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Steady suction-based aerodynamic control for suppressing vortex induced vibration of a bridge deck section

机译:用于抑制涡旋型桥型涡旋振动的稳定吸入式空气动力学控制

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The control effects of Vortex-Induced Vibration of bridge deck sections under steady suction are investigated by wind tunnel experiments. The analysis results show that the steady suction efficiently reduces the vortex-induced vibration amplitude, increases the Vortex-Induced Vibration (VIV) critical wind speed, and shortens lock-in wind speed range. The suction arranged on the undersurface near the leeward side of the model shows the best result. To study the mechanism of the steady suction control, the CFD-based numerical analysis is performed aiming at the baseline case and several other cases which have better control effect. The results and analysis demonstrate that the steady suction flow can enhance the A-mode secondary wake instability, and therefore the large scale spanwise vortex is suppressed so as to reduce aerodynamic forces.
机译:通过风洞实验研究了桥接甲板段的涡旋凸型振动的控制效应。分析结果表明,稳定抽吸有效地降低了涡旋诱导的振动幅度,提高了涡旋诱导的振动(VIV)临界风速,并缩短锁定风速范围。布置在模型的Leeward侧附近的下表面上的抽吸显示了最佳结果。为了研究稳定吸力控制的机制,基于CFD的数值分析针对基线情况和具有更好控制效果的其他情况。结果和分析表明,稳定抽吸流可以增强A模式二次唤醒不稳定性,因此抑制了大规模的血管涡流,以减小空气动力。

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