首页> 外文期刊>International Communications in Heat and Mass Transfer >NUMERICAL ANALYSIS OF TURBULENT CROSS STRESSES AND PRESSURE IN THE DEVELOPING REGION OF AN AXISYMMETRIC JET
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NUMERICAL ANALYSIS OF TURBULENT CROSS STRESSES AND PRESSURE IN THE DEVELOPING REGION OF AN AXISYMMETRIC JET

机译:轴对称射流发展区湍流交叉应力和压力的数值分析

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摘要

A numerical study was conducted of the transition region of an axisymmetric isothermal jet, from 10 to 44 diameters downstream of the nozzle exit. The transition region is of particular interest because if offers an opportunity to examine the relationship among physical quantities in a developing flow. A model for the Reynolds cross-stress terms was developed from empirical correlations of mean velocity. It was then used, along with correlations for RMS velocities, to numerically predict pressure in the developing region. This turbulence model is more accurate than experimental measurements in high Reynolds number, transitional flows because the scales of turbulence in these conditions are too small to resolve experimentally. Numerical results show that close coupling exists between the mean axial velocity and the Reynolds cross-stresses. Similarly, a close relationship exists between the axial and radial RMS velocity fluctuations and the developing pressure gradients in the axial and radial direction. Therefore, when the mean velocities reach fully similar form, similarity of Reynolds cross stresses is also required. The axial and radial fluctuations continue to develop, and asymptotically approach similar forms at rates closely matching the decay of the mean pressure gradients. The information presented here can be used to test turbulence models applied to developing flows.
机译:对轴对称等温射流的过渡区域进行了数值研究,其直径为喷嘴出口下游的10到44个直径。过渡区域特别受关注,因为它提供了一个机会来检查发育流中物理量之间的关系。雷诺交叉应力项的模型是根据平均速度的经验相关性开发的。然后将其与RMS速度的相关性一起用于数值预测发育区域中的压力。在高雷诺数,过渡流动下,这种湍流模型比实验测量更为准确,因为在这些条件下,湍流的尺度太小,无法通过实验解析。数值结果表明,平均轴向速度与雷诺交叉应力之间存在紧密耦合。类似地,轴向和径向RMS速度波动与轴向和径向方向上逐渐形成的压力梯度之间也存在密切的关系。因此,当平均速度达到完全相似的形式时,也需要雷诺交叉应力的相似性。轴向和径向波动继续发展,并且以与平均压力梯度的衰减紧密匹配的速率渐近地接近类似形式。此处提供的信息可用于测试应用于流动的湍流模型。

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