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Analysis of turbulent axisymmetric inner near wake

机译:湍流轴对称内部靠近尾迹的分析

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An analysis is presented describing the characteristics of mean velocity profile in the axisymmetric turbulent inner near-wake flow behind a body of revolution. The near wake is developing under zero streamwise pressure gradient and the upstream turbulent boundary layer is fully developed. It is shown that the boundary layer condition that exists at the trailing edge can be used to describe the mean velocity profiles in the inner near wake. It is shown that the logarithmic layer of the upstream turbulent boundary layer continues to be valid for some more distance in the near wake, and as the streamwise distance is increased, the logarithmic layer is slowly getting destroyed. It is also shown that the central line velocity exhibits a logarithmic behaviour for large streamwise distance. Results of the analysis have been validated using available experimental data.
机译:提出了一种分析,描述了旋转体轴对称湍流内近尾流中近尾流中的平均速度曲线的特征。 近似尾迹在零流动压力梯度下开发,并且充分开发上游湍流边界层。 结果表明,在后缘处存在的边界层条件可用于描述内部近尾的平均速度分布。 结果表明,上游湍流边界层的对数层继续有效地在近似尾唤醒中的一些距离,并且随着流动距离增加,对数层缓慢被破坏。 还示出了中央线速度表现出用于大流动距离的对数行为。 使用可用的实验数据验证了分析结果。

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