2000
DOI: 10.1016/s0029-8018(98)00050-x
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A finite difference solution of the shear flow over a circular cylinder

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Cited by 75 publications
(88 citation statements)
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“…In the first branch (β ∈ [0, 0.2]), C x slowly decreases as a function of β. A similar trend was observed by Lei et al (2000), Kang (2006) and Cao et al (2010) in the same range of β, at comparable Reynolds numbers. As the shear parameter is increased above 0.…”
Section: Fluid Forcessupporting
confidence: 85%
See 1 more Smart Citation
“…In the first branch (β ∈ [0, 0.2]), C x slowly decreases as a function of β. A similar trend was observed by Lei et al (2000), Kang (2006) and Cao et al (2010) in the same range of β, at comparable Reynolds numbers. As the shear parameter is increased above 0.…”
Section: Fluid Forcessupporting
confidence: 85%
“…The case of a fixed circular cylinder placed in planar shear flow has been addressed experimentally Kwon, Sung & Hyun 1992;Sumner & Akosile 2003;Cao et al 2007) and numerically (Jordan & Fromm 1972;Yoshino & Hayashi 1984;Chew, Luo & Cheng 1997;Lei, Cheng & Kavanagh 2000;Kang 2006;Cao et al 2010). These prior studies, which mainly focused on linear shear, quantified the evolution of the vortex shedding frequency and time-averaged fluid forces as functions of the shear parameter (β), defined as the inflow velocity gradient normalized by the cylinder diameter and the oncoming flow velocity at the centre of the body.…”
Section: Introductionmentioning
confidence: 99%
“…A second-order scheme is used for aIl the time dependent terms. For details of numerical Implementation, readers are refered to Lei et al (1999).…”
Section: Methodsmentioning
confidence: 99%
“…Moreover, H = 4π 2 e 4πξ , Re = 2u ∞ a ν , u ∞ is the free-stream velocity, ν is the kinematic viscosity, and the dimensionless time is t = t * u ∞ a . The sketch of shear flow, which shows the change of the velocity in the cross-section plane of the cylinder, with a linear velocity profile u = u ∞ + Gy [43] over a cylinder in two-dimensional domain is shown in Figure 2, where u ∞ is the free-stream velocity at the center-line θ = 0, y is the coordinate in the lateral direction with y = 0 at the center of the cylinder, and G is the lateral velocity gradient. Defining the shear rate K as…”
Section: Governing Equationsmentioning
confidence: 99%