Citation: | Deng Hongwu, Tan Yan, Wang Jiaren, et al. Flow and heat transfer in the complex passages of turbine blade trailing edge[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(9): 1013-1016. (in Chinese) |
[1] 刘庆东.涡轮叶片新内冷结构的实验研究 .北京:北京航空航天大学能源与动力工程学院,2006 Liu Qingdong.Cooled turbine blade structure of a new experimental study .Beijing:School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,2006(in Chinese) [2] 曹玉璋,邱绪光.实验传热学[M].北京:国防工业出版社,1998 Cao Yuzhang,Qiu Xuguang.Experimental heat transfer[M].Beijing:National Defense Industry Press,1998(in Chinese) [3] 丁水汀,刘丽艳,李莉,等.涡轮叶片尾缘复合通道隔板结构[J].北京航空航天大学学报,2006,32(3):276-279 Ding Shuiting,Liu Liyan,Li Li,et al.Different structure diaphragm plates in complex passages of turbine blade trailing edge[J].Journal of Beijing University of Aeronautics and Astronautics,2006,32(3):276-279(in Chinese) [4] 丁水汀,刘丽艳,李莉,等.涡轮叶片尾缘复合通道中隔板结构对换热特性的影响[J].航空动力学报,2006,21(3):523-527 Ding Shuiting,Liu Liyan,Li Li,et al.The effect of different clapboards structure in turbine blade trailing edge complex passages on heat transfer characteristics [J].Journal of Aerospace Power,2006,21(3):523-527(in Chinese)
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