| Citation: | WANG Hao, ZHANG Haoguang, JING Fengyu, et al. Study on mechanism of slotted stator blade inhibiting boundary layer separation in a single-stage axial flow compressor[J]. Journal of Aerospace Power, 2025, 40（6）：20230520 doi: 10.13224/j.cnki.jasp.20230520
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The mechanism of slotted stator blade controlling boundary layer separations was studied, and the transonic single-stage axial flow compressor NASA Stage 35 was selected as the research object. Based on three front slot outlet positions and two rear slot outlet positions, six double-slot schemes were designed. The numerical calculation results indicated that under small and medium mass flow rate conditions, all the schemes improved the compressor total performance. When the outlets of front slot and rear slot were located at 13%
| [1] |
ZHANG Haoguang,WANG Hao,DONG Feiyang,et al. Mechanism study on the effect of self-circulating casing treatment with different circumferential coverage ratios on the axial compressor stability[J]. 2023,35(5): 056112.
|
| [2] |
ZHANG Haoguang,WANG Hao,LI Qi,et al. Mechanism underlying the effect of self-circulating casings with different circumferential coverage ratios on the aerodynamic performance of a transonic centrifugal compressor[J]. Aerospace,2023,10(3): 312. doi: 10.3390/aerospace10030312
|
| [3] |
LI Jiabin,JI Lucheng. Efficient design method for applying vortex generators in turbomachinery[J]. Journal of Turbomachinery,2019,141(8): 081005. doi: 10.1115/1.4042990
|
| [4] |
李嘉宾,季路成,伊卫林. 叶片通道内涡流发生器变工况适应性[J]. 航空动力学报,2019,34(3): 728-736. LI Jiabin,JI Lucheng,YI Weilin. Load adaptability of vortex generators in blade passage[J]. Journal of Aerospace Power,2019,34(3): 728-736. (in Chinese
LI Jiabin, JI Lucheng, YI Weilin. Load adaptability of vortex generators in blade passage[J]. Journal of Aerospace Power, 2019, 34(3): 728-736. (in Chinese)
|
| [5] |
吴培根,王如根,罗凯,等. 开槽叶片对大转角扩压叶栅性能的影响[J]. 航空动力学报,2013,28(11): 2503-2509. WU Peigen,WANG Rugen,LUO Kai,et al. Effect of slotted blade on performance of high-turning angle compressor cascades[J]. Journal of Aerospace Power,2013,28(11): 2503-2509. (in Chinese
WU Peigen, WANG Rugen, LUO Kai, et al. Effect of slotted blade on performance of high-turning angle compressor cascades[J]. Journal of Aerospace Power, 2013, 28(11): 2503-2509. (in Chinese)
|
| [6] |
张相毅,周敏,王如根,等. 叶片压力面到吸力面射流对其气动特性的影响[J]. 空气动力学学报,2006,24(2): 152-156. ZHANG Xiangyi,ZHOU Min,WANG Rugen,et al. Research on the effect of jet flow from pressure surface to suction surface on performance of blade[J]. Acta Aerodynamica Sinica,2006,24(2): 152-156. (in Chinese doi: 10.3969/j.issn.0258-1825.2006.02.003
ZHANG Xiangyi, ZHOU Min, WANG Rugen, et al. Research on the effect of jet flow from pressure surface to suction surface on performance of blade[J]. Acta Aerodynamica Sinica, 2006, 24(2): 152-156. (in Chinese) doi: 10.3969/j.issn.0258-1825.2006.02.003
|
| [7] |
曹志远. 附面层抽吸对轴流压气机流动控制及性能影响的研究[D]. 西安: 西北工业大学,2014. CAO Zhiyuan. Study on the influence of boundary layer suction on flow control and performance of axial flow compressor[D]. Xi’an: Northwestern Polytechnical University,2014. (in Chinese
CAO Zhiyuan. Study on the influence of boundary layer suction on flow control and performance of axial flow compressor[D]. Xi’an: Northwestern Polytechnical University, 2014. (in Chinese)
|
| [8] |
SIEMANN J,KRENZ I,SEUME J R. Experimental investigation of aspiration in a multi-stage high-speed axial-compressor[R]. Seoul,Korea: ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition,2016.
|
| [9] |
HEINRICH A,TIEDEMANN C,PEITSCH D. Experimental investigations of the aerodynamics of highly loaded tandem vanes in a high-speed stator cascade[R]. Madrid,Spain: 11th European Conference on Turbomachinery Fluiddynamics & Thermodynamics,2015.
