| Citation: | GAO Limin, TU Panpan, YANG Song, et al. Fouling modeling based on multiple cosine functions and its influence on aerodynamic performance of compressor cascade[J]. Journal of Aerospace Power, 2025, 40（9）：20240379 doi: 10.13224/j.cnki.jasp.20240379
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To simulate the irregular roughness characteristics of a compressor blade surface, a geometric model describing the irregular roughness of a compressor cascade was established based on multiple cosine functions, so as to capture key parameters of compressor blade roughness characteristics. Using a diffuser cascade as the research subject, the effect of different fouling rough structure parameters on the aerodynamic performance of the diffuser cascade was investigated through numerical simulation. The results indicated that cascade fouling led to aerodynamic degradation and increase of flow loss, with the deterioration of aerodynamic performance being more pronounced with higher fouling roughness structure heights, especially at negative incidences. In comparison, the width of the fouling rough structure had a lesser effect on aerodynamic performance degradation. The total pressure loss was more sensitive to fouling than the pressure ratio; for instance, when fouling caused a maximum increase of 145.75% in total pressure loss, the corresponding pressure ratio decreased by only 3.07%.
| [1] |
TARABRIN A P, SCHUROVSKY V A, BODROV A I, et al. An analysis of axial compressor fouling and a blade cleaning method[J]. Journal of Turbomachinery, 1998, 120(2): 256-261. doi: 10.1115/1.2841400
|
| [2] |
李本威, 李冬, 李姜华, 等. 单级压气机性能衰退定量研究[J]. 航空动力学报, 2010, 25(7): 1588-1594. LI Benwei, LI Dong, LI Jianghua, et al. Quantitative research on performance degradation of single-stage compressor[J]. Journal of Aerospace Power, 2010, 25(7): 1588-1594. (in Chinese
LI Benwei, LI Dong, LI Jianghua, et al. Quantitative research on performance degradation of single-stage compressor[J]. Journal of Aerospace Power, 2010, 25(7): 1588-1594. (in Chinese)
|
| [3] |
高丽敏, 王浩浩, 杨光, 等. 关于叶片前缘加工缺陷及气动合格性的探讨[J]. 推进技术, 2023, 44(1): 22010031. GAO Limin, WANG Haohao, YANG Guang, et al. Discussion on machining defects of blade leading edge and aerodynamic qualification[J]. Journal of Propulsion Technology, 2023, 44(1): 22010031. (in Chinese
GAO Limin, WANG Haohao, YANG Guang, et al. Discussion on machining defects of blade leading edge and aerodynamic qualification[J]. Journal of Propulsion Technology, 2023, 44(1): 22010031. (in Chinese)
|
| [4] |
WHEELER A P S, SOFIA A, MILLER R J. The effect of leading-edge geometry on wake interactions in compressors[J]. Journal of Turbomachinery, 2007, 131(4): 1769-1779.
|
| [5] |
王占学, 刘增文, 叶新农. 某型涡扇发动机部件老化对性能影响的分析与计算[J]. 航空动力学报, 2007, 22(5): 792-796. WANG Zhanxue, LIU Zengwen, YE Xinnong. Effect of component deterioration on turbofan engine performance[J]. Journal of Aerospace Power, 2007, 22(5): 792-796. (in Chinese doi: 10.3969/j.issn.1000-8055.2007.05.018
WANG Zhanxue, LIU Zengwen, YE Xinnong. Effect of component deterioration on turbofan engine performance[J]. Journal of Aerospace Power, 2007, 22(5): 792-796. (in Chinese) doi: 10.3969/j.issn.1000-8055.2007.05.018
|
| [6] |
SUDER K L, CHIMA R V, STRAZISAR A J, et al. The effect of adding roughness and thickness to a transonic axial compressor rotor[J]. Journal of Turbomachinery, 1995, 117(4): 491-505. doi: 10.1115/1.2836561
|
| [7] |
高磊, 王子楠, 耿少娟, 等. 表面粗糙度对压气机叶栅损失特性影响的实验研究[J]. 推进技术, 2016, 37(7): 1263-1270. GAO Lei, WANG Zinan, GENG Shaojuan, et al. Experimental study for effects of surface roughness on compressor cascade loss characteristics[J]. Journal of Propulsion Technology, 2016, 37(7): 1263-1270. (in Chinese
GAO Lei, WANG Zinan, GENG Shaojuan, et al. Experimental study for effects of surface roughness on compressor cascade loss characteristics[J]. Journal of Propulsion Technology, 2016, 37(7): 1263-1270. (in Chinese)
|
| [8] |
孔纯彬. 表面粗糙度对扩压叶栅性能影响的试验研究[D]. 西安: 西北工业大学, 2021. KONG Chunbin. Experimental study on the effect of roughness on diffuser cascade performance[D]. Xi’an: Northwestern Polytechnical University, 2021. (in Chinese
KONG Chunbin. Experimental study on the effect of roughness on diffuser cascade performance[D]. Xi’an: Northwestern Polytechnical University, 2021. (in Chinese)
|
| [9] |
BACK S C, HOBSON G V, SONG S J, et al. Effect of surface roughness location and Reynolds number on compressor cascade performance[C]//Proceedings of ASME Turbo Expo: Power for Land, Sea, and Air. Glasgow, UK: ASME, 2010: 121-128.
