Optimisation of a 180° U-shaped bend shape for a turbine blade cooling passage leading to a pressure loss coefficient of approximately 0.6

Published 2015 View Full Article

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Title
Optimisation of a 180° U-shaped bend shape for a turbine blade cooling passage leading to a pressure loss coefficient of approximately 0.6
Authors
Keywords
-
Journal
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
Volume 230, Issue 8, Pages 1371-1384
Publisher
SAGE Publications
Online
2015-10-24
DOI
10.1177/0954410015611148
References
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