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机构地区:[1]哈尔滨工业大学结构工程灾变与控制教育部重点实验室,黑龙江哈尔滨150090 [2]哈尔滨工业大学土木工程学院,黑龙江哈尔滨150090 [3]河海大学土木与交通学院,江苏南京210098
出 处:《建筑结构学报》2016年第12期10-19,共10页Journal of Building Structures
基 金:国家自然科学基金面上项目(51278160;51478155;51378147)
摘 要:大跨度柱面屋盖结构的风荷载特性具有明显的雷诺数效应,其屋盖几何特征对风荷载雷诺数效应影响较大。为此,以柱面屋盖为研究对象,开展了考虑几何特征影响的雷诺数效应风洞试验,变化几何特征参数包括矢跨比(f/L为1/6~1/2)和长跨比(B/L为1~12),试验雷诺数Re范围为6.90×10^4~1.38×10^6。基于风洞试验数据,分析了模型表面风压分布规律、压力梯度和升阻力曲线等。研究结果表明:柱面屋盖长跨比减小、矢跨比增大会使雷诺数转捩区间的下限值向高雷诺数范围转移,即三维绕流效应使得分离边界层出现转捩滞后现象;当模型长跨比B/L由12减小至1时,雷诺数转捩区间下限值从1.66×10^5逐渐增大至4.14×10^5;当矢跨比f/L由1/3增加至1/2时,转捩区间下限值则从2.48×10^5增大至4.14×10^5;对矢跨比1/6屋盖模型,在试验雷诺数(6.90×10^4~2.48×10^5)范围内无明显雷诺数效应。There is a strong dependence of aerodynamic loads for large-span cylindrical roofs on Reynolds number effect, and the Reynolds number sensitivities are greatly influenced by the geometric characteristics of the roofs. As a result, based on the series of Reynolds number tests of cylindrical roof model, the influences of geometric parameters on the Reynolds number effects were investigated. Different rise to span ratios (f/L was from 1/6 to 1/2) and width to span ratios (B/L was from I to 12) were considered, and the Reynolds numbers ranged from 6.90 × 10^4 to 1.38 × 10^6. Based on the data derived from wind tunnel tests, the wind pressure distributions, pressure gradients and lift and drag force coefficients were analyzed. The test results show that there is a direct shift of the transitional Reynolds number towards high Re level owing to the increasing rise to span ratio, whilst the decreasing length to span ratio. This reveals that three-dimensional flow will postpone the transition of separated shear layers from laminar to turbulent over the roof surface. The lower limits of critical Reynolds number increases from 1.66 × 10^5 to 4. 14 × 10^5with B/L decreasing from 12 to 1, whilst the lower limits increases from 2. 48 × 10^5 to 4. 14 × 10^5 withf/L increasing from 1/3 to 1/2. There is no Reynolds number effect for cylinder roofs with f/L of 1/6 in the range of test Reynolds number from 6. 9 × 10^4 to 2. 48 × 10^5.
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