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Experimental validation of large eddy simulations of flow and heat transfer in a stationary ribbed duct

机译:大涡模拟在固定肋管中流动和传热的实验验证

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Accurate prediction of ribbed duct flow and heat transfer is of importance to the gas turbine industry. The present study comprehensively validates the use of large eddy simulations (LES) for predicting flow and heat transfer with measured flowfield data in a stationary duct with 90° ribs and elucidates on the detailed physics encountered in the developing flow region, the fully developed region, and the 180° bend region. Among the major flow features predicted with accuracy are flow transition at the entrance of the duct; the distribution of mean and turbulent quantities in the developing, fully developed, and 180° bend; the development of secondary flows in the duct cross-section and the 180° bend; and friction and heat transfer augmentation. At the duct inlet, both the computations and experiments show that the peak turbulence intensities reach values as high as 40% in the streamwise and spanwise directions and 32% in the vertical direction, and a comparison of values along the centerline of the developing flow region shows that the mean flow and turbulent quantities do not become fully developed until they reach beyond the seventh rib of the duct. Turbulence intensities in the 180° bend are found to reach values as high as 50%, and local heat transfer comparisons show that the heat transfer augmentation shifts towards the outside wall downstream of the bend with little or no shift upstream. In addition to primary flow effects, secondary flow impingement on the smooth walls is found to develop by the third rib, while it continues to evolve downstream of the sixth rib. In all different aspects, it is found that LES produces the correct physics both qualitatively and quantitatively to within 10-15% of experiments.
机译:精确预测带肋管道的流量和热传递对燃气轮机行业至关重要。本研究全面验证了使用大型涡流模拟(LES)来预测流动和传热的能力,并利用在90°肋骨的固定管道中测得的流场数据进行了预测,并阐明了在发育中的流动区域,充分发达的区域中遇到的详细物理现象,和180°弯曲区域。可以准确预测的主要流量特征包括管道入口处的流量过渡。展开,完全展开和180°弯曲时的平均和湍流量的分布;管道横截面和180°弯曲处二次流的发展;以及摩擦和传热的增加。在导管入口处,计算和实验均表明,在水流方向和翼展方向上,湍流峰值强度达到高达40%的值,而在垂直方向上达到32%,并且沿流动区域的中心线的值比较结果表明,平均流量和湍流量只有在达到管道的第七根肋骨之前才能充分发展。发现180°弯曲处的湍流强度达到高达50%的值,并且局部传热比较显示,传热增强向弯曲下游的外壁移动,而上游几乎没有或没有移动。除了主要的流动效应外,还发现第三肋在平滑壁上产生了二次流撞击,而在第六肋的下游继续发展。在所有不同方面,发现LES在定性和定量方面都能产生正确的物理结果,达到实验的10-15%。

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