| Citation: | Wang Haichao, Jia Yushuai, Fang Hongyi, et al. Effect of radiation on the comprehensive cooling efficiency modalization of turbine vane and its correction[J]. Journal of Aerospace Power, 2026, 41(7):20250211 doi: 10.13224/j.cnki.jasp.20250211 |
To accurately evaluate the comprehensive cooling efficiency of turbine vane under high-temperature and high-pressure conditions, numerical simulations were performed to investigate the influence of thermal radiation on the extrapolation accuracy from low operating condition experiments. The results showed that without considering thermal radiation, the deviation between the extrapolated average comprehensive cooling efficiency and the real value was 3.14%. However, when radiation effects were included, the deviation increased significantly to 6.48%, indicating that thermal radiation was a primary factor causing modeling inaccuracy. To address this issue, a correction model in the form of a power function was constructed based on key dimensionless parameters: mainstream Reynolds number ratio, temperature ratio, and pressure ratio. The specific form of the correlation was determined using non-linear regression on multi-condition simulation data. Validation results demonstrated that after applying the proposed correction correlation, the maximum deviation of cooling efficiency between high and low operating conditions was controlled within 1.21%. The proposed method can significantly improve the accuracy of modeling prediction.
| [1] |
杨登文, 黄康, 李世峰, 等. 主流物性参数对燃气涡轮冷却叶片气热耦合性能评估影响[J]. 航空动力学报, 2026, 41(2): 20240198. Yang Dengwen, Huang Kang, Li Shifeng, et al. Effect of thermophysical property of the mainstream on the cooling performance evaluation of gas turbine vane[J]. Journal of Aerospace Power, 2026, 41(2): 20240198. (in Chinese
Yang Dengwen, Huang Kang, Li Shifeng, et al. Effect of thermophysical property of the mainstream on the cooling performance evaluation of gas turbine vane[J]. Journal of Aerospace Power, 2026, 41(2): 20240198. (in Chinese)
|
| [2] |
魏威, 张耘隆, 刘汉宇, 等. 基于离散坐标法的辐射模型研究[J]. 强度与环境, 2022, 49(5): 125-128. Wei Wei, Zhang Yunlong, Liu Hanyu, et al. The evaluation of WSGGM based on the discrete ordinates method[J]. Structure & Environment Engineering, 2022, 49(5): 125-128. (in Chinese doi: 10.19447/j.cnki.11-1773/v.2022.05.019
Wei Wei, Zhang Yunlong, Liu Hanyu, et al. The evaluation of WSGGM based on the discrete ordinates method[J]. Structure & Environment Engineering, 2022, 49(5): 125-128. (in Chinese) doi: 10.19447/j.cnki.11-1773/v.2022.05.019
|
| [3] |
成珂, 李新中, 束鹏程, 等. 蒙特卡洛法计算G型辐冷器抛物面屏耦合因子的研究[J]. 制冷学报, 2003, 24(1): 23-27. Cheng Ke, Li Xinzhong, Shu Pengcheng, et al. Research on calculating exchange factors of the parabolic reflector of the G-type radiant cooler by the Monte Carlo method[J]. Refrigeration Journal, 2003, 24(1): 23-27. (in Chinese doi: 10.3969/j.issn.0253-4339.2003.01.006
Cheng Ke, Li Xinzhong, Shu Pengcheng, et al. Research on calculating exchange factors of the parabolic reflector of the G-type radiant cooler by the Monte Carlo method[J]. Refrigeration Journal, 2003, 24(1): 23-27. (in Chinese) doi: 10.3969/j.issn.0253-4339.2003.01.006
|
| [4] |
Colladay R S, Stepka F S. Similarity constraints in testing of cooled engine parts[R]. NASA-TN-D-7707, 1974.
|
| [5] |
Asok Kumar N, Kale S R. Numerical simulation of steady state heat transfer in a ceramic-coated gas turbine blade[J]. International Journal of Heat and Mass Transfer, 2002, 45(24): 4831-4845. doi: 10.1016/S0017-9310(02)00190-4
|
| [6] |
张丽芬, 刘振侠, 廉筱纯. 气冷涡轮叶片三维换热问题计算[J]. 航空动力学报, 2007, 22(8): 1268-1272. Zhang Lifen, Liu Zhenxia, Lian Xiaochun. Numerical study of 3D heat transfer for turbine blade with air cooling[J]. Journal of Aerospace Power, 2007, 22(8): 1268-1272. (in Chinese doi: 10.3969/j.issn.1000-8055.2007.08.011
Zhang Lifen, Liu Zhenxia, Lian Xiaochun. Numerical study of 3D heat transfer for turbine blade with air cooling[J]. Journal of Aerospace Power, 2007, 22(8): 1268-1272. (in Chinese) doi: 10.3969/j.issn.1000-8055.2007.08.011
|
| [7] |
Wang Tianyi, Xuan Yimin, Han Xingsi. Analysis of transient radiation-convection coupled effects on the HP turbine blade heat load with hot streak inlet[J]. Applied Thermal Engineering, 2018, 138: 705-721. doi: 10.1016/j.applthermaleng.2018.04.110
|
| [8] |
Sun P, Li X Y, Ren J, et al. Analysis of radiation-convection coupled effects on the turbine vane with different gas compositions[R]. ASME Paper GT2020-14376, 2020.
