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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Bibliographic Details
Main Authors: Che Sidik, Nor Azwadi, Kianpour, Ehsan
Format: Article
Published: Hindawi Publishing 2014
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Online Access:http://eprints.utm.my/id/eprint/62870/
http://dx.doi.org/10.1155/2014/470576
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Institution: Universiti Teknologi Malaysia
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