|
| [10] |
BACK S C, HOBSON G V, SONG S J, et al. Effects of Reynolds number and surface roughness magnitude and location on compressor cascade performance[J]. Journal of Turbomachinery, 2012, 134(5): 051013. doi: 10.1115/1.4003821
|
| [11] |
OSVALDO V Z M. Analysis of gas turbine compressor fouling and washing on line[D]. Cranfield, UK: Cranfield University, 2007.
|
| [12] |
MORINI M, PINELLI M, SPINA P R, et al. Computational fluid dynamics simulation of fouling on axial compressor stages[J]. Journal of Engineering for Gas Turbines and Power, 2010, 132(7): 072401. doi: 10.1115/1.4000128
|
| [13] |
ALDI N, MORINI M, PINELLI M, et al. Performance evaluation of nonuniformly fouled axial compressor stages by means of computational fluid dynamics analyses[J]. Journal of Turbomachinery, 2014, 136(2): 021016. doi: 10.1115/1.4025227
|
| [14] |
程泓智, 王名扬, 周创鑫, 等. 低雷诺数下高负荷轴流压气机表面表面粗糙度流动调控机制[J]. 航空动力学报, 2022, 37(2): 283-295. CHENG Hongzhi, WANG Mingyang, ZHOU Chuangxin, et al. Surface roughness flow control mechanism of highly-loaded axial compressor under low Reynolds number conditions[J]. Journal of Aerospace Power, 2022, 37(2): 283-295. (in Chinese
CHENG Hongzhi, WANG Mingyang, ZHOU Chuangxin, et al. Surface roughness flow control mechanism of highly-loaded axial compressor under low Reynolds number conditions[J]. Journal of Aerospace Power, 2022, 37(2): 283-295. (in Chinese)
|
| [15] |
孙爽, 雷志军, 卢新根, 等. 基于表面表面粗糙度的超高负荷低压涡轮叶片附面层控制[J]. 航空动力学报, 2016, 31(4): 836-846. SUN Shuang, LEI Zhijun, LU Xingen, et al. Boundary layer control of ultra-high-lift low pressure turbine blade with surface roughness[J]. Journal of Aerospace Power, 2016, 31(4): 836-846. (in Chinese
SUN Shuang, LEI Zhijun, LU Xingen, et al. Boundary layer control of ultra-high-lift low pressure turbine blade with surface roughness[J]. Journal of Aerospace Power, 2016, 31(4): 836-846. (in Chinese)
|
| [16] |
石慧, 陈绍文, 张辰, 等. 基于动叶污垢沉积的数值模拟[J]. 航空动力学报, 2012, 27(5): 1061-1067. SHI Hui, CHEN Shaowen, ZHANG Chen, et al. Numerical simulation of fouling deposition in compressor rotor[J]. Journal of Aerospace Power, 2012, 27(5): 1061-1067. (in Chinese
SHI Hui, CHEN Shaowen, ZHANG Chen, et al. Numerical simulation of fouling deposition in compressor rotor[J]. Journal of Aerospace Power, 2012, 27(5): 1061-1067. (in Chinese)
|
| [17] |
琚亚平, 张楚华. 积垢对离心压气机叶轮气动性能的影响[J]. 工程热物理学报, 2013, 34(7): 1262-1265. JU Yaping, ZHANG Chuhua. Impact of fouling on aerodynamic performance of centrifugal compressor impeller[J]. Journal of Engineering Thermophysics, 2013, 34(7): 1262-1265. (in Chinese
JU Yaping, ZHANG Chuhua. Impact of fouling on aerodynamic performance of centrifugal compressor impeller[J]. Journal of Engineering Thermophysics, 2013, 34(7): 1262-1265. (in Chinese)
|
| [18] |
LAYCOCK R G, FLETCHER T H. Time-dependent deposition characteristics of fine coal fly ash in a laboratory gas turbine environment[J]. Journal of Turbomachinery, 2013, 135(2): 021003. doi: 10.1115/1.4006639
|
| [19] |
WANG Lisong, WANG Zhongyi, WANG Yanhua, et al. Numerical simulation of low Reynolds number 2-d rough blade compressor cascade[J]. Frontiers in Energy Research, 2022, 10: 950559. doi: 10.3389/fenrg.2022.950559
|
| [20] |
SUN Haiou, WANG Lisong, WANG Zhongyi, et al. Simulation of the effect of nonuniform fouling thickness on an axial compressor stage performance[J]. Advances in Mechanical Engineering, 2021, 13(7): 1-11.
