2001
DOI: 10.1002/1097-0363(20010415)35:7<763::aid-fld112>3.0.co;2-s
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Computational modelling of flow around a circular cylinder in sub-critical flow regime with various turbulence models

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Cited by 86 publications
(38 citation statements)
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“…It can be seen from the table 2 that the calculated results of case A1 are quite different from that of the simulation [7][8] and experimental results [6] . Among them, the drag coefficient is 31.3% smaller than that of experimental results, while the Strouhal number (St) is 52% larger than that of experimental results.…”
Section: Resultsmentioning
confidence: 80%
“…It can be seen from the table 2 that the calculated results of case A1 are quite different from that of the simulation [7][8] and experimental results [6] . Among them, the drag coefficient is 31.3% smaller than that of experimental results, while the Strouhal number (St) is 52% larger than that of experimental results.…”
Section: Resultsmentioning
confidence: 80%
“…This result is in keeping with the study of Franke et al (1989), who evaluated the details of the experiments of Cantwell and Coles (1983) and compared the results with numerical simulations applying the widely used standard k-ε turbulence model. A possible reason for Franke et al (1989) failing to obtain good predictions of flow field around the cylinder may be that the k-ε turbulence closure model adopted in their study is incapable of accurately predicting the turbulent flow field where the local anisotropy plays an important role (Tutar and Holdo, 2001).…”
Section: Discussion Of the Numerical Resultsmentioning
confidence: 99%
“…Two-equation turbulence closure models are the widely adopted methods in engineering applications and geophysical fluid dynamics studies because of their computational efficiency and acceptable accuracy. Bosch and Rodi (1998) and Tutar and Holdo (2001) performed numerical investigations on the influence of the turbulence closure methods of the flow around a square cylinder and a circular cylinder, respectively; however, all of them limited their studies to sub-critical flow regimes (Reynolds number around 10 5 ). In the present study, the drag coefficients of the flow on a circular cylinder are calculated at Reynolds number 10 6 (supercritical regime) using different advection schemes and turbulence models.…”
Section: Introductionmentioning
confidence: 99%
“…Alternatively a semi-or quasi-implicit form of the scheme may be employed to obtain unsteady state solutions. Unsteady state RANS solutions are often referred to as URANS solutions [15][16][17][18][19][20].…”
Section: Solution Procedures For Turbulent Flow Equationsmentioning
confidence: 99%