Hylton L D, Mihelc M S, Turner E R, et al. Analyticaland experiment evaluation of the heat transferdistribution over the surface of turbine vane [R]. NASACR-168015, 1985.
[2]
刘高文, 刘松龄. 喷射角对涡轮叶栅端壁气膜冷却传热的影响[J]. 推进技术, 2002, 23(6): 496-512.Liu Gaowen, Liu Songling. Influence of injection angleon the thermodynamic aspects of endwall film-cooling ina turbine cascade [J]. Journal of Propulsion Technology,2002, 23(6): 496-512. (in Chinese)
[3]
苏生, 刘建军, 安柏涛. 内冷涡轮叶栅三维气热耦合数值模拟[J]. 航空动力学报, 2007, 22(12): 2018-2024.Su Sheng, Liu Jianjun, An Baitao. Numerical simulationof turbine vane with three dimensional aero-thermalcoupled heat transfer [J]. Journal of Aerospace Power,2007, 22(12): 2018-2024. (in Chinese)
[4]
吴宏, 陶智, 徐国强. 带气膜出流的旋转叶片冲击冷却的实验研究[J]. 航空动力学报, 2000, 15(4): 375-380.Wu Hong, Tao Zhi, Xu Guoqiang. Experiments ofimpinging cooling in leading edge of rotating blades withoutflow film [J]. Journal of Aerospace Power, 2000, 15(4): 375-380. (in Chinese)
[5]
Radomsky R W. Detailed boundary layer measurementson a turbine stator vane at elevated freestream turbulencelevels [C]. ASME Turbo Expo 2001: Power for Land,Sea, & Air. 2001.
[6]
Bammert K, Sandstede H. Measurements of theboundary layer development along a turbine blade withrough surfaces [J]. ASME Journal of Engineering for GasTurbines and Power, 1980, 102: 978-983.
[7]
Turner A, Tarada F, Bayley F. Effects of surfaceroughness on heat transfer to gas turbine blades [R].AGARD-CP-390, 1985.
[8]
Blair M F. An Experimental study of heat transfer in alarge-scale turbine rotor passage [J]. Journal ofTurbomachinery, 1994, 116: 1– 13.
[9]
Hoffs A, Drost U, Bolcs A. Heat transfer measurementson a turbine airfoil at various reynolds numbers andturbulence intensities including effects of surfaceroughness [C]. ASME paper 96-GT-169, 1996.
[10]
Bogard D G, Schmidt D L, Tabbita M. Characterizationand laboratory simulation of turbine airfoil surfaceroughness and associated heat transfer [J]. Journal ofTurbomachinery, 1998, 120: 337-342.
[11]
Van Fossen G J, Simoneau R J, Ching C Y. Influence ofturbulence parameters, reynolds number, and body shapeon stagnation region heat transfer [J]. Heat Transfer,1995, 117: 597-603.
[12]
Brevet P, Dorignac C, Jolly M, Vullierme J J. Heattransfer to a row of impinging jets in consideration ofoptimization [J]. Heat and Mass Transfer, 2002, 45:4191-200.
[13]
Srinath V E, David Kontrovitz. Jet Impingements heattransfer on dimpled target surface [J]. Heat and FluidFlow, 2002, 23: 22-28.
[14]
Jiang H W, Han J C. Effect of film hole row location onfilm effectives on a gas turbine blade [J]. Journal of HeatTransfer, 1996, 118: 327-333.
[15]
Ou S, Han J C, Mehendale A B, et al. Unsteady wake ona linear turbine blade cascade with air and CO2 filminjection: Part 1-effect on heat transfer coefficients [J].Journal of Turbine Machinery, 1994, 116: 721-729.
[16]
Hylton L D, Mihelc M S, Turner E R, et al. Analyticaland experiment evaluation of the heat transferdistribution over the surface of turbine vane [R]. NASACR-168015, 1983.
[17]
Medic G, Durbin P A. Toward improved prediction ofheat transfer on turbine blades [J]. Journal ofTurbomachinery, 2002, 124: 187-192.
