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Turbulent Transport Modeling of Shear Flows around an Aerodynamic Wing. Development of Turbulent Near-Wall Model and Its Application to Recirculating Flows

机译:气动机翼周围剪切流动的湍流输运模型。湍流近壁模型的研制及其在循环流动中的应用

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Progress in implementing and refining two near-wall turbulence models in which the near-wall region is divided into either two or three zones is outlined. These models were successfully applied to the computation of recirculating flows. The research was further extended to obtaining experimental results of two different recirculating flow conditions in order to check the validity of the present models. Two different experimental apparatuses were set up: axisymmetric turbulent impinging jets on a flat plate, and turbulent flows in a circular pipe with a abrupt pipe expansion. It is shown that generally better results are obtained by using the present near-wall models, and among the models the three-zone model is superior to the two-zone model.

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