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A Reynolds-averaged turbulence modeling approach using three transport equations for the turbulent viscosity, kinetic energy, and dissipation rate

机译:使用雷诺平均湍流建模方法,使用三个传输方程来确定湍流粘度,动能和耗散率

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摘要

A Reynolds-averaged approach to turbulent shear flows is sought with resort to a three-equation method. Its novelty is the introduction of a turbulent-viscosity transport equation through the transport equation for the Reynolds stress in addition to those for the turbulent kinetic energy and the dissipation rate. The latter two equations are used for evaluating the dimensional coefficients in the former. The aim of this model is to enhance the capability to cope with nonstationary and advection effects in various turbulent flows. The adaptability to them is confirmed through the application to homogeneous-shear and supersonic free-shear flows. In particular, the reasonable prediction is obtained in the latter where the growth rate of the shear layer is suppressed with the increase in the convective Mach number. The present model is also applied to a three-dimensional flow past a wing tip as an instance of complex aeronautical flows, and the excessive diffusion of the trailing vortices is shown to be suppressed. The turbulent-viscosity representation for the Reynolds stress is systematically supplemented with nonlinear effects of mean-velocity gradient tensors, and its adequacy is verified in a channel flow.
机译:寻求雷诺平均的湍流剪切方法,并求助于三方程法。它的新颖之处在于,除了湍动能和耗散率外,还通过雷诺应力的输运方程引入了湍流-粘性输运方程。后两个方程式用于评估前者的尺寸系数。该模型的目的是增强应对各种湍流中的非平稳和平流效应的能力。通过应用于均质剪切流和超音速自由剪切流,证实了它们的适应性。特别地,在后者中获得了合理的预测,其中随着对流马赫数的增加,剪切层的生长速率受到抑制。本模型还适用于经过复杂的航空流的情况通过机翼尖端的三维流,并且显示出尾涡的过度扩散被抑制。用平均速度梯度张量的非线性效应系统地补充了雷诺应力的湍流-粘性表示,并在通道流中验证了其适当性。

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