Experimental study of cooling air effect on overall cooling of laminated configuration at a turbine vane end-wall
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Engineering (miscellaneous)
Reference27 articles.
1. Fundamental gas turbine heat transfer;Han;J. Therm. Sci. Eng. Appl.,2013
2. Advanced cooling in gas turbines 2016 Max Jakob memorial award paper;Han;J. Heat Tran.,2018
3. A comparison of cylindrical and fan-shaped film-cooling holes on a vane endwall at low and high freestream turbulence levels;Colban;J. Turbomach.,2008
4. Heat transfer and film cooling for the endwall of a first stage turbine vane;Thole;Int. J. Heat Mass Tran.,2005
5. Review of platform cooling technology for high pressure turbine blades;Wright,2014
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