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首页> 外文期刊>Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering >Effects of turbulence intensity and scale on surface pressure fluctuations on the roof of a low-rise building in the atmospheric boundary layer
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Effects of turbulence intensity and scale on surface pressure fluctuations on the roof of a low-rise building in the atmospheric boundary layer

机译:湍流强度与规模对大气边界层低层建筑物屋顶表面压力波动的影响

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摘要

The effects of turbulence scales on the surface pressure fluctuations near the roof edge were investigated using the IBHS Research Center's full-scale wind tunnel under four sets of flow conditions on a full-scale replica of the TTU-WERFL building. These flow conditions ranged from streamwise turbulence intensities of 4%-16%, with varied spectral content. It was found that it is the energy levels of the streamwise velocity fluctuations over the range of non-dimensional frequencies, 0.1 fH/V 2, which are active, controlling both the magnitude and distribution of the surface pressure fluctuations near the roof edge of low-rise buildings in the atmospheric boundary layer. The data indicate that, for the relatively high levels of turbulence energy typical of the atmospheric surface layer, there are (i) significantly smaller mean reattachment lengths, with (ii) much higher peak and fluctuating pressures, which are (iii) located closer to the roof edge. This range wavenumbers is one to two orders of magnitude larger in size than those associated with the width of the separated shear layer and Melbourne's small-scale turbulence parameter. This implies that partial turbulence simulation methods must capture the energy at these scales in order to lead to accurate wind tunnel simulations of low-rise building aerodynamics.
机译:在TTU-WERFL建筑的全规模复制品上的四组流动条件下,使用IBHS研究中心的全尺寸风洞研究了湍流尺度对屋顶边缘附近的表面压力波动。这些流动条件范围为4%-16%的流动湍流强度,具有变化的光谱含量。结果发现,它是无尺寸频率范围内的流速速度波动的能量水平,0.1& / v&图2是有效的,控制大气边界层低层建筑物屋顶边缘附近的表面压力波动的大小和分布。数据表明,对于大气表面层的典型型湍流能量相对较高,存在(i)显着较小的平均重新连接长度,具有(ii)更高的峰值和波动压力,其靠近(iii)更靠近屋顶边缘。该范围波数的尺寸大于与与分离的剪切层和墨尔本的小型湍流参数相关联的尺寸较大一到两个数量级。这意味着部分湍流仿真方法必须在这些秤上捕获能量,以便导致低层建筑空气动力学的准确风隧道模拟。

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