Numerical study of jet impingement cooling on a smooth curve surface

Impinging jets are a best method of achieving particularly high heat transfer coefficient and are therefore employed in many engineering applications. In this study we seek to understand the mechanism of the distributed heat on the curve surface with the goal of identifying preferred methods t...

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Main Author: Hayder, Ali Mohammed
Format: Thesis
Language:English
English
English
Published: 2014
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Online Access:http://eprints.uthm.edu.my/1437/1/24p%20ALI%20MOHAMMED%20HAYDER.pdf
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spelling my-uthm-ep.14372021-10-03T07:21:46Z Numerical study of jet impingement cooling on a smooth curve surface 2014-12 Hayder, Ali Mohammed TJ255-265 Heat engines Impinging jets are a best method of achieving particularly high heat transfer coefficient and are therefore employed in many engineering applications. In this study we seek to understand the mechanism of the distributed heat on the curve surface with the goal of identifying preferred methods to predicting jet performance. The goals that have been achieved in the numerical results displayed are determine the influence of impingement jet characteristics on thermal and flow field on a curve surface, determine the variation of Nusselt numbers (NuD) along the curve surface in order to understand the heat transfer characteristics and study the effect of position (in the center, in the mid and in the end) and angle (α=90°, 60° and 30°) of jet impingement on curve surface, different Reynolds numbers (ReD) in range of (5000, 6000, 7000, 8000 and 9000). The program, which was extracted results it is (GAMBIT 2.4.6) and (FLUENT 6.3), simulation is (2-D) in submerged jet flow and the continuity, momentum and energy equations were solved by means of a finite volume method (FVM). This study covers the effect of different Reynolds numbers (ReD) on average Nusselt numbers (Nuavg) and local Nusselt numbers (NuD). From the result, the average Nusselt numbers (Nuavg) increased with the increase of Reynolds numbers (ReD) for all cases, in comparison between different positions (center, mid and end), of nozzle on curve surface at angle (α=90°) the maximum value of average Nusselt numbers (Nuavg=388.3) is found when the nozzle locate in the end followed by the mid position and smallest value of average Nusselt numbers (Nuavg=182.25) in the center of curve surface. In case of slant angle (α=60º) the maximum value of average Nusselt numbers (Nuavg=387.47) is found when the nozzle locate in the end followed by the mid position and smallest value of average Nusselt numbers (Nuavg=308.3) in the center of curve surface. 2014-12 Thesis http://eprints.uthm.edu.my/1437/ http://eprints.uthm.edu.my/1437/1/24p%20ALI%20MOHAMMED%20HAYDER.pdf text en public http://eprints.uthm.edu.my/1437/2/ALI%20MOHAMMED%20HAYDER%20COPYRIGHT%20DECLARATION.pdf text en staffonly http://eprints.uthm.edu.my/1437/3/ALI%20MOHAMMED%20HAYDER%20WATERMARK.pdf text en validuser mphil masters Universiti Tun Hussein Onn Malaysia Fakulti Kejuruteraan Mekanikal dan Pembuatan
institution Universiti Tun Hussein Onn Malaysia
collection UTHM Institutional Repository
language English
English
English
topic TJ255-265 Heat engines
spellingShingle TJ255-265 Heat engines
Hayder, Ali Mohammed
Numerical study of jet impingement cooling on a smooth curve surface
description Impinging jets are a best method of achieving particularly high heat transfer coefficient and are therefore employed in many engineering applications. In this study we seek to understand the mechanism of the distributed heat on the curve surface with the goal of identifying preferred methods to predicting jet performance. The goals that have been achieved in the numerical results displayed are determine the influence of impingement jet characteristics on thermal and flow field on a curve surface, determine the variation of Nusselt numbers (NuD) along the curve surface in order to understand the heat transfer characteristics and study the effect of position (in the center, in the mid and in the end) and angle (α=90°, 60° and 30°) of jet impingement on curve surface, different Reynolds numbers (ReD) in range of (5000, 6000, 7000, 8000 and 9000). The program, which was extracted results it is (GAMBIT 2.4.6) and (FLUENT 6.3), simulation is (2-D) in submerged jet flow and the continuity, momentum and energy equations were solved by means of a finite volume method (FVM). This study covers the effect of different Reynolds numbers (ReD) on average Nusselt numbers (Nuavg) and local Nusselt numbers (NuD). From the result, the average Nusselt numbers (Nuavg) increased with the increase of Reynolds numbers (ReD) for all cases, in comparison between different positions (center, mid and end), of nozzle on curve surface at angle (α=90°) the maximum value of average Nusselt numbers (Nuavg=388.3) is found when the nozzle locate in the end followed by the mid position and smallest value of average Nusselt numbers (Nuavg=182.25) in the center of curve surface. In case of slant angle (α=60º) the maximum value of average Nusselt numbers (Nuavg=387.47) is found when the nozzle locate in the end followed by the mid position and smallest value of average Nusselt numbers (Nuavg=308.3) in the center of curve surface.
format Thesis
qualification_name Master of Philosophy (M.Phil.)
qualification_level Master's degree
author Hayder, Ali Mohammed
author_facet Hayder, Ali Mohammed
author_sort Hayder, Ali Mohammed
title Numerical study of jet impingement cooling on a smooth curve surface
title_short Numerical study of jet impingement cooling on a smooth curve surface
title_full Numerical study of jet impingement cooling on a smooth curve surface
title_fullStr Numerical study of jet impingement cooling on a smooth curve surface
title_full_unstemmed Numerical study of jet impingement cooling on a smooth curve surface
title_sort numerical study of jet impingement cooling on a smooth curve surface
granting_institution Universiti Tun Hussein Onn Malaysia
granting_department Fakulti Kejuruteraan Mekanikal dan Pembuatan
publishDate 2014
url http://eprints.uthm.edu.my/1437/1/24p%20ALI%20MOHAMMED%20HAYDER.pdf
http://eprints.uthm.edu.my/1437/2/ALI%20MOHAMMED%20HAYDER%20COPYRIGHT%20DECLARATION.pdf
http://eprints.uthm.edu.my/1437/3/ALI%20MOHAMMED%20HAYDER%20WATERMARK.pdf
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