Detailed flow and heat transfer analyses for an airfoil trailing-edge rib-roughened cooling channel with jet impingement
Author(s) -
Xue
Publication year - 2018
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.17760/d20292860
Subject(s) - mechanics , nusselt number , heat transfer , airfoil , turbulence , trailing edge , materials science , reynolds number , turbine blade , computational fluid dynamics , jet (fluid) , leading edge , geometry , physics , turbine , thermodynamics , mathematics
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