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Heat transfer characteristics of fan-shaped hole effusion cooling for a constant hole exit width - Numerical simulation and experimental validation

机译:恒孔出口宽度的扇形空穴积液冷却传热特性 - 数值模拟和实验验证

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摘要

In order to study the effusion cooling mechanism of fan-shaped holes with a constant exit width, numerical simulations and the corresponding experimental verifications are carried out on a flat plate with ten rows of fan shaped film cooling holes. The entrance diameter and the exits width of the cooling holes are kept at D and 3D, respectively. While the thickness of the flat plate is kept at 10D/3. The holes are arranged in a staggered pattern with the constant stream-wise and span-wise spacing of 8.5D and 6.5D, respectively. The hole inclination angles of 20 degrees, 25 degrees and 30 degrees, the hole expansion angles of 10 degrees and 13 degrees, and the blowing ratios ranged from 0.5 to 7.5 are considered. Shear stress transport k - omega turbulence model is adopted for the numerical simulation. The numerical results are validated experimentally using thermo-chromic liquid crystal technology, showing good agreements. Through the simulation, the effects of the inclination angle and the expansion angle of the holes as well as the blowing ratio on the film cooling effectiveness are analyzed and discussed in detail. A correlation for the area averaged effectiveness is developed for the prediction of row-by-row superposition effects of effusion cooling with fan-shaped holes.
机译:为了研究具有恒定出口宽度的扇形孔的积液冷却机构,在具有十排风扇形膜冷却孔的平板上进行数值模拟和相应的实验验证。冷却孔的入口直径和退出宽度分别保持在D和3D。虽然平板的厚度保持在10d / 3。孔以交错的图案布置,具有恒定的流动和跨越8.5d和6.5d的横向间距。孔倾斜角20度,25度和30度,空穴膨胀角为10度,13度,并且吹出比率范围为0.5至7.5。用剪切应力运输K - Omega湍流模型用于数值模拟。使用热铬液晶技术实验验证数值结果,显示出良好的协议。通过模拟,分析倾斜角度和孔的膨胀角的效果以及吹膜冷却效果的吹出比率。开发了对面积平均效果的相关性,用于预测扇形孔的逐行叠加效果的预测。

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