Effects of the layout of film holes near the vane leading edge on the endwall cooling and phantom cooling of the vane suction side surface
Author:
Affiliation:
1. Institute of Turbomachinery, School of Energy & Power Engineering, Xi’an Jiaotong University, Xi’an, PR China
2. Division of Heat Transfer, Department of Energy Sciences, Lund University, Lund, Sweden
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
https://www.tandfonline.com/doi/pdf/10.1080/10407782.2017.1326788
Reference28 articles.
1. Gas Turbine Heat Transfer and Cooling Technology
2. A Review of Shaped Hole Turbine Film-Cooling Technology
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