[1] Makki Y H, Jakubowski G S. An Experimental Study of Film Cooling from Diffused Trapezoidal Shaped Holes[R]. AIAA 86-1326
[2] Gritsch M, Schulz A, Wittig S. Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes with Expanded Exits[R]. ASME 97-GT-164.
[3] Gritsch M, Schulz A, Wittig S. Film-Cooling Holes with Expanded Exits: Near Hole Heat Transfer Coefficients [J]. Journal of Heat Fluid Flow, 2000, 121(6):146-153.
[4] Lee K D, Kim K Y. Shape Optimization of a Fan-Shaped Hole to Enhance Film-Cooling Effectiveness[J].International Journal of Heat & Mass Transfer, 2010, 53(15-16): 2996-3005.
[5] Rao K V, Liu J S, Crites D C, et al. Enhanced Film Cooling Effectiveness with Surface Trenches[R]. ASME 2013-GT-94530
[6] Jiang H W, Han J C. Effect of Film Hole Row Location on Film Effectiveness on a Gas Turbine Blade[ J]. Journal of Heat Transfer, 1996, 118(3): 327-333.
[7] 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 Hui-ren, XIANG An-ding, XU Du-chun, et al. An Experimental Investigation of Film Cooling Effectiveness on the Surface of Turbine Blade[J]. Journal of Propulsion Technology, 2003, 24(6): 528-5 31.)
[8] 朱惠人, 马兰, 许都纯, 等. 孔位对涡轮叶片表面气膜冷却换热系数的影响[J]. 推进技术, 2005, 26(4): 302-306. (ZHU Hui-ren, MA Lan, XU Du-chun, et al. Influences of Position of Hole-Rows on Film Cooling Heat Transfer of Turbine Blade Surface[J]. Journal of Propulsion Technology, 2005, 26(4):302-306.)
[9] Winka J R, Anderson J B. Convex Curvature Effects on Film Cooling Adiabatic Effectiveness[R]. ASME 2013-GT-95243.
[10] 张宗卫, 朱惠人, 刘聪, 等. 全气膜冷却叶片表面换热系数和冷却效率研究[J]. 西安交通大学学报, 2012, 46(7): 103-107.
[11] 李红才, 朱惠人, 任战鹏, 等. 短周期风洞上动叶表面压力和换热测量[J]. 西安交通大学学报, 2013, 47(3): 114-119.
[12] 李红才, 朱惠人, 付猛. 短周期风洞中导叶表面压力和换热测量[J]. 航空动力学报, 2013, 28(4): 819-824.
[13] Arts T, Duboue J M, Rollin G. Aero-Thermal Performance Measurements and Analysis of a Two-Dimensional High Turning Rotor Blade[R]. ASME 1997-GT-120.
[14] 樊建博, 朱惠人, 刘聪, 等. 攻角对涡轮叶片表面流动及换热的影响[J]. 推进技术, 2014, 35(10):1372-1377. (FAN Jian-bo , ZHU Hui-ren, LIU Cong, et al. Effects of Different Incidences on Surface Flow and Heat Transfer in Turbine Blade[J]. Journal of Propulsion Technology, 2014, 35(10): 1372-1377.)
[15] Newman A, Xue S, Ng W, et al. Performance of a Showerhead and Shaped Hole Film Cooled Vane at High Freestream Turbulence and Transonic Conditions[R]. ASME 2011-GT-451.
[16] Oldfield M L G. Impulse Response Processing of Transient Heat Transfer Gauge Signals[J]. Journal of Turbomachinery, 2008, 130(2): 1-9.
[17] Smith D E, Bubb J V, Popp O, et al. An Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade: Part I—Steady Heat Transfer[R]. ASME 2000-GT-0202.
[18] 李红才, 朱惠人, 任战鹏, 等. 短周期跨声速风洞叶栅换热实验验证[J]. 西安交通大学学报, 2013, 47(9): 49-54.
[19] Liess C. Film Cooling with Ejection from a Row of Inclined Circular Holes: An Experimental Study for the Application to Gas Turbine Blades[M]. USA: Von Karman Institute for Fluid Dynamics, 1973.(编辑:张荣莉) * 收稿日期:2015-05-15;修订日期:2015-08-25。基金项目:国家重点基础研究发展规划资助项目(2013CB035702)。作者简介:付仲议,男,博士生,研究领域为航空发动机高温部件冷却。E-mail: 252922326@qq.com
|