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...
| Main Authors: | , , , , , |
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| Format: | Article |
| Published: |
North Atlantic University Union
2015
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| Subjects: |