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[1]姚家旭,雷 蒋.不同横向距离下双射流孔流动与冷却特性实验研究[J].火箭推进,2018,44(01):36-43.
 YAO Jiaxu,LEI Jiang.Experimental study on flow and cooling characteristics of double-jet film-cooling holes at different spanwise distances[J].Journal of Rocket Propulsion,2018,44(01):36-43.
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不同横向距离下双射流孔流动与冷却特性实验研究

参考文献/References:

[1] SINHA A K, BOGARD D G, CRAWFORD M E. Film-cooling effectiveness downstream of a single row of holes with variable density ratio [J]. ASME journal of turbomachinery, 1991, 113(3): 442-449.
[2] HYAMS D G, LEYLEK J H. A detailed analysis of film cooling physics: Part III -streamwise injection with shaped holes[J]. ASME journal of turbomachinery, 2000, 122(1): 122-132.
[3] WRIGHT L M, MCCLAIN S T, BROWN C P, et al. Assessment of a couble hole film cooling geometry using S-PIV and PSP: GT2013-94614 [R]. USA: ASME, 2013.
[4] KUSTERER K, BOHN D, SUGIMOTO T, et al. Double-jet ejection of cooling air for improved film cooling [J]. ASME journal of turbomachinery, 2007, 129(4): 809-815.
[5] KUSTERER K, ELYAS A, BOHN D, et al. Film cooling effectiveness comparison between shaped- and double jet film cooling holes in a row arrangment [C]// Proceeings of ASME Turbo Expo 2010: Power for Land, Sea, and Air. [S.l.]: ASME, 2010: 1503-1515.
[6] WANG Z, LIU J J, AN B T, et al. Effects of axial row-spacing for double-jet film-cooling on the cooling effectiveness[C]// Proceedings of ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. [S.l.]: ASME, 2011: 483-492.
[7] WANG Z, LIU J J, ZHANG C. Impacts of geometric parameters of double-jet film cooling on anti-kidney vortex structure and cooling effectiveness: GT2013-94038 [R]. [S.l.]: ASME 2013.
[8] HAN C, REN J. Multi-parameter iInfluence on combined-hole film cooling system [J]. International journal of heat and mass transfer, 2012, 55(15): 4232-4240.
[9] HAN C, CHI Z R, REN J, et al. Optimal arrangement of combined-hole for improving film cooling effectiveness: GT2013-94561 [R]. [S.l.]: ASME, 2013.
[10] HAN J C, RALLABANDI A. Turbine blade film cooling using PSP technique [J]. Frontiers in heat and mass transfer(FHMT), 2010, 1(1): 101-109.
[11] KENDALL A, KOOCHESFAHANI M. A method for estimating wall friction in turbulent wall-bounded flows [J]. Experiments in fluids, 2008, 44(5): 773-780.
[12] WRIGHT L M, MCCLAIN S T, CLEMENSON M D. Effect of freestream turbulence intensity on film cooling jet structure and surface effectiveness using PIV and PSP [J]. ASME journal of turbomachinery, 2011, 133(4): 041023.
[13] WRIGHT L M, MCCLAIN S T, CLEMENSON M D. Effect of density ratio on flat plate film cooling with shaped holes using PSP [J]. ASME journal of turbomachinery, 2011, 133(4): 041011.
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备注/Memo

收稿日期:2017-07-09; 修回日期:2017-08-30 基金项目:国家自然科学基金(51776153) 作者简介: 姚家旭(1993—),男,硕士研究生,研究领域为燃气轮机热端部件传热与冷却

更新日期/Last Update: 1900-01-01