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TURBULENCE STATISTICS IN THE DEVELOPING URBAN BOUNDARY-LAYER

机译:发展城市边界层的湍流统计

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In experimental modelling of flow over very rough, urban-like surfacesHowever, this type of profile is only true in the inertial sublayer of a boundary layer that has adjusted to the underlying roughness. When the wind encounters a new surface roughness, the extent of the disturbed boundary layer is about 1/10 of the fetch, and only the bottom 10% of this internal boundary layer is in equilibrium with the new surface. Since many experimental studies are done with a fetch of building obstacles of the order of 100H or less, where H is the average building height, the extentof the inertial sublayer should only be about 1H. This is less than the depth of the typical roughness sublayer, in which the local perturbations due to individual obstacles disrupt the flow. Thus, in practice there should be no distinguishable layer inwhich the conditions for a semi-logarithmic profile are satisfied. Despite these limitations, when the velocity profile u(z) is plotted as a function of In(z-d) in these short arrays, the resulting data usually follows a reasonably straight line in theinternal boundary layer, and a value of can be is extracted from the slope.
机译:在非常粗糙的流量的实验建模中,城市样表面的无论如何,这种类型的轮廓仅在已经调整到底层粗糙度的边界层的惯性子层中真实。当风遇到新的表面粗糙度时,受干扰的边界层的程度为约1/10,并且仅具有新表面的该内部边界层的底部10%处于平衡状态。由于许多实验研究是用大约100h或更小的建筑物障碍物的取样完成的,其中H是平均建筑高度,惯性子层的程度应该仅为约1h。这少于典型粗糙度子层的深度,其中由于个体障碍物引起的局部扰动会破坏流量。因此,在实践中,应该没有区分的层,这是满足半对数轮廓的条件。尽管这些限制,当速度分布U(z)作为在这些短阵列中(Zd)的函数绘制时,所得到的数据通常在内部边界层中的相当直线遵循,并且可以从中提取值斜坡。

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