Computational Fluid Dynamics Study of a Nonpremixed Turbulent Flame Using openfoam: Effect of Chemical Mechanisms and Turbulence ModelsSource: Journal of Energy Resources Technology:;2021:;volume( 143 ):;issue: 011::page 112303-1Author:Noume, Hermann Chopkap
,
Bomba, Valentin
,
Obounou, Marcel
,
Fouda, Henri Ekobena
,
Sapnken, Flavian Emmanuel
DOI: 10.1115/1.4049740Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This article presents a study of the influence of chemical mechanisms and turbulence models on Reynolds-averaged Navier–Stokes (RANS) simulations of the CH4/H2/N2-air turbulent diffusion flame, i.e., the so-called DLR-A flame. The first part of this study is focused on the assessment of the influence of four chemical models on predicted profiles of the DLR-A flame. The chemical mechanisms considered are as follows: (i) a C2 compact skeletal mechanism, which is derived from the GRI3.0 mechanism using an improved multistage reduction method, (ii) a C1 skeletal mechanism containing 41 elementary reactions amongst 16 species, (iii) the global mechanism by Jones and Lindstedt, (iv) and a global scheme consisting of the overall reactions of methane and dihydrogen. RANS numerical results (e.g., velocities, temperature, species, or the heat production rate profiles) obtained running the reactingFOAM solver with the four chemical mechanisms as well as the standard k − ɛ model, the partially stirred reactor (PaSR) combustion model, and the P − 1 radiation model indicate that the C2 skeletal mechanism yields the best agreement with measurements. In the second part of this study, four turbulence models, namely, the standard k − ɛ model, the renormalization group (RNG) k − ɛ model, realizable k − ɛ model, and the k − ω shear stress transport (SST) model, are considered to evaluate their effects on the DLR-A flame simulation results obtained with the C2 skeletal mechanism. Results reveal that the predictions obtained with the standard k − ɛ and the RNG k − ɛ models are in very good agreement with the experimental data. Hence, for simple jet flame with moderately high Reynolds number such as the DLR-A flame, the standard k-epsilon can model the turbulence with a very good accuracy.
|
Collections
Show full item record
contributor author | Noume, Hermann Chopkap | |
contributor author | Bomba, Valentin | |
contributor author | Obounou, Marcel | |
contributor author | Fouda, Henri Ekobena | |
contributor author | Sapnken, Flavian Emmanuel | |
date accessioned | 2022-02-05T22:35:55Z | |
date available | 2022-02-05T22:35:55Z | |
date copyright | 2/12/2021 12:00:00 AM | |
date issued | 2021 | |
identifier issn | 0195-0738 | |
identifier other | jert_143_11_112303.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4277818 | |
description abstract | This article presents a study of the influence of chemical mechanisms and turbulence models on Reynolds-averaged Navier–Stokes (RANS) simulations of the CH4/H2/N2-air turbulent diffusion flame, i.e., the so-called DLR-A flame. The first part of this study is focused on the assessment of the influence of four chemical models on predicted profiles of the DLR-A flame. The chemical mechanisms considered are as follows: (i) a C2 compact skeletal mechanism, which is derived from the GRI3.0 mechanism using an improved multistage reduction method, (ii) a C1 skeletal mechanism containing 41 elementary reactions amongst 16 species, (iii) the global mechanism by Jones and Lindstedt, (iv) and a global scheme consisting of the overall reactions of methane and dihydrogen. RANS numerical results (e.g., velocities, temperature, species, or the heat production rate profiles) obtained running the reactingFOAM solver with the four chemical mechanisms as well as the standard k − ɛ model, the partially stirred reactor (PaSR) combustion model, and the P − 1 radiation model indicate that the C2 skeletal mechanism yields the best agreement with measurements. In the second part of this study, four turbulence models, namely, the standard k − ɛ model, the renormalization group (RNG) k − ɛ model, realizable k − ɛ model, and the k − ω shear stress transport (SST) model, are considered to evaluate their effects on the DLR-A flame simulation results obtained with the C2 skeletal mechanism. Results reveal that the predictions obtained with the standard k − ɛ and the RNG k − ɛ models are in very good agreement with the experimental data. Hence, for simple jet flame with moderately high Reynolds number such as the DLR-A flame, the standard k-epsilon can model the turbulence with a very good accuracy. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Computational Fluid Dynamics Study of a Nonpremixed Turbulent Flame Using openfoam: Effect of Chemical Mechanisms and Turbulence Models | |
type | Journal Paper | |
journal volume | 143 | |
journal issue | 11 | |
journal title | Journal of Energy Resources Technology | |
identifier doi | 10.1115/1.4049740 | |
journal fristpage | 112303-1 | |
journal lastpage | 112303-12 | |
page | 12 | |
tree | Journal of Energy Resources Technology:;2021:;volume( 143 ):;issue: 011 | |
contenttype | Fulltext |