2009
DOI: 10.1016/j.apm.2008.01.017
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Numerical simulation of laminar flow past a circular cylinder

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Cited by 316 publications
(139 citation statements)
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“…The turbulence is modeled through the kω-SST turbulence model by Menter [43]. Unsteady state computations have been successfully applied to the similar cases in the previous studies of Mahbubar et al [44] and Rajani et al [45]. All the simulations were converged until a satisfactory residual convergence was achieved on the velocities, pressure, and turbulence quantities.…”
Section: Computational Setupmentioning
confidence: 99%
“…The turbulence is modeled through the kω-SST turbulence model by Menter [43]. Unsteady state computations have been successfully applied to the similar cases in the previous studies of Mahbubar et al [44] and Rajani et al [45]. All the simulations were converged until a satisfactory residual convergence was achieved on the velocities, pressure, and turbulence quantities.…”
Section: Computational Setupmentioning
confidence: 99%
“…The flow remains steady and laminar for Reynolds number between 5 and 47 and the wake starts becoming unstable at a critical Reynolds number around 47, leading to the shedding of alternate vortices from the cylinder surface at definite frequencies, well known as the von Karman vortex street. The laminar vortex shedding is observed to be continuing up to a value of Re of about 190, beyond which the two-dimensional flow becomes unstable which leads to the formation and amplification of three-dimensional instabilities in the far wake region (Zhang et al 1995;Williamson 1996;Thompson et al 1996;Mittal and Balachandra 1997;Mittal 2001;Rajani et al 2009). These three dimensional disturbance leads to the simultaneous formation of spanwise and streamwise vortex structure along the spanwise direction and the far wake zone undergoes transition from laminar to turbulent state.…”
Section: Introductionmentioning
confidence: 99%
“…In general, the mean drag force is found to reduce as the Reynolds number augments. The cause is the decline of the viscous contribution which plays a role for the total drag force within the laminar ow regime [51]. The comparison of the amplitudes of uctuating lift coe cient C A L at various Reynolds numbers is displayed in Table 3.…”
Section: Methodsmentioning
confidence: 99%
“…It could be observed that even though the Reynolds number is recalculated, the drag reduction feature of the modi ed cylinder is still satis ed. Another feature which deserves to be mentioned is that in the considered Reynolds number range, the average drag coe cient of ow over usual cylinder changes slightly (which could be referred to the work of Rajani et al [51]). However, the percentage of drag reduction of the modi ed cylinder is signi cant.…”
Section: Drag Forcesmentioning
confidence: 99%