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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2010
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my-usm-ep.427362019-04-12T05:26:53Z Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades 2010-05 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 http://eprints.usm.my/42736/ http://eprints.usm.my/42736/1/SUFIAN_FARID_SHAKER.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuteraan Makanikal |
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Universiti Sains Malaysia |
| collection |
USM Institutional Repository |
| language |
English |
| topic |
TJ1-1570 Mechanical engineering and machinery |
| 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 |
| 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 |
| qualification_level |
Master's degree |
| author |
Shaker, Sufian Farid |
| author_facet |
Shaker, Sufian Farid |
| author_sort |
Shaker, Sufian Farid |
| title |
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_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_sort |
finite volume based numerical investigation on the effects of internal cooling and film cooling on the thermal performance of gas
turbine blades |
| granting_institution |
Universiti Sains Malaysia |
| granting_department |
Pusat Pengajian Kejuteraan Makanikal |
| publishDate |
2010 |
| url |
http://eprints.usm.my/42736/1/SUFIAN_FARID_SHAKER.pdf |
| _version_ |
1747821095578238976 |