梁洪超, 楼文娟, 丁浩, 卞荣. 非线性振型结构HFFB试验模态力计算方法及不确定性分析[J]. 工程力学, 2019, 36(3): 71-78. DOI: 10.6052/j.issn.1000-4750.2018.01.0008
引用本文: 梁洪超, 楼文娟, 丁浩, 卞荣. 非线性振型结构HFFB试验模态力计算方法及不确定性分析[J]. 工程力学, 2019, 36(3): 71-78. DOI: 10.6052/j.issn.1000-4750.2018.01.0008
LIANG Hong-chao, LOU Wen-juan, DING Hao, BIAN Rong. GENERALIZED FORCE CALCULATION METHOD AND UNCERTAINTY ANALYSIS OF NONLINEAR MODE STRUCTURE IN HFFB TESTS[J]. Engineering Mechanics, 2019, 36(3): 71-78. DOI: 10.6052/j.issn.1000-4750.2018.01.0008
Citation: LIANG Hong-chao, LOU Wen-juan, DING Hao, BIAN Rong. GENERALIZED FORCE CALCULATION METHOD AND UNCERTAINTY ANALYSIS OF NONLINEAR MODE STRUCTURE IN HFFB TESTS[J]. Engineering Mechanics, 2019, 36(3): 71-78. DOI: 10.6052/j.issn.1000-4750.2018.01.0008

非线性振型结构HFFB试验模态力计算方法及不确定性分析

GENERALIZED FORCE CALCULATION METHOD AND UNCERTAINTY ANALYSIS OF NONLINEAR MODE STRUCTURE IN HFFB TESTS

  • 摘要: 基于高频测力天平风洞试验对非线性振型结构的风致响应提出了改进的评估方法。假设结构风荷载沿高度的分布与阵风风压分布相同,采用结构真实振型计算风荷载模态力。推导了高耸结构风荷载模态力及风致响应计算公式,可以考虑结构多阶真实振型,从而使高频测力天平方法可更为准确地评估非线性振型结构的风致响应及等效静力风荷载。对某一质量、刚度有突变的高耸结构进行了高频测力天平风洞试验,与现有的线性化振型法进行对比,结果表明在弱非线性振型下,线性化振型法得到的加速度响应较层荷载假设方法偏大约40%。研究了层荷载分布的不确定性对计算加速度响应结果的影响,结果表明在阵风剖面层荷载的假设下,荷载分布的不确定性对结构最大加速度响应的影响很小,验证了本文方法的适用性。

     

    Abstract: Based on the high-frequency-force-balance test, an improved method for evaluating wind-induced response of nonlinear mode-shape structures is proposed. The vertical distribution of wind load is assumed to be the same with gust wind pressure, then real mode shapes are used to calculate the generalized wind forces. The computational formulas of generalized wind forces and wind-induced responses are derived, and the higher modes can be considered, so that the high-frequency-force-balance method can accurately evaluate the wind-induced responses and equivalent static wind loads of nonlinear mode shape structures. A high-frequency-force-balance test of a tall structure with changes in mass and stiffness is conducted. Comparing the proposed method with linear mode shape method, the computational error of the linear mode assumption is analyzed, and it shows that the acceleration response of a nonlinear mode shape structure can be 40% overestimated applying the linear mode shape method. The influence of the load distribution uncertainty is studied. The results show that under the assumption of gust wind profile load, the load distribution uncertainty has little effect on the maximum acceleration response, which proves the applicability of the proposed method.

     

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