| Citation: | DU Kun, ZHANG Rongxia, JIA Yihao, et al. Numerical study on discrete film cooling performance of non-axisymmetric endwall[J]. Journal of Aerospace Power, 2025, 40(6):20230734 doi: 10.13224/j.cnki.jasp.20230734 |
The non-axisymmetric endwall can effectively reduce the circumferential pressure difference and control the complex secondary flow inside the passage. Consequently, this enhanced the aerodynamic performance of the airfoil. The non-axisymmetric endwall significantly impacted the outlet area of the film holes and the trajectory of the coolant. The concave-convex changes along the circumferential and axial directions on a flat plate were studied to explore the effects of different shaping positions on the film cooling characteristics. A row of discrete film holes at positions of 10%
| [1] |
杜昆,陈麒好,孟宪龙,等. 陶瓷基复合材料在航空发动机热端部件应用及热分析研究进展[J]. 推进技术,2022,43(2): 210380. DU Kun,CHEN Qihao,MENG Xianlong,et al. Advancement in application and thermal analysis of ceramic matrix composites in aeroengine hot components[J]. Journal of Propulsion Technology,2022,43(2): 210380. (in Chinese
DU Kun, CHEN Qihao, MENG Xianlong, et al. Advancement in application and thermal analysis of ceramic matrix composites in aeroengine hot components[J]. Journal of Propulsion Technology, 2022, 43(2): 210380. (in Chinese)
|
| [2] |
陈娉婷,李雪英,任静,等. 燃烧室温度剖面对非轴对称端壁冷却的影响[J]. 工程热物理学报,2019,40(1): 191-197. CHEN Pingting,LI Xueying,REN Jing,et al. Influence of combustor outlet profile on a contoured vane endwall cooling[J]. Journal of Engineering Thermophysics,2019,40(1): 191-197. (in Chinese
CHEN Pingting, LI Xueying, REN Jing, et al. Influence of combustor outlet profile on a contoured vane endwall cooling[J]. Journal of Engineering Thermophysics, 2019, 40(1): 191-197. (in Chinese)
|
| [3] |
尤付浩,李相君,鲁庆,等. 基于二次流控制规律的非轴对称端壁造型优化设计[J]. 航空动力学报,2024,39(2): 20220215. YOU Fuhao,LI Xiangjun,LU Qing,et al. Non-axisymmetric endwall based on secondary flow control law modeling optimization design[J]. Journal of Aerospace Power,2024,39(2): 20220215. (in Chinese
YOU Fuhao, LI Xiangjun, LU Qing, et al. Non-axisymmetric endwall based on secondary flow control law modeling optimization design[J]. Journal of Aerospace Power, 2024, 39(2): 20220215. (in Chinese)
|
| [4] |
茅晓晨,赵磊,高丽敏,等. 进气畸变及非轴对称端壁造型对紧凑型压气机中介机匣性能的影响[J]. 航空动力学报,2024,39(1): 20220126. MAO Xiaochen,ZHAO Lei,GAO Limin,et al. Effects of inlet distortion and non-axisymmetric endwall modeling on performance of compact compressor intermediate duct[J]. Journal of Aerospace Power,2024,39(1): 20220126. (in Chinese
MAO Xiaochen, ZHAO Lei, GAO Limin, et al. Effects of inlet distortion and non-axisymmetric endwall modeling on performance of compact compressor intermediate duct[J]. Journal of Aerospace Power, 2024, 39(1): 20220126. (in Chinese)
|
| [5] |
LANGSTON L S. Secondary flows in axial turbines: a review[J]. Annals of the New York Academy of Sciences,2001,934: 11-26. doi: 10.1111/j.1749-6632.2001.tb05839.x
|
| [6] |
WANG H P,OLSON S J,GOLDSTEIN R J,et al. Flow visualization in a linear turbine cascade of high-performance turbine blades: ASME Paper GT 1995-78811 [R]. New York,US: ASME,2015.
