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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my-usm-ep.409382018-07-06T08:05:51Z Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance 2013 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 http://eprints.usm.my/40938/ http://eprints.usm.my/40938/1/AMIR_HUSSEIN_ALI_24_pages.pdf application/pdf en public phd doctoral Universiti Sains Malaysia Pusat Pengajian Kejuruteraan Mekanik |
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Universiti Sains Malaysia |
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USM Institutional Repository |
| language |
English |
| topic |
TJ1-1570 Mechanical engineering and machinery |
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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 |
| qualification_name |
Doctor of Philosophy (PhD.) |
| qualification_level |
Doctorate |
| 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 |
| granting_institution |
Universiti Sains Malaysia |
| granting_department |
Pusat Pengajian Kejuruteraan Mekanik |
| publishDate |
2013 |
| url |
http://eprints.usm.my/40938/1/AMIR_HUSSEIN_ALI_24_pages.pdf |
| _version_ |
1747820843684069376 |