promising solution at first sight, is not applicable due to its prohibitive computational cost on such large Reynolds number wall-bounded flows. For an affordable cost, we propose a strategy which consists in: reducing the computational domain to a small region around the phenomenon of interest (RANS-LES embedded approach), perform a Wall-Modelled Large-Eddy Simulation (WMLES) in the reduced domain and generate a turbulent inflow at the reduced domain inlet. The test case selected is a hot Jet-In-Cross-Flow experimentally studied by Albugues (2005) [1]. We simulate the real geometry of the wind-tunnel model, which imposes strong constraints on the inflow generation and numerical method. It is shown that an advanced inflow generation, combining a stochastic velocity fluctuation injection and a dynamic forcing term (Laraufie et al., 2011) [17], is mandatory to obtain a realistic turbulent flow upstream of the jet. In the jet wake, the wall temperature estimated by the WMLES agrees well with the experimental measurements.
机译:交叉流热喷气机在航空中经常遇到,在新飞机的早期设计过程中,准确估算喷气机尾流中的壁温至关重要。但是,常见的两方程式RANS模型无法估算射流尾流中的壁温。乍看之下,大涡模拟的使用似乎是一个有前途的解决方案,但由于其在如此大的雷诺数边界壁流上的计算成本过高,因此不适用。为了获得可承受的成本,我们提出了一种策略,该策略包括:将计算域缩小到感兴趣现象周围的小区域(RANS-LES嵌入式方法),在缩减域中执行墙模型大涡模拟(WMLES)并在缩小域入口处产生湍流。选择的测试用例是Albugues(2005)[1]实验研究的热射流。我们模拟了风洞模型的实际几何形状,这对流入量和数值方法施加了强大的约束。结果表明,将随机速度波动注入和动态强迫项结合起来进行先进的入流生成(Laraufie等人,2011)[17],对于获得射流上游的逼真的湍流是必不可少的。在喷气尾流中,由WMLES估算的壁温与实验测量值非常吻合。

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