Experimental investigations on cooling characteristics of different trailing-edge cutback geometries
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference27 articles.
1. Gas Turbine Heat Transfer and Cooling Technology;Han,2013
2. Optimum trailing edge ejection for cooled gas turbine blades;Schobeiri;J. Turbomach.,1989
3. Investigation of the relationship between the 3D flow structure and surface heat transfer within a realistic gas turbine blade trailing edge internal serpentine cooling channel;Baek;Int. J. Heat Mass Transfer,2022
4. Cooling characteristics of the trailing-edge slot downstream from internal multi-ribbed channel;Ye;Int. J. Heat Mass Transfer,2022
5. Experimental and numerical study of turbulent flow and heat transfer in a Wedge-shaped channel with guiding pin fins for turbine blade trailing edge cooling;Liang;Int. J. Heat Mass Transfer,2021
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