Study of utilizing double lateral sub holes at different spanwise angles on blade film cooling effectiveness
A numerical study of the effect of using double lateral sub-holes at different span-wise angles on flow structure and film-cooling performance is performed. The lateral angles for each sub-hole change from 10° to 20° at the same film-hole diameter (12.7 mm) and jet angle (35°). The flow-field analys...
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Published in | International communications in heat and mass transfer Vol. 117; p. 104728 |
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Main Authors | , , , , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.10.2020
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Subjects | |
Online Access | Get full text |
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