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薄平板气动导数的数值仿真技术 被引量:6
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作者 祝志文 陈政清 顾明 《湖南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2005年第5期11-15,共5页
提出了一种基于计算流体动力学方法计算流线型断面气动导数的数值模型.该模型以粘性不可压Navier-Stokes方程和有限体积法为基础,通过求解作强迫振动的断面绕流场,由得到的气动力时程得到断面的气动导数.利用该模型数值模拟了薄平板的... 提出了一种基于计算流体动力学方法计算流线型断面气动导数的数值模型.该模型以粘性不可压Navier-Stokes方程和有限体积法为基础,通过求解作强迫振动的断面绕流场,由得到的气动力时程得到断面的气动导数.利用该模型数值模拟了薄平板的气动导数,其仿真结果与薄平板气动导数风洞试验值、Theodorsen理想平板解析解的一致性,证明了本文方法的有效性.该数值方法可应用于桥梁断面颤振导数的识别. 展开更多
关键词 桥梁空气动力学 颤振导数 薄平板 数值仿真技术
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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that lead to the linear superposability of the unsteady aerodynamic forces in cases of thin airfoil sections are no longer valid for a bluff section.Theoretical models of bridge aerodynamics such as the one related to flutter-buffeting analysis and those concerning aerodynamic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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