|
| [10] |
张金欧文,庄皓琬,滕金芳. 轴流压气机串列静子叶片弯掠设计优化[J]. 科学技术与工程,2020,20(32): 13482-13486. ZHANG Jinouwen,ZHUANG Haowan,TENG Jinfang. Design optimization of axial compressor tandem stators using sweep and dihedral[J]. Science Technology and Engineering,2020,20(32): 13482-13486. (in Chinese doi: 10.3969/j.issn.1671-1815.2020.32.056
ZHANG Jinouwen, ZHUANG Haowan, TENG Jinfang. Design optimization of axial compressor tandem stators using sweep and dihedral[J]. Science Technology and Engineering, 2020, 20(32): 13482-13486. (in Chinese) doi: 10.3969/j.issn.1671-1815.2020.32.056
|
| [11] |
KAN Xiaoxu,WU Wanyang,ZHONG Jingjun. Effects of vortex dynamics mechanism of blade-end treatment on the flow losses in a compressor cascade at critical condition[J]. Aerospace Science and Technology,2020,102: 105857. doi: 10.1016/j.ast.2020.105857
|
| [12] |
GRIEPENTROG H F L. Performance prediction for high turning low aspect ratio stator cascades in the transonic regime[J]. Journal of Engineering for Power,1970,92(4): 390-398. doi: 10.1115/1.3445369
|
| [13] |
RAMZI M,BOIS G,ABDERRAHMANE G. Numerical study of passive control with slotted blading in highly loaded compressor cascade at low Mach number[J]. International Journal of Fluid Machinery and Systems,2011,4(1): 97-103. doi: 10.5293/IJFMS.2011.4.1.097
|
| [14] |
RAMZI M,ABDERRAHMANE G. Passive control via slotted blading in a compressor cascade at stall condition[J]. Journal of Applied Fluid Mechanics,2013,6(4): 571-580.
|
| [15] |
穆小强,陆利蓬. 叶根开槽叶栅对角区分离的控制[J]. 燃气涡轮试验与研究,2007,20(3): 28-33. MU Xiaoqiang,LU Lipeng. Corner separation control by bleed slot at the root of blade[J]. Gas Turbine Experiment and Research,2007,20(3): 28-33. (in Chinese doi: 10.3969/j.issn.1672-2620.2007.03.007
MU Xiaoqiang, LU Lipeng. Corner separation control by bleed slot at the root of blade[J]. Gas Turbine Experiment and Research, 2007, 20(3): 28-33. (in Chinese) doi: 10.3969/j.issn.1672-2620.2007.03.007
|
| [16] |
唐雨萌,柳阳威,陆利蓬. 高负荷叶栅角区分离的叶片端区开槽实验研究[J]. 工程热物理学报,2020,41(4): 845-850. TANG Yumeng,LIU Yangwei,LU Lipeng. Experimental investigation of the blade end slots on controlling the corner separation in a highly loaded compressor cascade[J]. Journal of Engineering Thermophysics,2020,41(4): 845-850. (in Chinese
TANG Yumeng, LIU Yangwei, LU Lipeng. Experimental investigation of the blade end slots on controlling the corner separation in a highly loaded compressor cascade[J]. Journal of Engineering Thermophysics, 2020, 41(4): 845-850. (in Chinese)
|
| [17] |
TANG Yumeng,LIU Yangwei,LU Lipeng,et al. Experimental investigation of flow control using blade end slots in a highly loaded compressor cascade[R]. Hawaii,US: 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery,2017.
|
| [18] |
王何建,刘波,张博涛. 大弯角开槽叶栅槽道位置与结构研究[J]. 推进技术,2021,42(12): 2675-2683. WANG Hejian,LIU Bo,ZHANG Botao. Slot position and structure of large camber slotted cascades[J]. Journal of Propulsion Technology,2021,42(12): 2675-2683. (in Chinese
WANG Hejian, LIU Bo, ZHANG Botao. Slot position and structure of large camber slotted cascades[J]. Journal of Propulsion Technology, 2021, 42(12): 2675-2683. (in Chinese)
|
| [19] |
ROCKENBACH R W. Single stage experimental evaluation of slotted rotor and stator blading: Part Ⅸ final report[R]. NASA CR-54553,1968.
|
| [20] |
胡加国,王如根,李坤,等. 跨声速压气机叶尖开槽射流扩稳策略探究[J]. 推进技术,2014,35(11): 1475-1481. HU Jiaguo,WANG Rugen,LI Kun,et al. Investigation on slot jetting flow method and mechanism of transonic compressor[J]. Journal of Propulsion Technology,2014,35(11): 1475-1481. (in Chinese
HU Jiaguo, WANG Rugen, LI Kun, et al. Investigation on slot jetting flow method and mechanism of transonic compressor[J]. Journal of Propulsion Technology, 2014, 35(11): 1475-1481. (in Chinese)
|
| [21] |
YOON S,AJAY R,CHALUVADI V,et al. A passive flow control to mitigate the corner separation in an axial compressor by a slotted rotor blade[R]. Phoenix,US: ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition,2019.
