Author:
Chen X.,Krawciw J.,Xia H.,Denman P.A.,Bonham C.,Carrotte J.F.
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference44 articles.
1. Adiabatic and overall effectiveness measurements of an effusion cooling array for turbine endwall application;Facchini;J. Turbomach.,2010
2. A. Ceccerini, B. Facchini, L. Tarchi, D. Toni, D. Coutandin, Combined effect of slot injection, effusion array and dilution hole on the cooling performance of a real combustor liner, in: ASME Turbo Expo, American Society of Mechanical Engineers, 2009, pp. GT2009–60047.
3. Assessment of various film-cooling configurations including shaped and compound angle holes based on large-scale experiments;Dittmar;J. Turbomach.,2003
4. D. Martin, Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling, Ph.D. thesis, Loughborough University, Loughborough, UK (2013).
5. The variation of heat transfer coefficient, adiabatic effectiveness and aerodynamic loss with film cooling hole shape;Sargison;Ann. N. Y. Acad. Sci.,2001
Cited by
6 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