2007
DOI: 10.1061/(asce)0733-9399(2007)133:2(213)
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Direct Numerical Simulation of Turbulent Flow in a Square Duct: Analysis of Secondary Flows

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Cited by 36 publications
(25 citation statements)
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“…Near the lower corner, a pair of counter-rotating secondary flows is observed, which are nearly symmetric along the corner bisector. These bottom secondary flows are similar to those observed in turbulent square duct flows by Gavrilakis [11], Huser and Biringen [14], and Joung et al [24]. Near the upper corner, another pair of counterrotating vortices is observed.…”
Section: Mean Flow Properties and Turbulence Structuressupporting
confidence: 87%
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“…Near the lower corner, a pair of counter-rotating secondary flows is observed, which are nearly symmetric along the corner bisector. These bottom secondary flows are similar to those observed in turbulent square duct flows by Gavrilakis [11], Huser and Biringen [14], and Joung et al [24]. Near the upper corner, another pair of counterrotating vortices is observed.…”
Section: Mean Flow Properties and Turbulence Structuressupporting
confidence: 87%
“…In the figure, the positive and negative values are denoted by solid and dashed lines, respectively. It can be seen that the distributions of all Reynolds stress components in the region away from the free surface are similar to those for square duct flows reported by Huser and Biringen [14] and Joung et al [24]. However, near the free surface, the distributions are different due to the free surface effect.…”
Section: Mean Flow Properties and Turbulence Structuressupporting
confidence: 81%
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“…Thereby, the velocity profiles are not fully developed at the nozzle exit and the turbulent intensities are of ∼10-20%, which is approximately two times the intensity found in fully developed turbulent flows in a square duct at a similar Reynolds number (see e.g., [56,57]). Furthermore, it is apparent, that measured inflow mean and rms velocity profiles differ slightly for different inclination angles, especially at the side facing the solid wall.…”
Section: Appendix B Inflow Conditions For Numerical Simulationsmentioning
confidence: 88%
“…Another key finding from the simulation, which is a consequence of these wall shear stress gradients, was that the streamwise velocity profile along the wall bisector exhibited an overshoot from the well-known logarithmic law (u + = 2.5 ln y + + 5.5) in the overlap layer when normalised by the average (across the duct perimeter) rather than local friction velocity, u τ = √ τ w /ρ, where ρ is the density. Other researchers who have conducted DNS of square duct turbulent flow and obtained similar results include Huser & Biringen (1993) and Joung, Choi & Choi (2007).…”
mentioning
confidence: 63%