The effect of blowing ratio on film cooling effectiveness using cylindrical and row trenched cooling holes with alignment angle of 90 degrees
This paper presents the effects of blowing ratio on film cooling performance adjacent to the combustor endwall using cylindrical and row trenched cooling holes with alignment angle of 90 degrees. A three-dimensional representation of a Pratt and Whitney gas turbine engine was simulated and analysed...
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Hindawi Publishing
2014
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