Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades

The inlet temperature of modern gas turbine engines has been increased to achieve higher thermal efficiency and increased output. The blade surfaces including the leading edge, suction side and pressure side are exposed to the most extreme heat loads, and therefore, must be adequately cooled to main...

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Main Author: Shaker, Sufian Farid
Format: Thesis
Language:en
Published: 2010
Subjects:
Online Access:http://eprints.usm.my/42736/1/SUFIAN_FARID_SHAKER.pdf
http://eprints.usm.my/42736/
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author Shaker, Sufian Farid
author_facet Shaker, Sufian Farid
author_sort Shaker, Sufian Farid
building Hamzah Sendut Library
collection Institutional Repository
content_provider Universiti Sains Malaysia
content_source USM Institutional Repository
continent Asia
country Malaysia
description The inlet temperature of modern gas turbine engines has been increased to achieve higher thermal efficiency and increased output. The blade surfaces including the leading edge, suction side and pressure side are exposed to the most extreme heat loads, and therefore, must be adequately cooled to maintain safety. This thesis presents steady computational predictions for a three-dimensional numerical investigation for different cooling arrangement of turbine blade model with both the internal cooling and combines cooling (film cooling) techniques.
format Thesis
id my.usm.eprints.42736
institution Universiti Sains Malaysia
language en
publishDate 2010
record_format eprints
spelling my.usm.eprints.42736 http://eprints.usm.my/42736/ Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades Shaker, Sufian Farid TJ1-1570 Mechanical engineering and machinery The inlet temperature of modern gas turbine engines has been increased to achieve higher thermal efficiency and increased output. The blade surfaces including the leading edge, suction side and pressure side are exposed to the most extreme heat loads, and therefore, must be adequately cooled to maintain safety. This thesis presents steady computational predictions for a three-dimensional numerical investigation for different cooling arrangement of turbine blade model with both the internal cooling and combines cooling (film cooling) techniques. 2010-05 Thesis NonPeerReviewed application/pdf en http://eprints.usm.my/42736/1/SUFIAN_FARID_SHAKER.pdf Shaker, Sufian Farid (2010) Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades. Masters thesis, Universiti Sains Malaysia.
spellingShingle TJ1-1570 Mechanical engineering and machinery
Shaker, Sufian Farid
Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
title Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
title_full Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
title_fullStr Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
title_full_unstemmed Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
title_short Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
title_sort finite volume based numerical investigation on the effects of internal cooling and film cooling on the thermal performance of gas turbine blades
topic TJ1-1570 Mechanical engineering and machinery
url http://eprints.usm.my/42736/1/SUFIAN_FARID_SHAKER.pdf
http://eprints.usm.my/42736/
url_provider http://eprints.usm.my/