|
| [7] |
GUO Zhendong,BU Hongyan,SONG Liming,et al. Experimental test of a 3D parameterized vane cascade with non-axisymmetric endwall[J]. Aerospace Science and Technology,2019,85: 429-442. doi: 10.1016/j.ast.2018.12.021
|
| [8] |
杜昆,贾毅豪,赵尊盛,等. 槽缝射流对高负荷涡轮非轴对称端壁冷却性能的影响研究[J]. 推进技术,2023,44(7): 2207080. DU Kun,JIA Yihao,ZHAO Zunsheng,et al. Effects of slot jet flow on non-axisymmetric endwall cooling performance in a high-load turbine[J]. Journal of Propulsion Technology,2023,44(7): 2207080. (in Chinese
DU Kun, JIA Yihao, ZHAO Zunsheng, et al. Effects of slot jet flow on non-axisymmetric endwall cooling performance in a high-load turbine[J]. Journal of Propulsion Technology, 2023, 44(7): 2207080. (in Chinese)
|
| [9] |
赵刚剑,刘波,那振喆,等. 采用新型非轴对称端壁优化设计方法提高涡轮性能的数值研究[J]. 推进技术,2014,35(5): 597-602. ZHAO Gangjian,LIU Bo,NA Zhenzhe,et al. Improving the performance of turbine based on a new optimization design method[J]. Journal of Propulsion Technology,2014,35(5): 597-602. (in Chinese
ZHAO Gangjian, LIU Bo, NA Zhenzhe, et al. Improving the performance of turbine based on a new optimization design method[J]. Journal of Propulsion Technology, 2014, 35(5): 597-602. (in Chinese)
|
| [10] |
陶志,武晓龙,祝培源,等. 非轴对称端壁造型对叶片端壁气热性能影响的研究[J]. 推进技术,2019,40(8): 1734-1742. TAO Zhi,WU Xiaolong,ZHU Peiyuan,et al. Research on effects of nonaxisymmetric endwall contouring on blade endwall aerothermal performance[J]. Journal of Propulsion Technology,2019,40(8): 1734-1742. (in Chinese
TAO Zhi, WU Xiaolong, ZHU Peiyuan, et al. Research on effects of nonaxisymmetric endwall contouring on blade endwall aerothermal performance[J]. Journal of Propulsion Technology, 2019, 40(8): 1734-1742. (in Chinese)
|
| [11] |
唐慧敏,刘帅强,罗华玲. 涡轮平面叶栅非轴对称端壁优化设计[J]. 航空动力学报,2015,30(3): 707-713. TANG Huimin,LIU Shuaiqiang,LUO Hualing. Optimal design of profiled endwall for turbine cascade[J]. Journal of Aerospace Power,2015,30(3): 707-713. (in Chinese
TANG Huimin, LIU Shuaiqiang, LUO Hualing. Optimal design of profiled endwall for turbine cascade[J]. Journal of Aerospace Power, 2015, 30(3): 707-713. (in Chinese)
|
| [12] |
田兴江,常海萍,张镜洋,等. 基于参数化脊线的非轴对称端壁成型方法[J]. 推进技术,2017,38(6): 1294-1301. TIAN Xingjiang,CHANG Haiping,ZHANG Jingyang,et al. Non-axisymmetric endwall contouring method based on parameterized ridge line[J]. China Industrial Economics,2017,38(6): 1294-1301. (in Chinese
TIAN Xingjiang, CHANG Haiping, ZHANG Jingyang, et al. Non-axisymmetric endwall contouring method based on parameterized ridge line[J]. China Industrial Economics, 2017, 38(6): 1294-1301. (in Chinese)
|
| [13] |
黄镜玮,孟福生,宋义康,等. 基于压力场分布的大子午扩张涡轮非轴对称端壁造型方法[J]. 航空动力学报,2020,35(5): 1051-1065. HUANG Jingwei,MENG Fusheng,SONG Yikang,et al. Non-axisymmetric endwall modeling for large meridional expansion turbines based on pressure field distribution[J]. Journal of Aerospace Power,2020,35(5): 1051-1065. (in Chinese
HUANG Jingwei, MENG Fusheng, SONG Yikang, et al. Non-axisymmetric endwall modeling for large meridional expansion turbines based on pressure field distribution[J]. Journal of Aerospace Power, 2020, 35(5): 1051-1065. (in Chinese)
|
| [14] |
胡书珍,吕剑波,罗华玲. 涡轮导叶非轴对称端壁技术研究[J]. 工程热物理学报,2022,43(5): 1233-1239. HU Shuzhen,LU Jianbo,LUO Hualing. Investigation of the profiled endwall for a high pressure turbine vane[J]. Journal of Engineering Thermophysics,2022,43(5): 1233-1239. (in Chinese
HU Shuzhen, LU Jianbo, LUO Hualing. Investigation of the profiled endwall for a high pressure turbine vane[J]. Journal of Engineering Thermophysics, 2022, 43(5): 1233-1239. (in Chinese)
|
| [15] |