|
| [9] |
Cao Feifei, Meng Xianlong, Fang Hongyi, et al. Investigation of scaling criteria and matching method of overall cooling effectiveness with thermal radiation[J]. Applied Thermal Engineering, 2023, 233: 121063. doi: 10.1016/j.applthermaleng.2023.121063
|
| [10] |
Vasudev S. Effects of gas radiation in scaled cooling effectiveness tests of turbine vanes[R]. AIAA-2006-5272, 2006.
|
| [11] |
Yin H, Li M F, Chi Z R, et al. Effect of radiative heat transfer factor on the temperature distribution of a first stage vane[R]. ASME Paper GT2014-25711, 2014.
|
| [12] |
王成军, 江平, 辛欣, 等. 进气温度对航空发动机燃烧室辐射换热的影响[J]. 航空发动机, 2013, 39(5): 31-33, 59. Wang Chengjun, Jiang Ping, Xin Xin, et al. Influence of inlet air temperature on radiation heat transfer for aeroengine combustor[J]. Aeroengine, 2013, 39(5): 31-33, 59. (in Chinese doi: 10.3969/j.issn.1672-3147.2013.05.007
Wang Chengjun, Jiang Ping, Xin Xin, et al. Influence of inlet air temperature on radiation heat transfer for aeroengine combustor[J]. Aeroengine, 2013, 39(5): 31-33, 59. (in Chinese) doi: 10.3969/j.issn.1672-3147.2013.05.007
|
| [13] |
刘友宏, 任浩亮. 辐射换热对平板气膜冷却性能影响[J]. 推进技术, 2017, 38(3): 588-596. Liu Youhong, Ren Haoliang. Effects of radiation heat transfer on film cooling performance of flat plate[J]. Journal of Propulsion Technology, 2017, 38(3): 588-596. (in Chinese doi: 10.13675/j.cnki.tjjs.2017.03.014
Liu Youhong, Ren Haoliang. Effects of radiation heat transfer on film cooling performance of flat plate[J]. Journal of Propulsion Technology, 2017, 38(3): 588-596. (in Chinese) doi: 10.13675/j.cnki.tjjs.2017.03.014
|
| [14] |
王睿, 刘存良, 李鹏刚, 等. 涡轮叶片前缘综合冷却效率匹配原则的验证研究[J]. 燃气涡轮试验与研究, 2025, 38(2): 110-118. Wang Rui, Liu Cunliang, Li Penggang, et al. Verification study on analogy principle of overall cooling effectiveness at turbine vane leading edge[J]. Gas Turbine Experiment and Research, 2025, 38(2): 110-118. (in Chinese doi: 10.3724/j.GTER.20250017
Wang Rui, Liu Cunliang, Li Penggang, et al. Verification study on analogy principle of overall cooling effectiveness at turbine vane leading edge[J]. Gas Turbine Experiment and Research, 2025, 38(2): 110-118. (in Chinese) doi: 10.3724/j.GTER.20250017
|
| [15] |
尹洪, 王文萍, 任静, 等. 燃烧室出口辐射对气膜冷却传热影响研究[J]. 工程热物理学报, 2012, 33(2): 214-217. Yin Hong, Wang Wenping, Ren Jing, et al. Research on the effect of combustor outlet radiation on the film cooling heat transfer[J]. Journal of Engineering Thermophysics, 2012, 33(2): 214-217. (in Chinese
Yin Hong, Wang Wenping, Ren Jing, et al. Research on the effect of combustor outlet radiation on the film cooling heat transfer[J]. Journal of Engineering Thermophysics, 2012, 33(2): 214-217. (in Chinese)
|
| [16] |
Mazzotta D W, Chyu M K, Alvin M A. Airfoil heat transfer characteristics in syngas and hydrogen turbines[R]. ASME Paper GT2007-28296, 2009.
|
| [17] |
Mick Y, Wörz B, Findeisen E, et al. Study on relevant effects concerning heat transfer of a convection cooled gas turbine blade under realistic engine temperature conditions[R]. ASME Paper GT2013-94185, 2013.
