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Vortex models for aeroelastic assessment of multi element bridge decks

机译:用于多层桥面气动弹性评估的Vortex模型

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This paper presents vortex models for determination of the critical wind speed for onset of aeroelastic instability (binary flutter) of a twin-deck bridge. First a simple mathematical mdoel is presented, based on the vortex concept of classical two-dimensional potential flow theory. In this model the cross-flow due to bound vorticity and the trailing potential wake(s), is balanced by the cross-flow due to a prescribed oscillatory motion of the deck structure. The simple model yields a frequency domain representation of the motion induced forces which is directly applicable in standard flutter routines. Advanced discrete vortex models of twin and multi element decks are discussed which involves time domain simulation of the motion induced aerodynamic forces. The paper establishes the effect of the horizontal distance between deck elements on the aeroelastic stability. Stability predictions, based on the mathematical models discussed, are compared to existing wind tunnel test results of twin-deck configurations. Good agreement is demonstrated.
机译:本文提出了用于确定双夹层桥梁气动弹性不稳定性(二进制颤振)发作临界风速的涡模型。首先,基于经典二维势流理论的涡旋概念,提出了一种简单的数学模型。在该模型中,由于约束涡旋和尾随电势引起的横流被甲板结构的规定振荡运动引起的横流所平衡。简单的模型产生运动感应力的频域表示,可直接应用于标准颤动程序。讨论了双单元和多单元甲板的高级离散涡模型,其中包括运动引起的空气动力的时域仿真。本文建立了甲板单元之间的水平距离对气动弹性稳定性的影响。根据讨论的数学模型,将稳定性预测与现有的双层结构风洞测试结果进行比较。表现出良好的协议。

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