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Large Eddy Simulations in Turbines: Influence of Roughness and Free-Stream Turbulence

机译:涡轮中的大型涡流模拟:粗糙度和自由流湍流的影响

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摘要

The individual and coupled effects of the incoming free-stream turbulence (FST) and surface roughness on the transition of a separated shear layer over a flat plate is numerically investigated using Large eddy simulation (LES). The upper wall of the test section is inviscid and specifically contoured to impose a streamwise pressure distribution over the flat plate to simulate the suction surface of a low pressure turbine (LPT) blade. The interaction of the streamwise streaks due to FST and roughness with the separated shear layer is captured. The streaks induced by FST are intermittent in nature and the streaks due to roughness are steady for a given topology of the rough surface. Both FST and roughness promoted near-wall mixing. The 'net effect' of mixing in the pre-separated region is manifested by a shift the inflection point of the velocity profile towards the wall. This resulted in the upstream shift of the transition point and a significant reduction in the size of the separation bubble. The combined effect of FST and roughness further reduced the size of separation bubble. The streamwise evolution of the boundary layer parameters has been compared for different cases. The potential 'roughness benefit' obtained in the case of highly loaded turbine blades in terms of its considerable reduction of profile loss is also shown.
机译:使用大涡模拟(LES)数值研究了流入的自由流湍流(FST)和表面粗糙度对平板上分离的剪切层过渡的个体和耦合效应。测试部分的上壁是不粘的,并且具有特定的轮廓,以在平板上施加沿流的压力分布,以模拟低压涡轮(LPT)叶片的吸力表面。捕获了由于FST和粗糙度引起的沿流条纹与分离的剪切层之间的相互作用。 FST引起的条纹本质上是断续的,并且对于给定的粗糙表面拓扑,由于粗糙度引起的条纹是稳定的。 FST和粗糙度都促进了近壁混合。在预分离区域中混合的“净效应”通过速度分布的拐点向壁的偏移来体现。这导致过渡点向上游移动,并大大减小了分离气泡的大小。 FST和粗糙度的共同作用进一步减小了分离气泡的尺寸。在不同情况下,已经比较了边界层参数的沿流演化。还显示了在高负荷涡轮机叶片情况下获得的潜在“粗糙度优势”,因为它可显着减少轮廓损失。

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