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Turbulence Modifications in the Roughness Sublayer of Flow over a Highly-Irregular Surface Topology

机译:在高度不规则的表面拓扑中粗糙化粗糙度模板中的湍流修改

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Stereoscopic particle image velocimetry measurements are made in two wall-parallel planes-one within and the other at the outer edge of the roughness sublayer-for flow over a rough-wall topology replicated from a turbine blade damaged by deposition of foreign materials. The surface roughness studied herein is highly irregular, contains a broad range of topological scales and is therefore representative of what one might encounter in a variety of technologically-relevant flows of interest. Significant modification of the turbulence within the roughness sublayer (y = 0.0655 = 1.7k, where k is the characteristic roughness height) is observed at streamwise-spanwise locations that are coincident with dominant topological features, particularly strong enhancement of the wall-normal velocity fluctuations, the Reynolds shear stress and the swirling strength (a vortex identifier). These heterogeneities are found to diminish significantly toward the outer edge of the roughness sublayer (y = 0 155), with the statistics of the turbulence relaxing toward a relatively homogeneous state in both the streamwise and spanwise directions. Interestingly, the heterogeneities observed within the roughness sublayer are quite localized around dominant topological features, indicating that sustained wakes are not generated downstream of these roughness features.
机译:立体粒子图像速度测量法在两个壁平面平面上进行,在粗糙度子层的外边缘,另一个在粗糙度子层的外边缘,用于从通过沉积异物损坏的涡轮机叶片复制的粗糙壁拓扑。本文所研究的表面粗糙度高度不规则,含有广泛的拓扑尺度,因此代表在各种技术相关的感兴趣流动中遇到的内容。在流动的晶状体位置观察到粗糙度子层内的湍流(Y = 0.0655 = 1.7K,其中K是特征粗糙度高度)的显着修改,该位置与主导拓扑特征一致,特别是壁正常速度波动的强大增强,雷诺剪切应力和旋转强度(涡旋标识符)。发现这些异质性朝向粗糙度子层(Y = 0 155)的外边缘显着减小,其中湍流的统计在流动和翼展方向上朝向相对均匀的状态朝向相对均匀的状态。有趣的是,在粗糙化子窗内观察到的异质性是围绕主要拓扑特征的局部化,表明在这些粗糙度特征的下游不会产生持续的唤醒。

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