Investigation of film cooling effectiveness from cylindrical cooling hole with anti vortex generator by numerical simulation
This study deals numerical study of the effect of anti vortex generator (AVG) on the film cooling performance of a circular cooling hole which has diameter (d = 20 mm) on a flat plate. The interaction between the jet cooling air and mainstream will result kidney vortex which will eliminate the fi...
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2015
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my-uthm-ep.12462021-09-30T06:40:53Z Investigation of film cooling effectiveness from cylindrical cooling hole with anti vortex generator by numerical simulation 2015-07 Abu Zarida, Abdallah Ali TJ751-805 Miscellaneous motors and engines Including gas, gasoline, diesel engines This study deals numerical study of the effect of anti vortex generator (AVG) on the film cooling performance of a circular cooling hole which has diameter (d = 20 mm) on a flat plate. The interaction between the jet cooling air and mainstream will result kidney vortex which will eliminate the film cooling effectiveness. Two types of AVG with different heights (H = 0.5 d and 0.25 d) are designed to eliminate the kidney vortex and investigate best film cooling effectiveness, where each of them is mounted to the flat plate upstream of the cooling hole by changing its lateral positions (A = 0.0 d, 0.25 d, 0.5 d and 0.75 d) with respect to the hole centerline and for each type has different distance respect to hole centerline. The changing of blowing ratio (BR = 0.5-1.5) was considered in this study. As for the validation, the present study was compared with the previous research done by other researchers using the results obtained from experimental data. The steady turbulence model shear stress transport (SST) that was used to simulate a film cooling configuration. The results have been presented in terms of laterally averaged film cooling comparison graphs, velocity field on x/d = 3.0, non-dimensional temperature on x/d = 3.0 and the vorticity on x/d = 3.0 which explained how the results obtained. Cases 04 and 07 gave the best positions for AVG where case 04 gave wide covered for laterally average film cooling effectiveness , while case 07 gave the highest expand distribution and the maximum value for film cooling effectiveness . 2015-07 Thesis http://eprints.uthm.edu.my/1246/ http://eprints.uthm.edu.my/1246/2/ABDALLAH%20ALI%20ABU%20ZARIDA%20COPYRIGHT%20DECLARATION.pdf text en staffonly http://eprints.uthm.edu.my/1246/1/24p%20ABDALLAH%20ALI%20ABU%20ZARIDA.pdf text en public http://eprints.uthm.edu.my/1246/3/ABDALLAH%20ALI%20ABU%20ZARIDA%20WATERMARK.pdf text en validuser mphil masters UTHM Faculty of Mechanical and Manufacturing Engineering |
| institution |
Universiti Tun Hussein Onn Malaysia |
| collection |
UTHM Institutional Repository |
| language |
English English English |
| topic |
TJ751-805 Miscellaneous motors and engines Including gas gasoline diesel engines |
| spellingShingle |
TJ751-805 Miscellaneous motors and engines Including gas gasoline diesel engines Abu Zarida, Abdallah Ali Investigation of film cooling effectiveness from cylindrical cooling hole with anti vortex generator by numerical simulation |
| description |
This study deals numerical study of the effect of anti vortex generator (AVG) on the film
cooling performance of a circular cooling hole which has diameter (d = 20 mm) on a flat
plate. The interaction between the jet cooling air and mainstream will result kidney
vortex which will eliminate the film cooling effectiveness. Two types of AVG with
different heights (H = 0.5 d and 0.25 d) are designed to eliminate the kidney vortex and
investigate best film cooling effectiveness, where each of them is mounted to the flat
plate upstream of the cooling hole by changing its lateral positions (A = 0.0 d, 0.25 d,
0.5 d and 0.75 d) with respect to the hole centerline and for each type has different
distance respect to hole centerline. The changing of blowing ratio (BR = 0.5-1.5) was
considered in this study. As for the validation, the present study was compared with the
previous research done by other researchers using the results obtained from experimental
data. The steady turbulence model shear stress transport (SST) that was used to simulate
a film cooling configuration. The results have been presented in terms of laterally
averaged film cooling comparison graphs, velocity field on x/d = 3.0, non-dimensional
temperature on x/d = 3.0 and the vorticity on x/d = 3.0 which explained how the results
obtained. Cases 04 and 07 gave the best positions for AVG where case 04 gave wide
covered for laterally average film cooling effectiveness , while case 07 gave
the highest expand distribution and the maximum value for film cooling effectiveness
. |
| format |
Thesis |
| qualification_name |
Master of Philosophy (M.Phil.) |
| qualification_level |
Master's degree |
| author |
Abu Zarida, Abdallah Ali |
| author_facet |
Abu Zarida, Abdallah Ali |
| author_sort |
Abu Zarida, Abdallah Ali |
| title |
Investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation |
| title_short |
Investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation |
| title_full |
Investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation |
| title_fullStr |
Investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation |
| title_full_unstemmed |
Investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation |
| title_sort |
investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation |
| granting_institution |
UTHM |
| granting_department |
Faculty of Mechanical and Manufacturing Engineering |
| publishDate |
2015 |
| url |
http://eprints.uthm.edu.my/1246/2/ABDALLAH%20ALI%20ABU%20ZARIDA%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/1246/1/24p%20ABDALLAH%20ALI%20ABU%20ZARIDA.pdf http://eprints.uthm.edu.my/1246/3/ABDALLAH%20ALI%20ABU%20ZARIDA%20WATERMARK.pdf |
| _version_ |
1747830756456005632 |