2020
DOI: 10.3390/en13174481
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Control and Suppression of Vortex Shedding from a Slightly Rough Circular Cylinder by a Discrete Vortex Method

Abstract: A discrete vortex method is implemented with a hybrid control technique of vortex shedding to solve the problem of the two-dimensional flow past a slightly rough circular cylinder in the vicinity of a moving wall. In the present approach, the passive control technique is inspired on the fundamental principle of surface roughness, promoting modifications on the cylinder geometry to affect the vortex shedding formation. A relative roughness size of ε*/d* = 0.001 (ε* is the average roughness and d* is the outer c… Show more

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Cited by 15 publications
(37 citation statements)
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“…All numerical simulations run until dimensionless time of t = 75, which is enough to reach a statistical equilibrium; the mean coefficient values (pressure distribution, drag and lift) are computed between 37.5 ≤ t ≤ 75.0. As previously presented by Oliveira et al [18], the adopted criterion to compute aerodynamic loads has sufficiently been refined attaining the saturation state of the numerical simulations; this behavior is typical of a Lagrangian technique.…”
Section: Resultsmentioning
confidence: 99%
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“…All numerical simulations run until dimensionless time of t = 75, which is enough to reach a statistical equilibrium; the mean coefficient values (pressure distribution, drag and lift) are computed between 37.5 ≤ t ≤ 75.0. As previously presented by Oliveira et al [18], the adopted criterion to compute aerodynamic loads has sufficiently been refined attaining the saturation state of the numerical simulations; this behavior is typical of a Lagrangian technique.…”
Section: Resultsmentioning
confidence: 99%
“…Furthermore, Figure 7 indicates that the lift coefficient,C L , oscillates regularly because of the periodic vortex shedding mechanism [41], and the lift force variation of the smooth cylinder is greater than that of the rough cylinder, which agrees with experimental tests conducted by Zhou et al [12]; the dash-dot lines in Figure 7 indicates the mean amplitude of lift force. In the present work, no analysis regarding the vortex shedding frequency is presented, however, a detailed discussion can be easily recuperated [14,17,18].…”
Section: Resultsmentioning
confidence: 99%
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