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The interaction between flow-induced vibration mechanisms of a square cylinder with varying angles of attack

机译:迎角变化的方圆柱体流致振动机理之间的相互作用

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摘要

This study examines the influence of angle of attack of a square section cylinder on the cylinder’s flow-induced vibration, where the direction of the vibration is transverse to the oncoming flow. Our experiments, which traversed the velocity–angle of attack parameter space in considerable breadth and depth, show that a low-mass ratio body can undergo combinations of both vortex-induced vibration and galloping. When the body has an angle of attack that makes it symmetric to the flow, such as when it assumes the square or diamond orientation, the two mechanisms remain independent. However, when symmetry is lost we find a mixed mode response with a new branch of vortex-induced oscillations that exceeds the amplitudes resulting from the two phenomena independently. The oscillations of this higher branch have amplitudes larger than the ‘upper branch’ of vortex-induced vibrations and at half the frequency. For velocities above this resonant region, the frequency splits into two diverging branches. Analysis of the amplitude response reveals that the transition between galloping and vortex-induced vibrations occurs over a narrow range of angle of incidence. Despite the rich set of states found in the parameter space the vortex shedding modes remain very similar to those found previously in vortex-induced vibration.
机译:这项研究研究了方形截面圆柱的迎角对圆柱的流动引起的振动的影响,该振动的方向垂直于迎面而来的流动。我们的实验在相当广度和深度上遍历了攻击参数空间的速度-角度,结果表明,低质量比的物体会经历涡流引起的振动和舞动的组合。当物体具有使其与流动对称的迎角时,例如当物体呈正方形或菱形方向时,这两种机制将保持独立。但是,当失去对称性时,我们发现混合模式响应具有新的涡流引起的振荡分支,该分支超过了独立于这两种现象的幅度。该较高分支的振荡幅度大于涡流引起的振动的“上部分支”,其频率为一半。对于高于该谐振区域的速度,频率分为两个分支。对幅度响应的分析表明,在驰豫和涡激振动之间的过渡发生在狭窄的入射角范围内。尽管在参数空间中发现了丰富的状态集,但涡旋脱落模式仍然与先前在涡旋诱发的振动中发现的状态非常相似。

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