2014
DOI: 10.1007/s00348-014-1682-z
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Vortex structure for flow over a heaving cylinder with a flexible tail

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Cited by 10 publications
(4 citation statements)
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“…In the experiment of Hu, Pan & Wang (2014), a circular cylinder with a FSP was forced to oscillate by the external sinusoidal excitation in the free stream, and the influence of the excitation frequency and L/D on the wake vortex structure was investigated. With the change of the excitation frequency and L/D , four different vortex shedding modes were observed in the wake, namely the 2S Kármán vortex, 2S reserved Kármán vortex, 2P mode and P + S mode.…”
Section: Introductionmentioning
confidence: 99%
“…In the experiment of Hu, Pan & Wang (2014), a circular cylinder with a FSP was forced to oscillate by the external sinusoidal excitation in the free stream, and the influence of the excitation frequency and L/D on the wake vortex structure was investigated. With the change of the excitation frequency and L/D , four different vortex shedding modes were observed in the wake, namely the 2S Kármán vortex, 2S reserved Kármán vortex, 2P mode and P + S mode.…”
Section: Introductionmentioning
confidence: 99%
“…Present study evaluates the effect of asymmetric oscillations of the cambered flexible wake splitter on the flow over a bluff body which has not been experimentally investigated yet. Moreover, the effective stiffness (П) of the present cambered flexible wake splitter (П =1.71) falls well in the range of chord-wise effective stiffness of few insects like bees and hawkmoths (0.19 ≤ П c ≤ 3.0) [6]. Equation (1) shows the expression for effective stiffness of the cambered flexible wake splitter,…”
Section: Introductionmentioning
confidence: 65%
“…The study also presented the effect of bending stiffness of the flexible splitter plate. In an experimental study it is shown that the flow characteristics of an oscillating circular cylinder significantly change with the increase in the length of the flexible tail particularly in between L/D = 3 & 4 [6]. The vortex shedding pattern changes from 2S_Karman mode at L/D = 2 to 2P mode at L/D = 3 and at L/D = 4 to 2S_reverse Karman vortex mode.…”
Section: Introductionmentioning
confidence: 99%
“…These two small-scale vortices are not the commonly thought trailing-edge vortex that is generated due to the motion of the film's trailing edge. For instance, in the experiment of Hu, Pan & Wang (2014), where a cylinder with a flexible film is forced to heave periodically in the free stream of a water tunnel, a clear trailing-edge vortex with a comparable size to that of the primary vortex is induced by the active downward or upward motion of the film's trailing edge. Besides, for the film of in the present investigation, a trailing edge vortex is formed from the shear layer induced by the motion of the trailing edge towards the negative direction (§ 3.5.1).…”
Section: Resultsmentioning
confidence: 99%