范小军,杜长河,李亮,邹佳生.4种冷却结构对叶片前缘流动换热影响的比较研究[J].西安交通大学学报,2017(07).

王纯,张勃,吉洪湖,赵旭阳.旋流冲击孔偏置方向对小尺寸涡轮叶片前缘冷却效果影响的数值研究[J].重庆理工大学学报(自然科学),2016(11).

刘友宏,任浩亮.冲击距与气膜孔方位角对旋流气膜冷却性能影响[J].推进技术,2016(07).

张鹏,付经伦,刘建军.气膜和冲击复合冷却结构耦合传热数值研究[J].工程热物理学报,2015(11).

王昌叶,刘钊,叶绿,丰镇平.叶片冲击/气膜复合冷却的数值研究[J].工程热物理学报,2015(01).

刘海涌,刘存良,武文明,王魁.斜射流梯形腔内靶面的冲击冷却换热特性实验研究[J].推进技术,2014(03).

徐虹艳,张靖周,谭晓茗.涡轮叶片尾缘内冷通道旋流冷却特性[J].航空动力学报,2014(01).

谷振鹏,邓宏武,陶智,朱剑琴.旋转状态下叶片前缘复合换热实验[J].北京航空航天大学学报,2011(11).

张宗卫,朱惠人,赵曙,郭涛.射流、旋流、出流共同作用下矩形通道换热特性[J].航空动力学报,2011(06).

刘钊,丰镇平,宋立明.实际叶片前缘冲击冷却流动和换热的数值研究[J].西安交通大学学报,2011(01).

徐国强,谢毅,丁水汀,孙纪宁,陶智.“冲击-气膜”复合式结构冷却效果数值研究[J].热科学与技术,2009(01).

Haifen Du,Ziyue Mei,Jiayao Zou,Wei Jiang,Danmei Xie.Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane[J].Entropy,2019.

Xing Yang,Zhansheng Liu,Qiang Zhao,Zhao Liu,Zhenping Feng,Fushui Guo,Liang Ding,Terrence W. Simon.Experimental and numerical investigations of overall cooling effectiveness on a vane endwall with jet impingement and film cooling[J].Applied Thermal Engineering,2019.

Liu, Zhao,Li, Jun,Feng, Zhenping.Numerical Study of Swirl Cooling in a Turbine Blade Leading-Edge Model[J].Journal of thermophysics and heat transfer,2015.

Zhao Liu,Lv Ye,Changyee Wang,Zhenping Feng.Numerical simulation on impingement and film composite cooling of blade leading edge model for gas turbine[J].Applied Thermal Engineering,2014.

Dyson Thomas E.,Bogard David G.,Piggush Justin D.,Kohli Atul.Overall Effectiveness for a Film Cooled Turbine Blade Leading Edge With Varying Hole Pitch[J].Journal of Turbomachinery,2013.

Roache P. J..Perspective: A Method for Uniform Reporting of Grid Refinement Studies[J].Journal of Fluids Engineering,1994(3).