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/
Abstract Abstract here
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author Ali, Amir Hussein
author_facet Ali, Amir Hussein
author_sort Ali, Amir Hussein
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-
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spelling usm-409382018-07-06T08:05:51Z 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.
spellingShingle TJ1-1570 Mechanical engineering and machinery
Ali, Amir Hussein
Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
thesis_level PhD
title 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_short 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
topic TJ1-1570 Mechanical engineering and machinery
url http://eprints.usm.my/40938/
work_keys_str_mv AT aliamirhussein numericalinvestigationontheeffectsofgeometricalparametersonfilmcoolingperformance