|
| [21] |
KIM T, BLOIS G, BEST J L, et al. PIV measurements of turbulent flow overlying large, cubic- and hexagonally-packed hemisphere arrays[J]. Journal of Hydraulic Research, 2020, 58(2): 363-383. doi: 10.1080/00221686.2019.1581671
|
| [22] |
VOLINO R J, SCHULTZ M P, FLACK K A. Turbulence structure in a boundary layer with two-dimensional roughness[J]. Journal of Fluid Mechanics, 2009, 635: 75-101. doi: 10.1017/S0022112009007617
|
| [23] |
WU Y, CHRISTENSEN K T. Spatial structure of a turbulent boundary layer with irregular surface roughness[J]. Journal of Fluid Mechanics, 2010, 655: 380-418. doi: 10.1017/S0022112010000960
|
| [24] |
CLAUSER F H. Turbulent boundary layers in adverse pressure gradients[J]. Journal of the Aeronautical Sciences, 1954, 21(2): 91-108. doi: 10.2514/8.2938
|
| [25] |
BONS J P. St and Cf augmentation for real turbine roughness with elevated freestream turbulence[J]. Journal of Turbomachinery, 2002, 124(4): 632-644. doi: 10.1115/1.1505851
|
| [26] |
于海峰, 陈卫, 程礼, 等. 航空发动机压气机叶片表面积垢行为[J]. 中国表面工程, 2021, 34(5): 188-197. YU Haifeng, CHEN Wei, CHENG Li, et al. Fouling behavior of aero-engine compressor blades surface[J]. China Surface Engineering, 2021, 34(5): 188-197. (in Chinese
YU Haifeng, CHEN Wei, CHENG Li, et al. Fouling behavior of aero-engine compressor blades surface[J]. China Surface Engineering, 2021, 34(5): 188-197. (in Chinese)
|
| [27] |
RATH N, MISHRA R K, KUSHARI A. Investigation of performance degradation in a mixed flow low bypass turbofan engine[J]. Journal of Failure Analysis and Prevention, 2023, 23(1): 378-388. doi: 10.1007/s11668-023-01590-2
|
| [28] |
GBADEBO S A, HYNES T P, CUMPSTY N A. Influence of surface roughness on three-dimensional separation in axial compressors[J]. Journal of Turbomachinery, 2004, 126(4): 455-463. doi: 10.1115/1.1791281
|
| [29] |
TAYLOR R P. Surface roughness measurements on gas turbine blades[J]. Journal of Turbomachinery, 1990, 112(2): 175-180. doi: 10.1115/1.2927630
|
| [30] |
BONS J P, TAYLOR R P, MCCLAIN S T, et al. The many faces of turbine surface roughness[J]. Journal of Turbomachinery, 2001, 123(4): 739-748. doi: 10.1115/1.1400115
|
| [31] |
SUMAN A, VULPIO A, PINELLI M, et al. Microtomography of soil and soot deposits: analysis of three-dimensional structures and surface morphology[J]. Journal of Engineering for Gas Turbines and Power, 2022, 144(10): 101010. doi: 10.1115/1.4055217
|
| [32] |
TURNER A B, TARADA F H A, BAYLEY F J. Effects of surface roughness on heat transfer to gas turbine blades: AGARD-CP-390 [R]. Brussels, Belgium: Advisory Group for Aerospace Research and Development, 1985.
