Novel multi-stage vortex cooling with bypass for turbine blade leading edge design considering rotational effect
Author:
Publisher
Elsevier BV
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference35 articles.
1. Influence of Biot number and geometric parameters on the overall cooling effectiveness of double wall structure with pins;Liu;Appl. Therm. Eng.,2021
2. Experimental and numerical study on film cooling effectiveness of an annular cascade endwall with different slot configuration;Tao;Int. J. Therm. Sci.,2020
3. Leading edge impingement cooling analysis with separators of a real gas turbine blade;Wu;Appl. Therm. Eng.,2022
4. Numerical study on flow and heat transfer characteristics of swirling jet on a dimpled surface with effusion holes at turbine blade leading edge;Kong;Appl. Therm. Eng.,2022
5. Effect of leading edge diameter ratio and mainstream Reynolds number on film cooling performance of rotating blade leading edge;Xie;Appl. Therm. Eng.,2021
Cited by 1 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. Transient film outflow performances of laminated cooling configurations in leading edges of turbine vane;Applied Thermal Engineering;2023-10
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