2000
DOI: 10.1016/s0307-904x(00)00018-4
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Computation of the turbulent plane plume using the k–ϵ–t′2–γ model

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Cited by 9 publications
(4 citation statements)
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“…Goldberg and Apsley [20] presented k-ε turbulence model for low Reynolds number based on the following three attributes: (1) it involves neither explicit wall distance nor normal-to-wall directionality, except to the first grid point off walls; (2) it enforces time scale reliability; (3) it involves a simple wall boundary condition for k-ω. Kalita et al [21] used the k-ϵ-t′2-γ model to present the computation of the turbulent plane plume. Song et al [22] investigated turbulence models in a CFD model of a blood pump.…”
Section: Resultsmentioning
confidence: 99%
“…Goldberg and Apsley [20] presented k-ε turbulence model for low Reynolds number based on the following three attributes: (1) it involves neither explicit wall distance nor normal-to-wall directionality, except to the first grid point off walls; (2) it enforces time scale reliability; (3) it involves a simple wall boundary condition for k-ω. Kalita et al [21] used the k-ϵ-t′2-γ model to present the computation of the turbulent plane plume. Song et al [22] investigated turbulence models in a CFD model of a blood pump.…”
Section: Resultsmentioning
confidence: 99%
“…Cho and Chung [22] developed a more economical intermittency model by incorporating an intermittency transport equation into an already existing ε − k turbulence model. Several groups extended the Cho and Chung [22] intermittency model and applied this to different applications such as an axisymmetric plume [23], and a plane plume [24]. Pope [25] also calculated intermittency using a velocity-composition transported PDF and Savill [26] discussed the development of a Reynolds stress intermittency transport model for predicting intermittency in transitional flows which was subsequently used successfully by Alvani [27] to improve PDF predictions for pre-ignition mixing of combusting ignitability.…”
Section: Boersma and Lelementioning
confidence: 99%
“…x > 0 y → ∞u = u a , T = T a (10) where u o andT o are the source velocity and temperature, u a and T a are the ambient values respectively and d is the slot width at the plume exit (d/2 is the slot half-width). The equations (1)-(3) form a parabolic system and are solved by using the well established method described by Patankar [14].…”
Section: The Mathematical Modelmentioning
confidence: 99%
“…A total of 500 lateral grid cells, distributed nonuniformly, have been used. This procedure has been used extensively for both turbulent plumes (Chen and Chen [2], Kalita et al, [10]) and for laminar plumes (Haaland and Sparrow, [7], Jia, [9]). …”
Section: The Mathematical Modelmentioning
confidence: 99%