Open AccessTurbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance
Author(s) -
Kaushik Saha
Publication year - 2022
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.31390/gradschool_dissertations.1774
Subject(s) - turbulator , pressure drop , trailing edge , heat transfer , coolant , turbine blade , materials science , mechanics , heat transfer enhancement , leading edge , tip clearance , turbine , turbulence , mechanical engineering , engineering , heat transfer coefficient , reynolds number , composite material , physics