|
| [22] |
吴培根,王如根,胡加国,等. 槽道出口位置对高负荷扩压叶栅性能的影响[J]. 热能动力工程,2014,29(2): 121-126,213. WU Peigen,WANG Rugen,HU Jiaguo,et al. Influence of the location of the slot at the outlet on the performance of a highly-loaded diffusion cascade[J]. Journal of Engineering for Thermal Energy and Power,2014,29(2): 121-126,213. (in Chinese
WU Peigen, WANG Rugen, HU Jiaguo, et al. Influence of the location of the slot at the outlet on the performance of a highly-loaded diffusion cascade[J]. Journal of Engineering for Thermal Energy and Power, 2014, 29(2): 121-126, 213. (in Chinese)
|
| [23] |
REID L,MOORE R. Design and overall performance of four highly loaded,high speed inlet stages for an advanced high-pressure-ratio core compressor[R]. NASA Technical Paper 1337,1978.
|
| [24] |
REID L,MOORE R D. Performance of a single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26,respectively,and with design pressure ratio of 1.82[R]. NASA TP-1338,1978.
|
| [25] |
WEIGL H J,PADUANO J D,FRECHETTE L G,et al. Active stabilization of rotating stall and surge in a transonic single stage axial compressor[J]. Journal of Turbomachinery,1998,120: 625-636. doi: 10.1115/1.2841772
|
| [26] |
李相君. 高负荷轴流压气机端区流动机制及被动控制[D]. 西安: 西北工业大学,2018. LI Xiangjun. Flow mechanism and passive control of high-load axial compressor end region[D]. Xi’an: Northwestern Polytechnical University,2018. (in Chinese
LI Xiangjun. Flow mechanism and passive control of high-load axial compressor end region[D]. Xi’an: Northwestern Polytechnical University, 2018. (in Chinese)
|
| [27] |
周敏,王如根,曾令君,等. 槽道宽度对压气机叶栅气动性能的影响[J]. 航空动力学报,2008,23(6): 1077-1081. ZHOU Min,WANG Rugen,ZENG Lingjun,et al. Effect of slot width on the aerodynamic performance of compressor cascade[J]. Journal of Aerospace Power,2008,23(6): 1077-1081. (in Chinese
ZHOU Min, WANG Rugen, ZENG Lingjun, et al. Effect of slot width on the aerodynamic performance of compressor cascade[J]. Journal of Aerospace Power, 2008, 23(6): 1077-1081. (in Chinese)
|
| [28] |
迟志东,楚武利,张耀峰,等. 缝式机匣处理对跨声速轴流压气机叶尖流场结构的非定常影响[J]. 西安交通大学学报,2021,55(11): 25-33. CHI Zhidong,CHU Wuli,ZHANG Yaofeng,et al. Unsteady effect of slot-type casing treatment on the rotor tip flow structures in a transonic axial flow compressor[J]. Journal of Xi’an Jiaotong University,2021,55(11): 25-33. (in Chinese
CHI Zhidong, CHU Wuli, ZHANG Yaofeng, et al. Unsteady effect of slot-type casing treatment on the rotor tip flow structures in a transonic axial flow compressor[J]. Journal of Xi’an Jiaotong University, 2021, 55(11): 25-33. (in Chinese)
|
| [29] |
王广,楚武利,张皓光,等. 端壁合成射流激励参数变化对跨声速轴流压气机性能的影响[J]. 西安交通大学学报,2021,55(5): 193-202. WANG Guang,CHU Wuli,ZHANG Haoguang,et al. Effects of the endwall synthetic jet excitation parameters on performance of transonic axial flow compressor[J]. Journal of Xi’an Jiaotong University,2021,55(5): 193-202. (in Chinese
WANG Guang, CHU Wuli, ZHANG Haoguang, et al. Effects of the endwall synthetic jet excitation parameters on performance of transonic axial flow compressor[J]. Journal of Xi’an Jiaotong University, 2021, 55(5): 193-202. (in Chinese)
|
| [30] |
YAN Song,CHU Wuli. Investigation on the influence of the structure parameters of blade tip recess on the performance of axial flow compressor[J]. Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering,2021,235(16): 2436-2450. doi: 10.1177/0954410021998101
|
| [31] |
张国臣,张成烽,曹志远,等. 叶片开缝和边界层抽吸耦合控制压气机失速裕度的数值研究[J]. 推进技术,2023,44(1): 210689. ZHANG Guochen,ZHANG Chengfeng,CAO Zhiyuan,et al. Numerical study on coupling of blade slotting and boundary layer suction to control compressor stall margin[J]. Journal of Propulsion Technology,2023,44(1): 210689. (in Chinese
ZHANG Guochen, ZHANG Chengfeng, CAO Zhiyuan, et al. Numerical study on coupling of blade slotting and boundary layer suction to control compressor stall margin[J]. Journal of Propulsion Technology, 2023, 44(1): 210689. (in Chinese)
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