Film cooling effectiveness of a leading-edge cooling array of a rotating turbine blade with twist
Author:
Publisher
Elsevier BV
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology,Fluid Flow and Transfer Processes,Mechanical Engineering
Reference36 articles.
1. Film cooling;Goldstein;Adv. Heat Transfer,1971
2. Gas turbine heat transfer and cooling technology;Han,2012
3. Stagnation region gas film cooling for turbine blade leading edge applications;Luckey;J. Aircr.,1976
4. Detailed film cooling measurements on a cylindrical leading edge model: effect of free-stream turbulence and coolant density;Ekkad;J. Turbomach.,1997
5. Stagnation film cooling and heat transfer, including its effect within the hole pattern;Mick;J. Turbomach.,1988
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Effect of film hole diameter and attack angle on the film cooling performance of leading edge with double swirl chamber under crossflow condition;Applied Thermal Engineering;2024-04
2. Experimental investigations on the heat transfer characteristic of impingement/swirl cooling structures inside turbine blade leading edge;International Communications in Heat and Mass Transfer;2024-01
3. Experimental investigations on flow characteristics of impingement/swirl cooling structures inside a blade leading edge;Physics of Fluids;2023-11-01
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