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J Comput Phys. 2007 Aug;225(2):1782-1809. doi: 10.1016/j.jcp.2007.02.017.
3
Numerical investigation of the hydrodynamics of carangiform swimming in the transitional and inertial flow regimes.过渡流和惯性流状态下鲹科鱼类游泳水动力学的数值研究。
J Exp Biol. 2008 May;211(Pt 10):1541-58. doi: 10.1242/jeb.015644.

在近尾流干涉区域中两个串联排列圆柱的涡激振动。

Vortex-induced vibrations of two cylinders in tandem arrangement in the proximity-wake interference region.

作者信息

Borazjani Iman, Sotiropoulos Fotis

机构信息

St Anthony Falls Laboratory, Department of Civil Engineering, University of Minnesota, 2 Third Avenue SE, Minneapolis, MN, USA.

出版信息

J Fluid Mech. 2009;621:321-364. doi: 10.1017/S0022112008004850.

DOI:10.1017/S0022112008004850
PMID:19693281
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC2728241/
Abstract

We investigate numerically vortex-induced vibrations (VIV) of two identical two-dimensional elastically mounted cylinders in tandem in the proximity-wake interference regime at Reynolds number Re = 200 for systems having both one (transverse vibrations) and two (transverse and in-line) degrees of freedom (1-DOF and 2-DOF, respectively). For the 1-DOF system the computed results are in good qualitative agreement with available experiments at higher Reynolds numbers. Similar to these experiments our simulations reveal: (1) larger amplitudes of motion and a wider lock-in region for the tandem arrangement when compared with an isolated cylinder; (2) that at low reduced velocities the vibration amplitude of the front cylinder exceeds that of the rear cylinder; and (3) that above a threshold reduced velocity, large-amplitude VIV are excited for the rear cylinder with amplitudes significantly larger than those of the front cylinder. By analysing the simulated flow patterns we identify the VIV excitation mechanisms that lead to such complex responses and elucidate the near-wake vorticity dynamics and vortex-shedding modes excited in each case. We show that at low reduced velocities vortex shedding provides the initial excitation mechanism, which gives rise to a vertical separation between the two cylinders. When this vertical separation exceeds one cylinder diameter, however, a significant portion of the incoming flow is able to pass through the gap between the two cylinders and the gap-flow mechanism starts to dominate the VIV dynamics. The gap flow is able to periodically force either the top or the bottom shear layer of the front cylinder into the gap region, setting off a series of very complex vortex-to-vortex and vortex-to-cylinder interactions, which induces pressure gradients that result in a large oscillatory force in phase with the vortex shedding and lead to the experimentally observed larger vibration amplitudes. When the vortex shedding is the dominant mechanism the front cylinder vibration amplitude is larger than that of the rear cylinder. The reversing of this trend above a threshold reduced velocity is associated with the onset of the gap flow. The important role of the gap flow is further illustrated via a series of simulations for the 2-DOF system. We show that when the gap-flow mechanism is triggered, the 2-DOF system can develop and sustain large VIV amplitudes comparable to those observed in the corresponding (same reduced velocity) 1-DOF system. For sufficiently high reduced velocities, however, the two cylinders in the 2-DOF system approach each other, thus significantly reducing the size of the gap region. In such cases the gap flow is entirely eliminated, and the two cylinders vibrate together as a single body with vibration amplitudes up to 50% lower than the amplitudes of the corresponding 1-DOF in which the gap flow is active. Three-dimensional simulations are also carried out to examine the adequacy of two-dimensional simulations for describing the dynamic response of the tandem system at Re = 200. It is shown that even though the wake transitions to a weakly three-dimensional state when the gap flow is active, the three-dimensional modes are too weak to affect the dynamic response of the system, which is found to be identical to that obtained from the two-dimensional computations.

摘要

我们对雷诺数Re = 200、处于近尾流干扰状态下的两个相同的二维弹性支撑串联圆柱的涡激振动(VIV)进行了数值研究,研究对象为具有一个自由度(横向振动)和两个自由度(横向和纵向)的系统(分别为1-DOF和2-DOF)。对于1-DOF系统,计算结果与较高雷诺数下的现有实验结果在定性上吻合良好。与这些实验类似,我们的模拟结果表明:(1)与单个圆柱相比,串联布置的运动幅度更大,锁定区域更宽;(2)在低折合速度下,前圆柱的振动幅度超过后圆柱;(3)在超过阈值折合速度时,后圆柱会激发大幅VIV,其幅度明显大于前圆柱。通过分析模拟流型,我们确定了导致这种复杂响应的VIV激发机制,并阐明了每种情况下近尾流涡量动力学和涡脱落模式。我们表明,在低折合速度下,涡脱落提供了初始激发机制,导致两个圆柱之间出现垂直分离。然而,当这种垂直分离超过一个圆柱直径时,相当一部分来流能够穿过两个圆柱之间的间隙,间隙流机制开始主导VIV动力学。间隙流能够周期性地将前圆柱的顶部或底部剪切层压入间隙区域,引发一系列非常复杂的涡 - 涡和涡 - 圆柱相互作用,从而产生压力梯度,导致与涡脱落同相的大幅振荡力,并导致实验观察到的更大振动幅度。当涡脱落是主导机制时,前圆柱的振动幅度大于后圆柱。在超过阈值折合速度时这种趋势的逆转与间隙流的出现有关。间隙流的重要作用通过对2-DOF系统的一系列模拟进一步得到说明。我们表明,当间隙流机制被触发时,2-DOF系统能够产生并维持与相应(相同折合速度)1-DOF系统中观察到的值相当的大幅VIV幅度。然而,对于足够高的折合速度,2-DOF系统中的两个圆柱相互靠近,从而显著减小了间隙区域的尺寸。在这种情况下,间隙流完全消失,两个圆柱作为一个整体一起振动,其振动幅度比间隙流活跃的相应1-DOF系统的幅度低达50%。还进行了三维模拟,以检验二维模拟对于描述Re = 200时串联系统动态响应的充分性。结果表明,尽管在间隙流活跃时尾流转变为弱三维状态,但三维模式太弱,无法影响系统的动态响应,发现其与二维计算结果相同。