2018
DOI: 10.1007/s00231-018-2470-8
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OpenFOAM based LES of slot jet impingement heat transfer at low nozzle to plate spacing using four SGS models

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Cited by 32 publications
(19 citation statements)
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“…[17]. The authors found that the κ − ε model fails to recover the oscillating behavior observed experimentally inside the SEN. Based on the previous analysis and the results presented in Shukla & Dewan [31], the transient numerical simulations presented in this work were carried out with the LES turbulence model, including the dynamicÎ o -equation SGS model as scale filtering.…”
Section: Numerical Analysis Using Cfdmentioning
confidence: 99%
“…[17]. The authors found that the κ − ε model fails to recover the oscillating behavior observed experimentally inside the SEN. Based on the previous analysis and the results presented in Shukla & Dewan [31], the transient numerical simulations presented in this work were carried out with the LES turbulence model, including the dynamicÎ o -equation SGS model as scale filtering.…”
Section: Numerical Analysis Using Cfdmentioning
confidence: 99%
“…e studied process is isothermal, and all temperature-dependent physical properties remain constant. Recently, Shukla and Dewan (2018) [13] presented a comparison of the prediction capabilities of four different subgrid stress (SGS) models for simulating the heat transfer in a slot jet impingement system with the Reynolds number of 20,000. e models analyzed in their work were Smagorinsky, WALE (wall-adapting local eddy-viscosity), k-equation, and dynamic k-equation. e authors of that work found that the velocity and turbulence profiles using the four LES models followed the trends of the experimental results.…”
Section: Governing Equations and Turbulence Modelmentioning
confidence: 99%
“…In order to numerically reproduce the flow pattern of the SEN, RANS and LES turbulence models were used previously to reproduce the internal flow pattern of the SEN [4,12,13]. In these works, it is possible to observe that RANS models could reproduce the average flow pattern; however, they do not obtain the transient dynamic flow behavior [2, 5-7, 9, 14-19].…”
Section: Introductionmentioning
confidence: 99%
“…The WALE model is developed by Nicoud and Ducros [29]. It works particularly well at near-wall conditions and at the transitional flow from laminar to turbulent [30]. Turbulence viscosity in WALE SGS is determined by Eq.…”
Section: Turbulence Sgsmentioning
confidence: 99%