Thermodynamic analyzes of film cooling for a restructured cooling holes at the end of gas turbine engine combustor
This research was done to analyze the effects of two different blowing ratios of BR=1.25 and BR=3.18 on the film cooling effectiveness at the combustor outlet, whereas the cylindrical and row trench holes with alignment angle of +60 degrees were considered. In the current research, a three-dimension...
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Main Authors: | Kianpour, Ehsan, C. S., Nor Azwadi, Mohammad Hussein, Razavi, M., Akbari, Masoud, Afrand, Golshokouh, Iman |
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Format: | Article |
Published: |
North Atlantic University Union
2015
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Online Access: | http://eprints.utm.my/id/eprint/59010/ |
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