Author:
Zhu Rui,Xie Gongnan,Li Shulei,Lei Jiang
Funder
National Natural Science Foundation of China
Natural Science Foundation of Shaanxi Province
Fundamental Research Funds for Central Universities of the Central South University
Higher Education Discipline Innovation Project
Basic and Applied Basic Research Foundation of Guangdong Province
Subject
Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics
Reference58 articles.
1. Gas turbine film cooling;Bogard;AIAA J. Propuls. Power,2006
2. Blowing ratio influence on jet mixing flow phenomena at the leading edge;Bohn,1999
3. An experimental study of density ratio effects on the film cooling injection from discrete holes by using Ply and PSP techniques;Johnson;Int. J. Heat Mass Transf.,2014
4. Aerodynamic losses in turbines with and without film cooling, as influenced by mainstream turbulence, surface roughness, airfoil shape, and mach number;Ligrani;Int. J. Rot. Mach.,2012
5. Large eddy simulation of compound angle hole film cooling with hole length-to-diameter ratio and internal crossflow orientation effects;Li;Int. J. Therm. Sci.,2017
Cited by
9 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