2019
DOI: 10.1177/0954406219866478
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Quantification of wake unsteadiness for low-Re flow across two staggered cylinders

Abstract: This work performs a numerical investigation on the two-dimensional flow across two circular cylinders in staggered arrangement at Re = 100. The seaparting distances between the centers of the cylinders are D/ d = 4–10 with Δ D/ d = 2 and T/ d = 0.0–2.0 with Δ T/ d = 0.5 in the streamwise and transverse directions, respectively, in which d is the cylinder diameter. Although the low- Re flow across staggered cylinders has been studied in a number of works, the authors mainly concerned about the identification a… Show more

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Cited by 22 publications
(13 citation statements)
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“…Finite element methods [24][25][26][27] and the finite volume method [28,29] are very effective tools to solve some partial differential equations (PDEs) on complex geometries, which is applied in a wide range of engineering and biomedical disciplines [30][31][32][33][34]. In this paper, the finite volume method is implemented to calculate the NS equation.…”
Section: Resultsmentioning
confidence: 99%
“…Finite element methods [24][25][26][27] and the finite volume method [28,29] are very effective tools to solve some partial differential equations (PDEs) on complex geometries, which is applied in a wide range of engineering and biomedical disciplines [30][31][32][33][34]. In this paper, the finite volume method is implemented to calculate the NS equation.…”
Section: Resultsmentioning
confidence: 99%
“…The above governing equations were solved by our in-house finite-difference code, which has been employed and well validated in our earlier works for steady-state natural convection in an enclosure [9,18], transient or unsteady mixed convection in an enclosure [19,20], and forced convection across cylinders [21][22][23][24][25][26]. The numerical details are omitted here for simplicity.…”
Section: Methodsmentioning
confidence: 99%
“…To ensure computational accuracy and computational efficiency, the entire computational domains adopt the structured hexahedral mesh generated by ANSYS-ICEM software. It is well known that the near-wall grid distribution directly affects calculation results [45]. Therefore, a boundary layer is generated near the wall to refine the mesh to meet the y+ requirements of the turbulence model, especially on the impeller blade wall and the volute tongue wall, as shown in Figure 5.…”
Section: Computational Meshmentioning
confidence: 99%