Numerical investigation of film cooling effectiveness over rotating curved surfaces:blowing ratio and curvature effect

[1] Goldstein R J. Film cooling in advances in heat transfer[M]. New York, London: Academic Press, 1971:321-379 [2] Pedersen D R, Eckert E R G, Goldstein. Film-cooling with large density differences between the mainstream and secondary fluid measured by the heat-mass transfer analogy [J]. ASME Journal of Heat Transfer, 1977 ,99:620-627 [3] 韩振兴,末永洁,刘石.吹风比对气膜冷却效率影响的实验研究[J]航空学报,2004,25(6):551-555 Han Zhenxing, Mo Yongjie, Liu Shi. Experimental research on film cooling effectivenesses at different blowing ratios[J]. Acta Aeronautica et Astronautica Sinica, 2004,25(6):551-555(in Chinese) [4] Goldstein R J, Eckert E R G. Film cooling of a gas turbine blade[J]. ASME Journal of Engineering for Power, 1978,100:476-481 [5] Lin Y L, Shih T I P. Film cooling over flat, convex, and concave surfaces . AIAA-99-0344,1999 [6] Kohli A, Bogard D G. Adiabatic effectiveness, thermal fields, and velocity fields for film cooling with large angle injections[J].ASME Journalof Turbomachinery, 1997, 119:352-358 [7] 陶智,杨晓军,丁水汀,等.旋转状态下曲率对气膜与主流掺混区域的影响[J].北京航空航天大学学报, 2007,33(2):132-135 Tao Zhi, Yang Xiaojun,Ding Shuiting, et al. Curvature effects on the film cooling with the rotation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007,33(2):132-135 [8] 葛绍岩,徐靖中.气膜冷却[M].北京:科学出版社,1995 Ge Shaoyan, Xu Jingzhong. Film cooling [M]. Beijing: Science Press, 1995(in Chinese) [9] 曹玉璋,陶智,徐国强,等.航空发动机传热学[M].北京:北京航空航天大学出版社,2005:108-110 Cao Yuzhang, Tao Zhi, Xu Guoqiang, et al. Aeroengine heat transfer[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2005:108-110(in Chinese)