DU Kun,JIA Yihao,SONG Hui,et al. Effect of slot jet flow on non-axisymmetric endwall cooling performance of high-load turbines[J]. Machines,2023,11(2): 134. doi: 10.3390/machines11020134
|
| [16] |
LIU Wei,WANG Songtao,WEN Fengbo. Numerical investigation of a turbine stator with nonaxisymmetric endwall profiling[J]. Journal of Thermal Science,2022,31(5): 1790-1803. doi: 10.1007/s11630-022-1673-y
|
| [17] |
白波,李志刚,李军. 轴向收敛造型对燃气涡轮叶栅端壁气膜冷却性能的影响[J]. 航空动力学报,2022,37(5): 1042-1053. BAI Bo,LI Zhigang,LI Jun. Influence of axially-convergent contouring on cascade end wall film cooling characteristics in gas turbine[J]. Journal of Aerospace Power,2022,37(5): 1042-1053. (in Chinese
BAI Bo, LI Zhigang, LI Jun. Influence of axially-convergent contouring on cascade end wall film cooling characteristics in gas turbine[J]. Journal of Aerospace Power, 2022, 37(5): 1042-1053. (in Chinese)
|
| [18] |
李志刚,白波,刘璐萱,等. 进口不重合和轴对称造型对跨声速涡轮叶栅端壁传热特性的影响[J]. 航空动力学报,2019,34(12): 2695-2705. LI Zhigang,BAI Bo,LIU Luxuan,et al. Effects of inlet misalignment and axisymmetric contouring on endwall heat transfer characteristics in transonic turbine cascade[J]. Journal of Aerospace Power,2019,34(12): 2695-2705. (in Chinese
LI Zhigang, BAI Bo, LIU Luxuan, et al. Effects of inlet misalignment and axisymmetric contouring on endwall heat transfer characteristics in transonic turbine cascade[J]. Journal of Aerospace Power, 2019, 34(12): 2695-2705. (in Chinese)
|
| [19] |
MENSCH A,THOLE K A. Overall effectiveness and flowfield measurements for an endwall with nonaxisymmetric contouring[J]. Journal of Turbomachinery,2016,138(3): 031007. doi: 10.1115/1.4031962
|
| [20] |
祝培源,陶志,姚韵嘉,等. 非轴对称端壁造型对叶片端壁综合传热特性的影响[J]. 风机技术,2019,61(6): 48-55. ZHU Peiyuan,TAO Zhi,YAO Yunjia,et al. Effects of nonaxisymmetric endwall contouring on blade endwall comprehensive heat transfer characteristics[J]. Chinese Journal of Turbomachinery,2019,61(6): 48-55. (in Chinese
ZHU Peiyuan, TAO Zhi, YAO Yunjia, et al. Effects of nonaxisymmetric endwall contouring on blade endwall comprehensive heat transfer characteristics[J]. Chinese Journal of Turbomachinery, 2019, 61(6): 48-55. (in Chinese)
|
| [21] |
CHEN Pingting,ZHAO Ke,LI Xueying,et al. Effects of varying non-axisymmetric contours of the turbine endwall on aerodynamics and heat transfer Aspects: a sensitivity analysis study[J]. International Journal of Thermal Sciences,2021,161: 106689. doi: 10.1016/j.ijthermalsci.2020.106689
|
| [22] |
杨寓全,刘存良,张杰,等. 分腔流量比对涡轮曲端壁表面冷却特性实验[J]. 航空学报,2021,42(7): 124399. YANG Yuquan,LIU Cunliang,ZHANG Jie,et al. Effect of mass flow ratios on film cooling characteristics of endwall: experimental study[J]. Acta Aeronautica et Astronautica Sinica,2021,42(7): 124399. (in Chinese
YANG Yuquan, LIU Cunliang, ZHANG Jie, et al. Effect of mass flow ratios on film cooling characteristics of endwall: experimental study[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(7): 124399. (in Chinese)
|
| [23] |
GUSTAFSON R,MAHMOOD G I,ACHARYA S. Flowfield in a film-cooled three-dimensional contoured endwall passage: aerodynamic measurements: ASME Paper GT 2007-47934 [R]. New York,US: ASME,2009.
|
| [24] |
MAHMOOD G I,GUSTAFSON R,ACHARYA S. Flow dynamics and film cooling effectiveness on a non-axisymmetric contour endwall in a two-dimensional cascade passage: ASME Paper GT 2009-48845 [R]. New York,US: ASME,2009.
|
| [25] |
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. doi: 10.1115/1.2812933
|
| [26] |
ROSE M G. Non-axisymmetric endwall profiling in the HP NGV’s of an axial flow gas turbine: ASME Paper GT 1994-78835[R]. New York,US: ASME,1994.
|