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Fluid–structure interaction of a square cylinder at different angles of attack

机译:方柱在不同迎角下的流固耦合

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摘要

This study investigates the free transverse flow-induced vibration (FIV) of an elastically mounted low-mass-ratio square cylinder in a free stream, at three different incidence angles: α = 0◦ , 20◦ and 45◦ . This geometric setup presents a body with an angle of attack, sharp corners and some afterbody, and therefore is a generic body that can be used to investigate a wide range of FIV phenomena. A recent study by Nemes et al. (J. Fluid Mech., vol. 710, 2012, pp. 102–130) provided a broad overview of the flow regimes present as a function of both the angle of attack α and reduced flow velocity U∗. Here, the focus is on the three aforementioned representative angles of attack: α = 0◦ , where the FIV is dominated by transverse galloping; α = 45◦ , where the FIV is dominated by vortex-induced vibration (VIV); and an intermediate value of α = 20◦, where the underlying FIV phenomenon has previously been difficult to determine. For the α = 0◦ case, the amplitude of oscillation increases linearly with the flow speed except for a series of regimes that occur when the vortex shedding frequency is in the vicinity of an odd-integer multiple of the galloping oscillation frequency, and the vortex shedding synchronizes to this multiple of the oscillation frequency. It is shown that only odd-integer multiple synchronizations should occur. These synchronizations explain the ‘kinks’ in the galloping amplitude response for light bodies first observed by Bearman et al. (J. Fluids Struct., vol. 1, 1987, pp. 19–34). For the α = 45◦ case, the VIV response consists of a number of subtle, but distinctly different regimes, with five regimes of high-amplitude oscillations, compared to two found in the classic VIV studies of a circular cylinder. For the intermediate α = 20◦ case, a typical VIV ‘upper branch’ occurs followed by a ‘higher branch’ of very large-amplitude response. The higher branch is caused by a subharmonic synchronization between the vortex shedding and the body oscillation frequency, where two cycles of vortex shedding occur over one cycle of oscillation. It appears that this subharmonic synchronization is a direct result of the asymmetric body. Overall, the FIV of the square cylinder is shown to be very rich, with a number of distinct regimes, controlled by both α and U∗. Importantly, α controls the underlying FIV phenomenon, as well as controlling the types of possible synchronization between the oscillation and vortex shedding.
机译:这项研究研究了自由流动中弹性安装的低质量比方筒在三个不同的入射角:α= 0°,20°和45°时的自由横向流致振动(FIV)。这种几何形状设置的物体具有攻角,尖角和一些残体,因此是可用于研究各种FIV现象的通用物体。 Nemes等人的最新研究。 (J. Fluid Mech。,第710卷,2012年,第102–130页)提供了对流态的广泛概述,该流态是迎角α和降低的流速U ∗的函数。这里,重点是上述三个代表性的迎角:α= 0°,其中FIV以横向驰豫为主导;反之亦然。 α= 45°,其中FIV由涡激振动(VIV)支配;中间值为α= 20°,以前很难确定潜在的FIV现象。对于α=0◦的情况,除了在涡旋脱落频率接近舞动振荡频率的奇数倍和涡旋附近发生的一系列状态外,振荡幅度随流速线性增加。脱落同步到振荡频率的此倍数。结果表明,仅奇数整数多个同步应该发生。这些同步解释了Bearman等人首先观察到的轻型物体的舞动幅度响应中的“扭结”。 (《流体结构》,第1卷,1987年,第19-34页)。对于α= 45°的情况,VIV响应由许多细微但截然不同的状态组成,具有五个高振幅振荡状态,而经典的VIV研究则是两个。对于中等α= 20°的情况,会出现典型的VIV“上部分支”,然后是幅值响应非常大的“较高分支”。较高的分支是由涡旋脱落与人体振荡频率之间的次谐波同步引起的,在该次谐波同步中,在一个振荡周期内发生了两个涡旋脱落周期。看来这种次谐波同步是不对称物体的直接结果。总的来说,方柱的FIV显示非常丰富,具有许多受α和U ∗控制的不同状态。重要的是,α控制潜在的FIV现象,以及控制振荡和涡旋脱落之间可能的同步类型。

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