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Vortex shedding characteristics around a circular cylinder with flexible film

机译:涡旋脱落特性围绕圆柱丝筒,柔性薄膜

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In this paper, an experimental study about the influence of flexible film on the vortex shedding characteristics behind a cylinder has been performed with increasing Reynolds number (Re) and the ratio of flexible film length to cylinder diameter (L/D). The smoke-wire technique is implemented for flow visualization. The detailed statistics and vortex shedding structures associated with pressure fluctuations owing to a flexible film behind a cylinder are presented. The focus of this paper is on efforts to reveal the influence on the distribution of fluctuation pressure and the frequency of vortex shedding resulting from flapping flexible film with different parameters of L/D. Our experimental results mainly reveal that when the flexible film is in asymmetric flapping mode behind the cylinder, the peak distribution of fluctuating pressure coefficients C-pf will deviates from central area. The Strouhal number decreases with the increase of LID. For L/D=3, the Strouhal number also decreases with increasing Re. It is found that the peak of fluctuating pressure spectrum is closely related with the non-dimensional parameter L/D, and the vortex shedding frequency obviously decreases with increasing of L/D. The fluctuating signal of flapping flexible film for L/D=5 effectively offsets the fluctuating signal behind a cylinder itself, and the peak of fluctuating pressure spectrum does not occur at Re=2500. Nevertheless, for L/D=3, the amplitude of fluctuating pressure spectrum obviously exceeds that of fluctuating pressure spectrum of L/D=0. Our results further reveal that flapping flexible film effectively controls the vortex shedding behind a cylinder with increasing of L/D. However, for L/D=3, the flapping flexible film results in harmonic excitation mode. (C) 2019 Published by Elsevier Masson SAS.
机译:在本文中,通过增加雷诺数(RE)和柔性薄膜长度与圆柱直径(L / D)的比率进行了关于芯膜对汽缸后面的涡旋脱落特性的影响的实验研究。烟丝技术用于流动可视化。提出了与压力波动相关的详细统计和涡流脱落结构,由于圆柱体后面的柔性薄膜。本文的重点是努力揭示对波动压力分布的影响和涡旋脱落的频率,从L / D的不同参数拍打柔性膜。我们的实验结果主要揭示了柔性薄膜在气缸后面处于不对称拍摄模式时,波动压力系数C-PF的峰值分布将偏离中心区域。随着盖子的增加,Strouhal数量会降低。对于L / D = 3,Strouhal数量也随着RE的增加而降低。发现波动压力谱的峰值与非尺寸参数L / D密切相关,涡流脱落频率随着L / D的增加而显然降低。 L / D = 5的拍打柔性膜的波动信号有效地抵消了气缸本身后面的波动信号,并且在RE = 2500处不会发生波动压力谱的峰值。然而,对于L / D = 3,波动压力谱的幅度明显超过L / D = 0的波动压力谱的幅度。我们的结果进一步揭示了吹拍柔性薄膜有效地控制圆筒后面的涡旋脱落,随着L / D的增加。然而,对于L / D = 3,扑振薄膜导致谐波激励模式。 (c)2019年由Elsevier Masson SA出版。

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