Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage

DOI10.1016/J.IJHEATMASSTRANSFER.2007.09.025zbMath1143.80335OpenAlexW2092931097MaRDI QIDQ929845

Hamn-Ching Chen, Huitao Yang, Je-Chin Han, Hee-Koo Moon

Publication date: 18 June 2008

Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijheatmasstransfer.2007.09.025

zbMATH Keywords

leading edgeCFDfilm coolinggas turbinerotating blade

Mathematics Subject Classification ID

Software, source code, etc. for problems pertaining to classical thermodynamics (80-04)

Uses Software

• FLUENT

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