Open AccessTurbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance
Author(s) -
Krishnendu Saha
Publication year - 2012
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.31390/gradschool_dissertations.1774
Subject(s) - turbulator , pressure drop , trailing edge , heat transfer , turbine blade , coolant , materials science , heat transfer enhancement , leading edge , mechanics , turbine , turbulence , tip clearance , mechanical engineering , structural engineering , engineering , heat transfer coefficient , reynolds number , composite material , physics
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