Open AccessAn experimental film cooling effectiveness introducing a new film hole geometry using pressure sensitive paint technique
Author(s) -
Yuan Yao
Publication year - 2019
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.17760/d20317909
Subject(s) - airfoil , coolant , mechanical engineering , pressure sensitive paint , turbine blade , materials science , thermal , gas turbines , vortex , turbine , aerospace engineering , engineering , mechanics , thermodynamics , physics , wind tunnel
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