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首页> 外文期刊>Boundary-layer Meteorology >Adjustment of Turbulent Boundary-Layer Flow to Idealized Urban Surfaces: A Large-Eddy Simulation Study
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Adjustment of Turbulent Boundary-Layer Flow to Idealized Urban Surfaces: A Large-Eddy Simulation Study

机译:湍流边界层流向理想城市表面的调整:大涡模拟研究

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Large-eddy simulations (LES) are performed to simulate the atmospheric boundary-layer (ABL) flow through idealized urban canopies represented by uniform arrays of cubes in order to better understand atmospheric flow over rural-to-urban surface transitions. The LES framework is first validated with wind-tunnel experimental data. Good agreement between the simulation results and the experimental data are found for the vertical and spanwise profiles of the mean velocities and velocity standard deviations at different streamwise locations. Next, the model is used to simulate ABL flows over surface transitions from a flat homogeneous terrain to aligned and staggered arrays of cubes with height . For both configurations, five different frontal area densities , equal to 0.028, 0.063, 0.111, 0.174 and 0.250, are considered. Within the arrays, the flow is found to adjust quickly and shows similar structure to the wake of the cubes after the second row of cubes. An internal boundary layer is identified above the cube arrays and found to have a similar depth in all different cases. At a downstream location where the flow immediately above the cube array is already adjusted to the surface, the spatially-averaged velocity is found to have a logarithmic profile in the vertical. The values of the displacement height are found to be quite insensitive to the canopy layout (aligned vs. staggered) and increase roughly from to as increases from 0.028 to 0.25. Relatively larger values of the aerodynamic roughness length are obtained for the staggered arrays, compared with the aligned cases, and a maximum value of is found at for both configurations. By explicitly calculating the drag exerted by the cubes on the flow and the drag coefficients of the cubes using our LES results, and comparing the results with existing theoretical expressions, we show that the larger values of for the staggered arrays are related to the relatively larger drag coefficients of the cubes for that configuration compared with the aligned one. The effective mixing length within and above different cube arrays is also calculated and a local maximum of within the canopy is found in all the cases, with values ranging from to . These patterns of are different from those used in existing urban canopy models.
机译:进行大涡模拟(LES)以模拟通过理想的城市雨棚(由均匀的立方体阵列代表)的大气边界层(ABL)流动,以便更好地理解从农村到城市表面过渡的大气流量。 LES框架首先通过风洞实验数据进行了验证。对于不同流向位置的平均速度和速度标准偏差的垂直和展向剖面,仿真结果与实验数据之间找到了很好的一致性。接下来,该模型用于模拟从平坦的均匀地形到具有高度的立方体的排列和交错阵列的表面过渡上的ABL流。对于这两种配置,考虑了五个不同的正面面积密度,分别为0.028、0.063、0.111、0.174和0.250。在阵列内,发现流量可以快速调整,并显示与第二排多维数据集之后的多维数据集相似的结构。在多维数据集阵列上方标识了一个内部边界层,并发现在所有不同情况下其内部深度都相似。在已经将立方体阵列正上方的流调整到表面的下游位置,发现空间平均速度在垂直方向上具有对数轮廓。发现位移高度的值对机盖布局非常不敏感(对齐与交错),并且从到大致从0.028增加到0.25。与对齐的情况相比,交错阵列获得的空气动力学粗糙度长度值相对较大,并且两种配置的最大值都在处找到。通过使用LES结果显式计算多维数据集对流施加的阻力和多维数据集的阻力系数,并将结果与​​现有的理论表达式进行比较,我们表明,交错数组的较大值与相对较大的数组有关。与对齐的立方体相比,该配置的立方体的阻力系数。在所有情况下,还计算了不同立方体阵列之内和之上的有效混合长度,并且在所有情况下都找到了顶篷内的局部最大值,其值范围为至。这些模式与现有城市机盖模型中使用的模式不同。

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