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Large eddy simulation of axial and compound angle holes with varying hole length-to-diameter ratio

机译:变径长径比的轴向和复合角孔的大涡模拟

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The effect of hole length to diameter ratio on flat plate film cooling effectiveness and flow structures of axial and compound angle hole is investigated by large eddy simulation (LES). Film cooling simulations are performed for three blowing ratios (M) ranging from 0.4 to 1.2, three hole length-to-diameter ratios (L/D) from 0.5 to 5 and two compound angle (β: 0°, 45°). The prediction accuracy is validated by the reported hydrodynamic data and present film effectiveness data measured by pressure sensitive paint (PSP). Results indicate that discrete hole with L=0.5 show highest film cooling effectiveness regardless of compound angle. Round hole generally shows an increasing trend as L increases from 2 to 5, while compound angle hole shows a complex trend concerning with blowing ratios and length to diameter ratios. 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). Scalar field transportation features are investigated to clarify how different vortex structures affect the temperature distribution and the film cooling effectiveness. It is also demonstrated that the counter rotating vortex pair (CRVP) which is observed in the time-averaged flow field of axial hole is originated in different vortex structures with varying blowing ratios and length to diameter ratios.
机译:通过大涡模拟(LES)研究了孔长径比对平板薄膜冷却效率以及轴向和复合角孔的流动结构的影响。针对范围从0.4到1.2的三个吹气比(M),范围从0.5到5的三个孔长径比(L / D)和两个复合角(β:0°,45°)进行薄膜冷却模拟。通过报告的水动力数据和通过压敏涂料(PSP)测量的当前薄膜有效性数据验证了预测精度。结果表明,与复合角无关,L = 0.5的离散孔显示出最高的薄膜冷却效率。随着L从2增加到5,圆孔通常显示出增加的趋势,而复合角孔则显示出与吹塑比和长径比有关的复杂趋势。这与以下事实有关:长径比会影响管内流动行为,开尔文-亥姆霍兹(K-H)结构的形成以及单个不对称主涡(SAMV)的发展。研究了标量场传输特征,以阐明不同的涡旋结构如何影响温度分布和薄膜冷却效率。还证明了在轴向孔的时间平均流场中观察到的反向旋转涡流对(CRVP)源自具有不同吹气比和长度直径比的不同涡流结构。

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