|
| [33] |
YUAN J, PIOMELLI U. Estimation and prediction of the roughness function on realistic surfaces[J]. Journal of Turbulence, 2014, 15(6): 350-365. doi: 10.1080/14685248.2014.907904
|
| [34] |
FLACK K A, SCHULTZ M P. Review of hydraulic roughness scales in the fully rough regime[J]. Journal of Fluids Engineering, 2010, 132(4): 041203. doi: 10.1115/1.4001492
|
| [35] |
SIGAL A, DANBERG J E. New correlation of roughness density effect on the turbulent boundary layer[J]. AIAA Journal, 1990, 28: 554-556. doi: 10.2514/3.10427
|
| [36] |
DIRLING R. A method for computing roughwall heat transfer rates on reentry nosetips: AIAA1973-763[R]. Reston, US: AIAA, 1973.
|
| [37] |
BONS J. A critical assessment of Reynolds analogy for turbine flows[J]. Journal of Heat Transfer, 2005, 127(5): 472-485. doi: 10.1115/1.1861919
|
| [38] |
THAKKAR M, BUSSE A, SANDHAM N. Surface correlations of hydrodynamic drag for transitionally rough engineering surfaces[J]. Journal of Turbulence, 2017, 18(2): 138-169. doi: 10.1080/14685248.2016.1258119
|
| [39] |
NIKURADSE J. Strömungsgesetze in rauhen Rohren[J] Journal of Applied Mathematics and Mechanics, 1933, 11(6): 409-411.
|
| [40] |
NIKURADSE J. Laws of flow in rough pipes: NACA-TM-1292[R]. Washington, US: National Advisory Committee for Aeronautics, 1950.
|
| [41] |
SCHLICHTING H. Experimentelle untersuchungen zum rauhigkeitsproblem[J]. Ingenieur-Archiv, 1936, 7(1): 1-34. doi: 10.1007/BF02084166
|
| [42] |
KADIVAR M, TORMEY D, MCGRANAGHAN G. A review on turbulent flow over rough surfaces: Fundamentals and theories[J]. International Journal of Thermofluids, 2021, 10: 100077. doi: 10.1016/j.ijft.2021.100077
|
| [43] |
高丽敏, 蔡宇桐, 徐浩亮, 等. 压气机叶片加工误差影响不确定分析[J]. 航空动力学报, 2017, 32(9): 2253-2259. GAO Limin, CAI Yutong, XU Haoliang, et al. Uncertainty analysis of machining error influence of compressor blade[J]. Journal of Aerospace Power, 2017, 32(9): 2253-2259. (in Chinese
GAO Limin, CAI Yutong, XU Haoliang, et al. Uncertainty analysis of machining error influence of compressor blade[J]. Journal of Aerospace Power, 2017, 32(9): 2253-2259. (in Chinese)
|
| [44] |
高丽敏, 蔡宇桐, 曾瑞慧, 等. 叶片加工误差对压气机叶栅气动性能的影响[J]. 推进技术, 2017, 38(3): 525-531. GAO Limin, CAI Yutong, ZENG Ruihui, et al. Effects of blade machining error on compressor cascade aerodynamic performance[J]. Journal of Propulsion Technology, 2017, 38(3): 525-531. (in Chinese
GAO Limin, CAI Yutong, ZENG Ruihui, et al. Effects of blade machining error on compressor cascade aerodynamic performance[J]. Journal of Propulsion Technology, 2017, 38(3): 525-531. (in Chinese)
|
| [45] |
高丽敏, 郭彦超, 李瑞宇, 等. 高亚声速下附面层抽吸控制压气机叶栅流动分离的研究[J]. 推进技术, 2022, 43(4): 200604. GAO Limin, GUO Yanchao, LI Ruiyu, et al. Flow separation of compressor cascade controlled by boundary layer suction at high subsonic velocity[J]. Journal of Propulsion Technology, 2022, 43(4): 200604. (in Chinese
GAO Limin, GUO Yanchao, LI Ruiyu, et al. Flow separation of compressor cascade controlled by boundary layer suction at high subsonic velocity[J]. Journal of Propulsion Technology, 2022, 43(4): 200604. (in Chinese)
|
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