Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance

The aim of this study is to investigate the effect of different kinds of cooling holes and staggered arrangements on adiabatic and conjugate film cooling effectiveness for convex surface of gas turbine blade. The investigation included a new cooling hole scheme called heart-shaped to solve the vorte...

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Main Author: Ali, Amir Hussein
Format: Thesis
Language:English
Published: 2013
Subjects:
Online Access:http://eprints.usm.my/40938/1/AMIR_HUSSEIN_ALI_24_pages.pdf
http://eprints.usm.my/40938/
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Institution: Universiti Sains Malaysia
Language: English
id my.usm.eprints.40938
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spelling my.usm.eprints.40938 http://eprints.usm.my/40938/ Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance Ali, Amir Hussein TJ1-1570 Mechanical engineering and machinery The aim of this study is to investigate the effect of different kinds of cooling holes and staggered arrangements on adiabatic and conjugate film cooling effectiveness for convex surface of gas turbine blade. The investigation included a new cooling hole scheme called heart-shaped to solve the vortex problem claimed to be responsible for the detrimental lift-off phenomenon in conventional simple cylinder film cooling holes. Also, the conjugate studies included a new conjugate blade technique called multi-layers to be helpful in speeding up the heat absorption from the upper blade surface. Fluent® has been utilized and realizable κ- 2013 Thesis NonPeerReviewed application/pdf en http://eprints.usm.my/40938/1/AMIR_HUSSEIN_ALI_24_pages.pdf Ali, Amir Hussein (2013) Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance. PhD thesis, Universiti Sains Malaysia.
institution Universiti Sains Malaysia
building Hamzah Sendut Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Sains Malaysia
content_source USM Institutional Repository
url_provider http://eprints.usm.my/
language English
topic TJ1-1570 Mechanical engineering and machinery
spellingShingle TJ1-1570 Mechanical engineering and machinery
Ali, Amir Hussein
Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
description The aim of this study is to investigate the effect of different kinds of cooling holes and staggered arrangements on adiabatic and conjugate film cooling effectiveness for convex surface of gas turbine blade. The investigation included a new cooling hole scheme called heart-shaped to solve the vortex problem claimed to be responsible for the detrimental lift-off phenomenon in conventional simple cylinder film cooling holes. Also, the conjugate studies included a new conjugate blade technique called multi-layers to be helpful in speeding up the heat absorption from the upper blade surface. Fluent® has been utilized and realizable κ-
format Thesis
author Ali, Amir Hussein
author_facet Ali, Amir Hussein
author_sort Ali, Amir Hussein
title Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
title_short Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
title_full Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
title_fullStr Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
title_full_unstemmed Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
title_sort numerical investigation on the effects of geometrical parameters on film cooling performance
publishDate 2013
url http://eprints.usm.my/40938/1/AMIR_HUSSEIN_ALI_24_pages.pdf
http://eprints.usm.my/40938/
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