Numerical simulation of vortex combustion for various air-fuel configurations

The purpose of this research is to study the effect of various air-fuel inlet configurations to the asymmetric vortex combustor in the non-premixed combustion of methane-air mixture using the standard k-ε turbulent model on Fluent Ansys commercial CFD software. In this study, the investigation is ma...

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Main Author: Porman, Jumari
Format: Thesis
Language:English
Published: 2015
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Online Access:http://eprints.utm.my/id/eprint/48692/1/JumariPormanMFKM2015.pdf
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spelling my.utm.486922020-06-17T03:25:11Z http://eprints.utm.my/id/eprint/48692/ Numerical simulation of vortex combustion for various air-fuel configurations Porman, Jumari TJ Mechanical engineering and machinery The purpose of this research is to study the effect of various air-fuel inlet configurations to the asymmetric vortex combustor in the non-premixed combustion of methane-air mixture using the standard k-ε turbulent model on Fluent Ansys commercial CFD software. In this study, the investigation is mainly emphasizes the influence of varying the numbers of air inlet of the vortex combustor. The simulation study has been perform in two conditions which are on cold flow (non-reacting flow) using air to define the structure of vortex flow inside the vortex combustor and also on reacting flow with mixture reaction on various equivalence ratio and various configuration numbers of air-inlets. From the isothermal simulation with air, the non-reacting flow field study was found maintain the forced-vortex azimuthal velocity patterns with strongly decaying vortex structure as per previous study. A central recirculation zone (CRZ) and two secondary recirculation zone (SRZ) also found develop in the asymmetric combustor however the size of CRZ and SRZ to be found depend on the velocity inlet magnitude and numbers of air inlet port. The study on reacting flow conditions revealed by increasing the numbers of air inlet, a better chaotic mixing observed at the bottom of the combustor which judged from the temperature distributions contour in the vortex combustor. The local temperature inside the vortex combustor observed proportional to equivalence ratio. The trend of the flame height observed proportional to equivalence ratio and predicted between 10 mm to 50 mm which is comparable to previous investigation. 2015 Thesis NonPeerReviewed application/pdf en http://eprints.utm.my/id/eprint/48692/1/JumariPormanMFKM2015.pdf Porman, Jumari (2015) Numerical simulation of vortex combustion for various air-fuel configurations. Masters thesis, Universiti Teknologi Malaysia, Faculty of Mechanical Engineering. http://dms.library.utm.my:8080/vital/access/manager/Repository/vital:89330?queryType=vitalDismax&query=Numerical+simulation+of+vortex+combustion+for+various+air-fule+configurations&public=true
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Porman, Jumari
Numerical simulation of vortex combustion for various air-fuel configurations
description The purpose of this research is to study the effect of various air-fuel inlet configurations to the asymmetric vortex combustor in the non-premixed combustion of methane-air mixture using the standard k-ε turbulent model on Fluent Ansys commercial CFD software. In this study, the investigation is mainly emphasizes the influence of varying the numbers of air inlet of the vortex combustor. The simulation study has been perform in two conditions which are on cold flow (non-reacting flow) using air to define the structure of vortex flow inside the vortex combustor and also on reacting flow with mixture reaction on various equivalence ratio and various configuration numbers of air-inlets. From the isothermal simulation with air, the non-reacting flow field study was found maintain the forced-vortex azimuthal velocity patterns with strongly decaying vortex structure as per previous study. A central recirculation zone (CRZ) and two secondary recirculation zone (SRZ) also found develop in the asymmetric combustor however the size of CRZ and SRZ to be found depend on the velocity inlet magnitude and numbers of air inlet port. The study on reacting flow conditions revealed by increasing the numbers of air inlet, a better chaotic mixing observed at the bottom of the combustor which judged from the temperature distributions contour in the vortex combustor. The local temperature inside the vortex combustor observed proportional to equivalence ratio. The trend of the flame height observed proportional to equivalence ratio and predicted between 10 mm to 50 mm which is comparable to previous investigation.
format Thesis
author Porman, Jumari
author_facet Porman, Jumari
author_sort Porman, Jumari
title Numerical simulation of vortex combustion for various air-fuel configurations
title_short Numerical simulation of vortex combustion for various air-fuel configurations
title_full Numerical simulation of vortex combustion for various air-fuel configurations
title_fullStr Numerical simulation of vortex combustion for various air-fuel configurations
title_full_unstemmed Numerical simulation of vortex combustion for various air-fuel configurations
title_sort numerical simulation of vortex combustion for various air-fuel configurations
publishDate 2015
url http://eprints.utm.my/id/eprint/48692/1/JumariPormanMFKM2015.pdf
http://eprints.utm.my/id/eprint/48692/
http://dms.library.utm.my:8080/vital/access/manager/Repository/vital:89330?queryType=vitalDismax&query=Numerical+simulation+of+vortex+combustion+for+various+air-fule+configurations&public=true
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score 13.160551