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Effect of jet's inlet temperature field excitation on heat transfer by turbulent impinging jet: an investigation based on large eddy simulations

机译:喷射入口温度场励磁对湍流撞击射流传热的影响:基于大涡模拟的研究

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In this paper, the effect of inlet temperature field excitation on the impinging jet heat transfer has been investigated using Large Eddy Simulation (LES). There are several experimental and numerical studies on the inlet velocity field excitations of a turbulent impinging jets, however, the temperature field excitation has not been done before. The Reynolds number (Re) of the jet is 23000 and dimensionless jets outlet to target wall distance is two. To ensure a good quality of the simulation, the non-excited jet is simulated first. From the simulation, it is found that the Strouhal number corresponding to the preferred mode of the unexcited jet is 0.328. The jets inlet temperature field is then excited with three different frequencies. The heat transfer enhancement is found to be possible with inlet temperature field excitation; however, the improvement depends crucially on the excitational frequencies.
机译:本文采用大涡模拟(LES)研究了入口温度场激发对撞击喷射热传递的影响。 有几个关于湍流撞击喷射器的入口速度场激发的实验性和数值研究,然而,在之前未完成温度场励磁。 射流的雷诺数(RE)是23000,靶壁距离的无量纲射流出口是两个。 为了确保良好的模拟质量,首先模拟非激励射流。 从模拟中,发现与未开发射流的优选模式对应的斯特鲁姆数为0.328。 然后用三种不同的频率激发喷气机入口温度场。 发现热传递增强有可能与入口温度励磁有可能; 然而,改进依赖于兴奋频率。

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