In the calculation of a regional film cooling effectiveness covered by arrayed discrete holes
conventional computational fluid dynamics (CFD) simulations are confronted with the challenges of complex grid modeling and high computation consumption. A parameterized kernel function was proposed to describe the distribution characteristics of a single fan-shaped hole and then to predict the film cooling efficiency. Integrating data-driven machine learning technique with the Sellers film cooling efficiency superposition method
the efficient prediction of cooling efficiency distribution in the coverage area of group holes was realized. Based on the parametric "Kernel" model
the cooling effectiveness distribution for both single and triple in-line rows of 7-7-7 fan-shaped holes were successfully replicated. Furthermore
In the given region
the layout of in-line group holes with the highest average cooling efficiency in the region was obtained with integer programming method. Results show that the parametric "Kernel" model can accurately reflect the distribution characteristics of cooling efficiency in the film hole coverage area
overcoming the limitation of traditional correlation equations that only predict spanwise average cooling efficiency
and significantly reduce the number of samples required for machine learning
which can be applied to the prediction of film cooling efficiency under different working conditions.
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references
韦宏, 祖迎庆. 基于真实密度比的单/三排扇形孔气膜冷却性能及流阻特性[J]. 航空动力学报, 2021, 36(11): 2331-2343. WEI Hong, ZU Yingqing. Film cooling performance and flow resistance characteristics of single/triple-row fan-shaped holes based on actual density ratio[J]. Journal of Aerospace Power, 2021, 36(11): 2331-2343.
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 of film cooling effectiveness on leading edge with various geometries[J]. Journal of Propulsion Technology, 2008, 29(2): 153-157.
王晓增, 阚瑞, 刘存良. 密度比对弯扭导叶扇形孔气膜冷却效率的影响[J]. 航空动力学报, 2023, 38(1): 70-78. WANG Xiaozeng, KAN Rui, LIU Cunliang. Effect of density ratio on film cooling characteristics of a bowed and twisted turbine vane with fan-shaped film holes[J]. Journal of Aerospace Power, 2023, 38(1): 70-78.
唐学智, 李录平, 黄章俊, 等. 孔间距对燃气轮机动叶气膜冷却效果的影响[J]. 动力工程学报, 2018, 38(2): 105-113, 131. TANG Xuezhi, LI Luping, HUANG Zhangjun, et al. Influence of hole spacing on the film cooling effectiveness of a gas turbine moving blade[J]. Journal of Chinese Society of Power Engineering, 2018, 38(2): 105-113, 131.
魏宽, 苗辉, 秦绪山, 等. 带冲击-气膜双层壁结构的涡轮导叶冷却特性源项法数值研究[J]. 推进技术, 2022, 43(6): 185-193. WEI Kuan, MIAO Hui, QIN Xushan, et al. Numerical study on cooling characteristics of turbine guide vanes with impingement/film double wall structure using source term method[J]. Journal of Propulsion Technology, 2022, 43(6): 185-193.
尹钊, 方祥军. 基于源项法的气膜冷却涡轮叶片多目标优化[J]. 推进技术, 2013, 34(10): 1339-1344. YIN Zhao, FANG Xiangjun. Multi-objective optimization of film-cooled turbine with source term method[J]. Journal of Propulsion Technology, 2013, 34(10): 1339-1344.
张玉芳, 黄望全. 用于冲击/发散双层壁冷却数值模拟的源项法模型[J]. 南京航空航天大学学报, 2017, 49(增刊1): 24-29. ZHANG Yufang, HUANG Wangquan. Source term model for impingement/effusion double-wall cooling numerical simulation[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2017, 49(Sup1): 24-29.
汪奇, 杨力, 饶宇. 深度学习方法在涡轮冷却中的应用综述[J]. 工程热物理学报, 2022, 43(3): 656-662. WANG Qi, YANG Li, RAO Yu. A review of deep learning methods in turbine cooling[J]. Journal of Engineering Thermophysics, 2022, 43(3): 656-662.
罗磊, 邢海峰, 王松涛. 基于机器学习的单孔绝热气膜冷却效率分布预测研究[J]. 推进技术, 2022, 43(4): 213-223.LUO Lei, XING Haifeng, WANG Songtao. Prediction of adiabatic film cooling efficiency distribution of single hole based on machine learning[J]. Journal of Propulsion Technology, 2022, 43(4): 213-223.
秦晏旻, 李雪英, 任静, 等. 基于BP神经网络的多参数气膜冷却效率研究[J]. 工程热物理学报, 2011, 32(7): 1127-1130.QIN Yanmin, LI Xueying, REN Jing, et al. Prediction of the adiabatic film cooling effectiveness influnenced by multi parameters based on BP neural network[J]. Journal of Engineering Thermophysics, 2011, 32(7): 1127-1130.
李左飙, 温风波, 唐晓雷, 等. 基于深度学习的单排孔气膜冷却性能预测[J]. 航空学报, 2021, 42(4): 307-318.LI Zuobiao, WEN Fengbo, TANG Xiaolei, et al. Prediction of single-row hole film cooling performance based on deep learning[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(4): 307-318.
BALDAUF S, SCHEURLEN M, SCHULZ A, et al. Correlation of film-cooling effectiveness from thermographic measurements at enginelike conditions[J]. Journal of Turbomachinery, 2002, 124(4): 686-698.
BUNKER R S. Turbine cooling design analysis[J]. Gas Turbine Handbook, 2005(1):296-308.
COLBAN W F, THOLE K A, BOGARD D. A film-cooling correlation for shaped holes on a flat-plate surface[J]. Journal of Turbomachinery, 2011, 133(1): 011002.
林翅翔, 崔晓峰, 戴韧. 预测扇形孔气膜冷却效率的一种新关联式及应用[J]. 动力工程学报, 2023, 43(11): 1440-1447.LIN Chixiang, CUI Xiaofeng, DAI Ren. A new correlation for predicting film cooling effectiveness of fan-shaped holes and its application[J]. Journal of Chinese Society of Power Engineering, 2023, 43(11): 1440-1447.
SCHROEDER R P, THOLE K A. Adiabatic effectiveness measurements for a baseline shaped film cooling hole[C]// Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Dusseldorf, Germany: American Society of Mechanical Engineers, 2014.
SELLERS Jr J P. Gaseous film cooling with multiple injection stations[J]. AIAA Journal, 1963, 1(9): 2154-2156.