Open AccessExperimental impingement heat transfer in a smooth channel with cross over jets and bleed holes
Author(s) -
A. gsaeng
Publication year - 2009
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.17760/d20000061
Subject(s) - reynolds number , trailing edge , nusselt number , mechanics , heat transfer , leading edge , materials science , airfoil , heat transfer enhancement , turbine blade , physics , geometry , turbine , turbulence , thermodynamics , mathematics
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