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PHYSICAL MODELLING OF URBAN ROUGHNESS USING ARRAYS OF REGULAR ROUGHNESS ELEMENTS

机译:使用常规粗糙度元素矩阵对城市粗糙度进行物理建模

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The aerodynamic behaviour of large urban agglomerations must be represented in increasingly greater detail, as large-scale numerical weather prediction and air pollution dispersion models are refined. The present study provides detailed measurements of the flow field in regular arrays of obstacles to obtain representative data on mean flow and turbulence statistics in urban-type areas. Obstacle arrays consisting of simple cubes and flat plate roughness commonly used in boundary layer simulations were placed in a simulated atmospheric boundary layer flow in a hydraulic flume. The scale factor was about 1:200 based on the obstacle height (50 mm). The results show no appreciable 'constant stress' region in the internal boundary layer above the buildings, since in any finite-length test array the boundary layer is always developing. However, if the RMS turbulence components are scaled by the local values of the shear stress, then there seems to be a universal scaling, with σ_u/u_* = 2.1, σ_υ/u_* = 1.65 and σ_w/u_* = 1.2. This greatly simplifies the parameterization of the first order turbulence statistics in obstacle arrays. It was also observed during the experiments that, compared to results in the cube arrays, the turbulence kinetic energy and the Reynolds stresses were almost doubled in the flat plate roughness arrays.
机译:随着大型数值天气预报和空气污染扩散模型的完善,必须越来越详细地描述大型城市群的空气动力学行为。本研究提供了规则障碍物阵列中流场的详细测量,以获得有关城市类型地区平均流量和湍流统计的代表性数据。通常在边界层模拟中使用的由简单的立方体和平板粗糙度组成的障碍物阵列放置在液压水槽中的模拟大气边界层流中。基于障碍物高度(50毫米),比例因子约为1:200。结果表明,在建筑物上方的内部边界层中没有明显的“恒定应力”区域,因为在任何有限长的测试阵列中,边界层始终在发展。但是,如果通过剪切应力的局部值对RMS湍流分量进行缩放,则似乎存在通用缩放比例,其中σ_u/ u_ * = 2.1,σ_υ/ u_ * = 1.65和σ_w/ u_ * = 1.2。这极大地简化了障碍物阵列中一阶湍流统计的参数化。在实验过程中还观察到,与立方体阵列中的结果相比,平板粗糙度阵列中的湍流动能和雷诺应力几乎增加了一倍。

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