|
| [18] |
薛宪阔, 刘彦丰. O2/CO2燃烧产物辐射换热系数计算方法及影响因素分析[J]. 广东电力, 2008, 21(12): 32-34. Xue Xiankuo, Liu Yanfeng. Analysis of radiative heat transfer coefficient calculation and influencing factors of oxy-fuel combustion productions[J]. Guangdong Electric Power, 2008, 21(12): 32-34. (in Chinese doi: 10.3969/j.issn.1007-290X.2008.12.009
Xue Xiankuo, Liu Yanfeng. Analysis of radiative heat transfer coefficient calculation and influencing factors of oxy-fuel combustion productions[J]. Guangdong Electric Power, 2008, 21(12): 32-34. (in Chinese) doi: 10.3969/j.issn.1007-290X.2008.12.009
|
| [19] |
Greiner N J, Marc D, Rutledge J L, et al. Effect of variable properties and radiation on convective heat transfer measurements at engine conditions[J]. ASME Journal of Heat and Mass Transfer, 2016, 138(11): 112002. doi: 10.1115/1.4033537
|
| [20] |
Wang Tianyi, Xuan Yimin, Han Xingsi. Analysis of transient radiation-convection coupled effects on the HP turbine blade heat load with hot streak inlet[J]. Appled Thermal Engineering, 2018, 138: 705-721.
Wang Tianyi, Xuan Yimin, Han Xingsi. Analysis of transient radiation-convection coupled effects on the HP turbine blade heat load with hot streak inlet[J]. Appled Thermal Engineering, 2018, 138: 705-721.
|
| [21] |
Badinand T, Fransson T H. Influence of the reference state in the SLW model for flows with strong temperature and pressure gradients[R]. ASME Paper GT2002-30230, 2009.
|
| [22] |
王天壹, 宣益民. 热辐射对气膜冷却叶片冷却性能影响[J]. 航空动力学报, 2018, 33(8): 1801-1810. Wang Tianyi, Xuan Yimin. Effect of thermal radiation on the heat transfer performance of a film cooling vane[J]. Journal of Aerospace Power, 2018, 33(8): 1801-1810. (in Chinese doi: 10.13224/j.cnki.jasp.2018.08.002
Wang Tianyi, Xuan Yimin. Effect of thermal radiation on the heat transfer performance of a film cooling vane[J]. Journal of Aerospace Power, 2018, 33(8): 1801-1810. (in Chinese) doi: 10.13224/j.cnki.jasp.2018.08.002
|
| [23] |
饶乐威, 王天壹, 连文磊. 热辐射对气膜冷却叶片表面热负荷的影响[J]. 航空发动机, 2023, 49(4): 38-47. Rao Lewei, Wang Tianyi, Lian Wenlei. Effect of thermal radiation on the thermal load of a film-cooled vane[J]. Aeroengine, 2023, 49(4): 38-47. (in Chinese doi: 10.13477/j.cnki.aeroengine.2023.04.006
Rao Lewei, Wang Tianyi, Lian Wenlei. Effect of thermal radiation on the thermal load of a film-cooled vane[J]. Aeroengine, 2023, 49(4): 38-47. (in Chinese) doi: 10.13477/j.cnki.aeroengine.2023.04.006
|
| [24] |
Menter F R, Langtry R B, Likki S R, et al. A correlation-based transition model using local variables: Part Ⅰ model formulation[J]. Journal of Turbomachinery, 2006, 128(3): 413. doi: 10.1115/1.2184352
|
| [25] |
Langtry R B, Menter F R, Likki S R, et al. A correlation-based transition model using local variables: Part Ⅱ test cases and industrial applications[J]. Journal of Turbomachinery, 2006, 128(3): 423-434. doi: 10.1115/1.2184353
|
| [26] |
陈立立, 郭正. 基于γ-Reθt转捩模型的低雷诺数翼型数值分析[J]. 航空学报, 2016, 37(4): 1114-1126. Chen Lili, Guo Zheng. Numerical analysis for low Reynolds number airfoil based on γ-Reθt transition model[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(4): 1114-1126. (in Chinese doi: 10.7527/S1000-6893.2015.0278
Chen Lili, Guo Zheng. Numerical analysis for low Reynolds number airfoil based on γ-Reθt transition model[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(4): 1114-1126. (in Chinese) doi: 10.7527/S1000-6893.2015.0278
|
| [27] |
Raithby G D, Chui E H. A finite-volume method for predicting a radiant heat transfer in enclosures with participating media[J]. Journal of Heat Transfer, 1990, 112(2): 415-423. doi: 10.1115/1.2910394
|
| [28] |
Halila E E, Lenahan D T, Thomas T T. High pressure turbine test hardware detailed design report[R]. NASA CR-167355, 1982.
|