| Citation: | TAN Xiao-ming, ZHU Xing-dan, GUO Wen, ZHANG Jing-zhou, WANG Yong-ming, PANG Bing-hua, SU Yun-liang, LIU Song. Heat transfer experiment on film cooling of turbine blade leading edge[J]. Journal of Aerospace Power, 2014, 29(11): 2672-2678. doi: 10.13224/j.cnki.jasp.2014.11.018
|
| [1] |
Najjar Y S H,Alghamdi A S,Al-Beirutty M H.Comparative performance of combined gas turbine systems under three different blade cooling schemes[J].Applied Thermal Engineering,2004,24(13):1919-1934.
|
| [2] |
Cho H H,Rhee D H.Effects of hole arrangement on local heat/mass transfer for impingement/effusion cooling with small hole spacing[R].ASME Paper 2004-GT-53685,2004.
|
| [3] |
Lu Y P,Ekkad S V,Bunker R S.Trench film cooling:effect of trench downstream edge and hole spacing[R].ASME Paper GT2008-50606,2008.
|
| [4] |
郭文,吉洪湖,蔡毅,等.复合式气冷涡轮导叶冷却设计与试验[J].航空动力学报,2005,20(3):456-459. GUO Wen,JI Honghu,CAI Yi,et al.Design and experimental research of compound air-cooled turbine guide vane[J].Journal of Aerospace Power,2005,20(3):456-459.(in Chinese)
|
| [5] |
Koc I,Parmakszoglu C,Cakan M.Numerical investigation of film cooling effectiveness on the curved surface[J].Energy Conversion and Management,2006,47(9/10):1231-1246.
|
| [6] |
曾军,王彬,康勇.气膜冷却涡轮导向叶片流场数值模拟[J].燃气涡轮实验与研究,2006,19(4):16-19. ZENG Jun,WANG Bin,KANG Yong.Numerical simulation of flow field in a turbine stator with film cooling[J].Gas Turbine Experiment and Research,2006,19(4):16-19.(in Chinese)
|
| [7] |
朱延鑫,谭晓茗,郭文,等.叶片前缘复合冷却结构的影响分析[J].工程热物理学报,2013,34(5):938-942. ZHU Yanxin,TAN Xiaoming,GUO Wen,et al.Impact of the blade leading edge composite cooling structure[J].Journal of Engineering Thermophysics,2013,34(5):938-942.(in Chinese)
|
| [8] |
朱延鑫,谭晓茗,郭文,等.出流孔型对平板气膜冷却影响机理的研究[J].推进技术,2013,34(4):499-505. ZHU Yanxin,TAN Xiaoming,GUO Wen,et al.Numerical simulation on effects of different film cooling holes on plate[J].Journal of Propulsion Technology,2013,34(4):499-505.(in Chinese)
|
| [9] |
YAO Yu,ZHANG Jingzhou,WANG Liping.Film cooling on a gas turbine blade suction side with converging slot-hole[J].International Journal of Thermal Sciences,2013,65:267-279.
|
| [10] |
DONG Ping,WANG Qiang,GUO Zhaoyuan,et al.Conjugate calculation of gas turbine vanes cooled with leading edge films[J].Chinese Journal of Aeronautics,2009,22(2):145-152.
|
| [11] |
York W D,Leylek J H.Leading edge film cooling physics:Part Ⅰ adiabatic effectiveness[R].ASME Paper 2002-GT-30167,2002.
|
| [12] |
York W D,Leylek J H.Leading-edge film cooling physics:Part Ⅱ heat transfer coefficients[R].ASME Paper 2002-GT-30167,2002.
|
| [13] |
朱惠人,向安定,许都纯,等.涡轮叶片表面气膜冷却效率的实验研究[J].推进技术,2003,24(6):528-531. ZHU Huiren,XIANG Anding,XU Duchun,et al.An experimental investigation of film cooling effectiveness on the surface of turbine blade[J].Journal of Propulsion Technology,2003,24(6):528-531.(in Chinese)
|
| [14] |
李广超,朱惠人,白江涛,等.气膜孔布局对前缘气膜冷却效率影响的实验[J].推进技术,2008,29(2):153-157. LI Guangchao,ZHU Huiren,BAI Jiangtao,et al.Experimental investigation on film cooling effectiveness on leading edge with various geometries[J].Journal of Propulsion Technology,2008,29(2):153-157.(in Chinese)
|
| [15] |
Ekkad S V,Ou S,Rivir R B.A transient infrared thermogrpahy method for simultaneous film cooling effectiveness and heat transfer coefficient measurements from a single test[J].Journal of Turbomachinery,2004,126(4):597-603.
|
| [16] |
Lu P Y,Allison D,Ekkad S V.Turbine blade showerhead film cooling:influence of hole angle and shaping[J].International Journal of Heat and Fluid Flow,2007,28(5):922-931.
|
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