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Large eddy simulation of compound angle hole film cooling with hole length-to-diameter ratio and internal crossflow orientation effects

机译:具有孔长度与直径比和内部横流定向效应的复合角孔膜冷却大型涡流模拟

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摘要

Compound angle hole film cooling with varying length-to-diameter ratio and internal crossflow orientations is investigated by large eddy simulation (LES). The film density ratio is 1.5, and the blowing ratio ranges from 0.4 to 1.2. The compound angle of 45 and three length-to-diameter ratios (L/D) from 0.5 to 5 are chosen for the simulations. In addition to the vertical inflow through the plenum, internal crossflow orientations that are perpendicular to and parallel to the mainstream flow are investigated. The prediction accuracy is validated by the reported hydrodynamic data and present film effectiveness data measured by pressure sensitive paint (PSP). Results show that compound angle hole film effectiveness generally shows a decreasing trend as length-to-diameter ratio increases, which is contrary to the cylindrical hole. This is associated with the fact that length-to-diameter ratio influences the in-tube flow behavior, formation of Kelvin-Helmholtz(K-H) structures, and development of single asymmetric main vortex (SAMV). The internal crossflow orientation is demonstrated to have a significant effect on the in tube flow behavior and the film cooling effectiveness. The perpendicular-counter flow and parallel-inline flow cases are found to provide more uniform hole exit velocity distributions than other internal crossflow orientations and vertical inflow case. Also found is that uniform hole exit velocity distribution provides favorable influence on the film effectiveness. (C) 2017 Elsevier Masson SAS. All rights reserved.
机译:通过大涡模拟(LES)研究了具有变化长度至直径比和内部横向取向的复合角孔膜冷却。膜密度比为1.5,吹出比率为0.4至1.2。选择仿真选择0.5至5的45至直径比(L / D)的复合角度。除了通过增压室的垂直流入之外,研究了垂直于主流流动和平行于主流流动的内部横向取向。通过压敏涂料(PSP)测量的报告的流体动力学数据和本膜效能数据验证了预测精度。结果表明,复合角孔膜效果通常表示随着长达直径比增加的趋势降低,与圆柱孔相反。这与直径长度的比率影响管内流行为,形成凯尔文 - 亥姆霍兹(K-H)结构的形成以及单一不对称主涡流(SAMV)的发展有关。对内部交叉流量取向被证明对管道流动行为和薄膜冷却效果具有显着影响。发现垂直计数器流动和平行于线流量壳体提供比其他内部横向取向和垂直流入壳体的更均匀的孔出口速度分布。另外发现是均匀的空穴出口速度分布对薄膜有效性提供了有利影响。 (c)2017年Elsevier Masson SAS。版权所有。

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    Tsinghua Univ Dept Thermal Engn Gas Turbine Inst Beijing 100084 Peoples R China;

    Tsinghua Univ Dept Thermal Engn Gas Turbine Inst Beijing 100084 Peoples R China;

    Tsinghua Univ Dept Thermal Engn Gas Turbine Inst Beijing 100084 Peoples R China;

    Tsinghua Univ Dept Thermal Engn Gas Turbine Inst Beijing 100084 Peoples R China;

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