| Citation: | HUANG Ming-hai, ZANG Shu-sheng, GE Bing, WENG Shi-lie. Method of infrared thermography measurement for temperature field of turbine vane in hot wind tunnel[J]. Journal of Aerospace Power, 2014, 29(11): 2679-2683. doi: 10.13224/j.cnki.jasp.2014.11.019 |
| [1] |
Boyle R J,Spuckler C M,Lucci B L,et al.Infrared low-temperature turbine vane rough surface heat transfer measurements[J].Journal of Turbomachinery,2001,123(1):168-177.
|
| [2] |
Gritsch M,Schulz A,Wittig S.Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits[J].Journal of Turbomachinery,1998,120(3):549-556.
|
| [3] |
Sundaram N,Thole K A.Bump and trench modifications to film-cooling holes at the vane-endwall junction[J].Journal of Turbomachinery,2008,130(4):041013.1-041013.9.
|
| [4] |
Dittmar J,Schulz A,Wittig S.Assessment of various film-cooling configurations including shaped and compound angle holes based on large-scale experiments[J].Journal of Turbomachinery,2003,125(1):57-64.
|
| [5] |
Ochs M,Schulz A,Bauer H J.Investigation of the influence of trailing edge shock waves on film cooling performance of gas turbine airfoils[R].ASME Paper GT2007-27482,2007.
|
| [6] |
Simeonides G,Van Lierde P,Van der Stichele S,et al.Infrared thermography in blowdown and intermittent hypersonic facilities[J].Journal of Thermophysics,1990,4(2):143-148.
|
| [7] |
Schulz A.Infrared thermography as applied to film cooling of gas turbine components[J].Measurement Science and Technology,2000,11(7):948-956.
|
| [8] |
Astarita T,Cardone G,Carlomagno G M.Infrared thermography:an optical method in heat transfer and fluid flow visualisation[J].Optics and Lasers in Engineering,2006,44(3/4):261-281.
|
| [9] |
Sargent S R,Hedlund C R,Ligrani P M.An infrared thermography imaging system for convective heat transfer measurements in complex flows[J].Measurement Science and Technology,1998,9(12):1974-1981.
|
| [10] |
马龙,王建华,吴向宇,等.利用红外技术进行层板冷却特性实验研究[J].航空动力学报,2008,23(4):657-661. MA Long,WANG Jianhua,WU Xiangyu,et al.Experimental investigation of the cooling performance of lamilloy using infrared thermal imaging technique[J].Journal of Aerospace Power,2008,23(4):657-661.(in Chinese)
|
| [11] |
赵鹏,刘高文,朱晓华,等.间距对凹坑强化传热和流动阻力的影响[J].航空动力学报,2009,24(10):2266-2271. ZHAO Peng,LIU Gaowen,ZHU Xiaohua,et al.Influence of dimple space on heat transfer enhancement and pressure loss in a dimpled rectangular channel[J].Journal of Aerospace Power,2009,24(10):2266-2271.(in Chinese)
|
| [12] |
吕锡嘉,王建华,刘庆东,等.应用红外热像技术实验研究层板结构冷却特性[J].航空动力学报,2009,24(10):2260-2265. LV Xijia,WANG Jianhua,LIU Qingdong,et al.Experimental investigation on cooling performance of laminated configuration using infrared thermal imaging technique[J].Journal of Aerospace Power,2009,24(10):2260-2265.(in Chinese)
|
| [13] |
ZHANG Chi,SONG Bo,LIN Yuzhen,et al.Measured overall effusion cooling effectiveness over a wide blowing ratio range using infrared imaging[J].Journal of Aerospace Power,2010,25(7):1454-1463.
|
| [14] |
常国强,常海萍,王寅会,等.曲面红外测温方向性误差分析与修正方法[J].航空动力学报,2010,25(2):302-307. CHANG Guoqiang,CHANG Haiping,WANG Yinhui,et al.Research on error analysis and correction of infrared temperature measurement for curved surface[J].Journal of Aerospace Power,2010,25(2):302-307.(in Chinese)
|
| [15] |
杨卫华,王梅娟,丁有红,等.冲击+同向对流+气膜冷却效果的试验[J].航空动力学报,2010,25(4):729-734. YANG Weihua,WANG Meijuan,DING Youhong,et al.Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling[J].Journal of Aerospace Power,2010,25(4):729-734.(in Chinese)
|
| [16] |
Aga V,Abhari R S.Influence of flow structure on compound angled film cooling effectiveness and heat transfer[J].Journal of Turbomachinery,2011,133(3):031029.1-031029.12.
|
| [17] |
Nakamata C,Mimura F,Matsushita M,et al.Local cooling effectiveness distribution of an integrated impingement and pin fin cooling configuration[R].ASME Paper GT2007-27020,2007.
|
| [18] |
Sweeney P C,Rhodes J F.An infrared technique for evaluating turbine airfoil cooling designs[J].Journal of Turbomachinery,2000,122(1):170-177.
|