A comparison of cylindrical and row trenched film-cooling holes on a combustor endwall surface at high blowing ratio
This study was done to study the effects of cylindrical and row trenched cooling holes with alignment angle of ±60 degrees at blowing ratio of BR=3.18 on the film cooling effectiveness near the combustor end wall surface. In this study, a three-dimensional representation of a Pratt and Whitney gas t...
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| Format: | Article |
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Penerbit Akademia Baru
2017
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| Online Access: | http://eprints.utm.my/id/eprint/76401/ https://www.scopus.com/inward/record.uri?eid=2-s2.0-85042745358&partnerID=40&md5=78b3c24f474fbc05dfaf2b9bc758b986 |
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