2007
DOI: 10.1016/j.compfluid.2007.02.001
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Lattice Boltzmann simulation of lid-driven swirling flow in confined cylindrical cavity

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Cited by 33 publications
(25 citation statements)
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“…On the other hand, one vortex break down bubble is seen at (1.5, 1290) and two break down bubbles occur in the vicinity of the cylinder axis. These distinct regimes in swirling flows and the complex flow structure for different (R A , Re) cases are strikingly consistent with prior numerical solution (e.g., [56,19,21,57]). Quantitative comparison of the computed structure of the axial velocities along the axis of symmetry obtained using the axisymmetric cascaded LB schemes for the above four sets of the aspect ratios R A and Reynolds number…”
Section: Swirling Flow In a Lid-driven Cylindrical Containersupporting
confidence: 88%
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“…On the other hand, one vortex break down bubble is seen at (1.5, 1290) and two break down bubbles occur in the vicinity of the cylinder axis. These distinct regimes in swirling flows and the complex flow structure for different (R A , Re) cases are strikingly consistent with prior numerical solution (e.g., [56,19,21,57]). Quantitative comparison of the computed structure of the axial velocities along the axis of symmetry obtained using the axisymmetric cascaded LB schemes for the above four sets of the aspect ratios R A and Reynolds number…”
Section: Swirling Flow In a Lid-driven Cylindrical Containersupporting
confidence: 88%
“…For example, Refs. [52,56] show that for cases (R A , Re) equal to (1.5, 990) and (2.5,1010), no vortex breakdown bubbles occur whereas for (1.5, 1290), they do occur.…”
Section: Swirling Flow In a Lid-driven Cylindrical Containermentioning
confidence: 96%
“…On the other hand, straightforward integration of the LBE on a non-uniform and/or unstructured mesh is not possible. This leads to difficulty in adapting the mesh to complex flow-structures such as separation, vortices, shear/ boundary layers etc., and to satisfy boundary conditions on irregular geometries [6]. Such difficulty may be overcome by decoupling the numerical mesh from the lattice structure, and taking recourse to, one of finite difference (FD) [7][8][9], finite element (FE) [10][11][12][13][14][15], or finite volume (FV) [16][17][18][19] approaches.…”
Section: Introductionmentioning
confidence: 99%
“…In the last two decades, LBE has been rapidly developed as an effective and promising numerical algorithm for computational fluid dynamics [4][5][6], which has also been applied to axisymmetric flows [7][8][9][10][11][12][13][14][15][16][17][18][19]. The straightforward way for LBE to simulate such flows is using a 3D LBE model with suitable curved boundary treatments [22][23][24]. Nevertheless, such approach implies the expensive computational costs for this 3D simulation which does not consider any symmetrical properties of the axisymmetric flows.…”
Section: Introductionmentioning
confidence: 99%