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流线箱梁弯扭耦合气动力非线性特性与颤振行为预测
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作者 赵林 王达 +2 位作者 方根深 崔巍 葛耀君 《中国公路学报》 EI CAS CSCD 北大核心 2024年第3期273-282,共10页
传统大跨度桥梁空气动力学颤振分析忽略了结构和气动力非线性,多用于预测颤振临界风速而难于对颤振后行为进行合理分析。为此,通过强迫振动试验对气动力叠加性进行详细考证,阐明其适用范围。在传统复模态特征值分析中引入了随幅值变化... 传统大跨度桥梁空气动力学颤振分析忽略了结构和气动力非线性,多用于预测颤振临界风速而难于对颤振后行为进行合理分析。为此,通过强迫振动试验对气动力叠加性进行详细考证,阐明其适用范围。在传统复模态特征值分析中引入了随幅值变化的结构阻尼比和颤振导数,实现了颤振后状态结构振幅的预测分析,并与风洞试验结果进行了对比验证。结果表明:试验范围(竖向振幅Ah/B≤1.0,扭转振幅Aα≤12°)内,流线箱梁断面弯扭耦合气动力近似满足叠加性;节段模型风洞试验中结构阻尼和气动力的幅值依赖性是系统非线性的主要表现形式,在复模态特征值分析中引入幅变的颤振导数和结构阻尼比可以较好地预测滞回颤振振幅随风速的变化关系。 展开更多
关键词 桥梁工程 流线箱梁断面 非线气动力 颤振后 气动力叠加性 复模态特征值法
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Superposability of unsteady aerodynamic loads on bridge deck sections 被引量:2
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作者 张志田 葛耀君 张伟峰 《Journal of Central South University》 SCIE EI CAS 2013年第11期3202-3215,共14页
The 2-dimensional unsteady aerodynamic forces,in the context of both a thin airfoil where theory of potential flow is always applicable and a bluff bridge-deck section where separated flow is typically induced,are inv... The 2-dimensional unsteady aerodynamic forces,in the context of both a thin airfoil where theory of potential flow is always applicable and a bluff bridge-deck section where separated flow is typically induced,are investigated from a point of view of whether or not they conform to the principle of linear superposition in situations of various structural motions and wind gusts.It is shown that some basic preconditions that lead to the linear superposability of the unsteady aerodynamic forces in cases of thin airfoil sections are no longer valid for a bluff section.Theoretical models of bridge aerodynamics such as the one related to flutter-buffeting analysis and those concerning aerodynamic admittance(AA)functions,however,necessitate implicitly this superposability.The contradiction revealed in this work may throw light on the perplexing problem of AA functions pertaining to the description of buffeting loads of bridge decks.Some existing theoretical AA models derived from flutter derivatives according to interrelations valid only for thin airfoil theories,which have been employed rather extensively in bridge aerodynamics,are demonstrated to be illogical.Finally,with full understanding of the preconditions of the applicability of linear superposability of the unsteady aerodynamic forces,suggestions in regard to experiment-based AA functions are presented. 展开更多
关键词 bridge unsteady load aerodynamic load SUPERPOSITION BUFFETING FLUTTER
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