2015
DOI: 10.1016/j.compfluid.2015.09.013
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Turbulent flow around a square cylinder at Reynolds number 22,000: A DNS study

Abstract: The turbulent flow around a square cylinder at Reynolds number 22000 (based on the cylinder diameter and the inflow velocity) is studied by means of direct numerical simulation. An overview of the numerical methods and the methodology used to verify the simulation is presented with special emphasis to determine the proper domain size and time-integration period.

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Cited by 153 publications
(114 citation statements)
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References 53 publications
(89 reference statements)
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“…While all references agree that the peak of u ′ 1 should occur just after x 1 ≈ d, the actual value of u ′ 1 /U ∞ at its peak varies between 0.28 and 0.56. We find the peak value of u ′ 1 /U ∞ to be close to 0.41 which is in agreement with the results of Lyn et al (1995) and Trias et al (2015) which were obtained at a larger Re. Lee & Kim (2001a) are shown in Lee & Kim (2001b).…”
Section: Comparison Of Mean Flow and Turbulence Intensity Profiles Wisupporting
confidence: 82%
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“…While all references agree that the peak of u ′ 1 should occur just after x 1 ≈ d, the actual value of u ′ 1 /U ∞ at its peak varies between 0.28 and 0.56. We find the peak value of u ′ 1 /U ∞ to be close to 0.41 which is in agreement with the results of Lyn et al (1995) and Trias et al (2015) which were obtained at a larger Re. Lee & Kim (2001a) are shown in Lee & Kim (2001b).…”
Section: Comparison Of Mean Flow and Turbulence Intensity Profiles Wisupporting
confidence: 82%
“…This is in line with the results reported in Voke (1996) and Sohankar (2006) where LES simulations at Re = 22000 are compared with the reference data of Lyn et al (1995). On the other hand, significant differences are also observed in the recovery velocity: while the present results and those of Lyn et al (1995), Lee & Kim (2001b) and Trias et al (2015) show a very slow increase of U 1 /U ∞ along x 1 /d from the value of about 0.6 at x 1 /d ≈ 3 to around 0.7 at x 1 /d ≈ 8 others find the mean velocity to be over 20% higher. It is unlikely that these differences are solely due to wind tunnel blockage and free-stream turbulence.…”
Section: Comparison Of Mean Flow and Turbulence Intensity Profiles Wisupporting
confidence: 82%
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