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Large Eddy Simulation of Inclined Jet in Cross Flow with Cylindrical and Fan-shaped Holes

机译:带有圆柱孔和扇形孔的错流斜流的大涡模拟

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A large eddy simulation (LES) investigation of the inclined jet in crossflow is presented in this paper. The angle between the hole and the main flow is 35 degrees, which represents a typical film cooling application. Two different geometries, namely the cylindrical hole and the fan-shaped hole, are investigated at a blowing ratio of 0.5, which is a representative value for film cooling. The numerical tool is first validated and then used to study the flow and the film cooling effectiveness of the cooling holes. Both the time averaged and the instantaneous flow characteristics are analyzed. In the time averaged results, the counter-rotating vortex pair has large effects on the mixing of the coolant with the main flow. The instantaneous results show that the mixing of the injected flow with the main flow is highly related to the unsteady coherent vortices. The difference in the cooling effectiveness distribution for the two holes is due to the different coherent vortices. The relationship between the coherent vortices and the temperature distribution is explained in detail. These results show that the vortices distribution at the exit of the hole has important influence on the later development of the hairpin vortices, thus affecting the temperature distribution and the cooling effectiveness.
机译:本文提出了横流中斜射流的大型涡模拟(LES)研究。孔与主流之间的夹角为35度,代表了典型的薄膜冷却应用。研究了两种不同的几何形状,即圆柱孔和扇形孔,其吹塑比为0.5,这是薄膜冷却的代表值。首先验证数值工具,然后将其用于研究冷却孔的流量和薄膜冷却效果。分析了时间平均和瞬时流量特性。在时间平均结果中,反向旋转涡流对冷却剂与主流的混合影响很大。瞬时结果表明,注入流与主流的混合与不稳定的相干涡旋高度相关。两个孔的冷却效率分布的差异是由于不同的相干涡。详细说明了相干涡旋与温度分布之间的关系。这些结果表明,孔出口处的涡流分布对发夹形涡流的后期发展具有重要影响,从而影响了温度分布和冷却效率。

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