Effects of LoD and PoD in combined-hole film cooling

Film cooling technique was used to provide thermal protection for turbine components from the hot combustion gases. Combined-hole film cooling system was introduced as a way to improve the film cooling performances. In the present work, a batch of simulations using combined-hole unit involving two r...

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Main Authors: Hassan, Haswira, Abdullah, Mohammad Kamil
Format: Article
Language:English
Published: Asian Research Publishing Network (ARPN) 2017
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Online Access:http://eprints.uthm.edu.my/5407/1/AJ%202017%20%28790%29.pdf
http://eprints.uthm.edu.my/5407/
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spelling my.uthm.eprints.54072022-01-09T06:50:41Z http://eprints.uthm.edu.my/5407/ Effects of LoD and PoD in combined-hole film cooling Hassan, Haswira Abdullah, Mohammad Kamil TJ Mechanical engineering and machinery Film cooling technique was used to provide thermal protection for turbine components from the hot combustion gases. Combined-hole film cooling system was introduced as a way to improve the film cooling performances. In the present work, a batch of simulations using combined-hole unit involving two round hole of film cooling with opposite compound-angle were carried out. The aim is to determine the arrangement of combined-hole which will produces highest film cooling effectiveness. The influence of geometrical and flow parameters; distance between two holes in mainstream direction, LoD, distance between two holes in lateral direction, PoD and blowing ratio, M were considered in the present study. The present study had been carried out using steady state Reynolds Averaged Navier Stokes (RANS) analysis of ANSYS CFX, at Reynolds number, Re = 4200 and blowing ratios, M = 0.5, 1.0, and 1.5. Nine different computational models with combination of three different values of PoD and LoD have been considered. The results shows that as the PoD and M increase, the lateral coverage of film cooling also increases, while increase on LoD shows minimal impact on the spread of the coolant downstream of the cooling hole. However, the increase of PoD and M also resulting drastic decrease of film cooling effectiveness downstream of the cooling hole as a result of the lift-off phenomena. Weak interaction between the two jets along the mainstream direction cause separation and lift-off of the coolant at further downstream. In addition to laterally average film cooling effectiveness, the results of area average film cooling effectiveness were also presented to determine the optimal arrangement of combined-hole. Overall, the combined hole film cooling provide better thermal protection in comparison with the single hole configuration. Asian Research Publishing Network (ARPN) 2017 Article PeerReviewed text en http://eprints.uthm.edu.my/5407/1/AJ%202017%20%28790%29.pdf Hassan, Haswira and Abdullah, Mohammad Kamil (2017) Effects of LoD and PoD in combined-hole film cooling. ARPN Journal of Engineering and Applied Sciences, 12 (8). pp. 2509-2514. ISSN 1819-6609
institution Universiti Tun Hussein Onn Malaysia
building UTHM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tun Hussein Onn Malaysia
content_source UTHM Institutional Repository
url_provider http://eprints.uthm.edu.my/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Hassan, Haswira
Abdullah, Mohammad Kamil
Effects of LoD and PoD in combined-hole film cooling
description Film cooling technique was used to provide thermal protection for turbine components from the hot combustion gases. Combined-hole film cooling system was introduced as a way to improve the film cooling performances. In the present work, a batch of simulations using combined-hole unit involving two round hole of film cooling with opposite compound-angle were carried out. The aim is to determine the arrangement of combined-hole which will produces highest film cooling effectiveness. The influence of geometrical and flow parameters; distance between two holes in mainstream direction, LoD, distance between two holes in lateral direction, PoD and blowing ratio, M were considered in the present study. The present study had been carried out using steady state Reynolds Averaged Navier Stokes (RANS) analysis of ANSYS CFX, at Reynolds number, Re = 4200 and blowing ratios, M = 0.5, 1.0, and 1.5. Nine different computational models with combination of three different values of PoD and LoD have been considered. The results shows that as the PoD and M increase, the lateral coverage of film cooling also increases, while increase on LoD shows minimal impact on the spread of the coolant downstream of the cooling hole. However, the increase of PoD and M also resulting drastic decrease of film cooling effectiveness downstream of the cooling hole as a result of the lift-off phenomena. Weak interaction between the two jets along the mainstream direction cause separation and lift-off of the coolant at further downstream. In addition to laterally average film cooling effectiveness, the results of area average film cooling effectiveness were also presented to determine the optimal arrangement of combined-hole. Overall, the combined hole film cooling provide better thermal protection in comparison with the single hole configuration.
format Article
author Hassan, Haswira
Abdullah, Mohammad Kamil
author_facet Hassan, Haswira
Abdullah, Mohammad Kamil
author_sort Hassan, Haswira
title Effects of LoD and PoD in combined-hole film cooling
title_short Effects of LoD and PoD in combined-hole film cooling
title_full Effects of LoD and PoD in combined-hole film cooling
title_fullStr Effects of LoD and PoD in combined-hole film cooling
title_full_unstemmed Effects of LoD and PoD in combined-hole film cooling
title_sort effects of lod and pod in combined-hole film cooling
publisher Asian Research Publishing Network (ARPN)
publishDate 2017
url http://eprints.uthm.edu.my/5407/1/AJ%202017%20%28790%29.pdf
http://eprints.uthm.edu.my/5407/
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score 13.18916