ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (12): 127734-127734.doi: 10.7527/S1000-6893.2022.27734
• Fluid Mechanics and Flight Mechanics • Previous Articles
Yinxin ZHU, Wenqiang PENG, Zhenbing LUO(), Ying KANG, Zhijie ZHAO, Pan CHENG, Jiefu LIU
Received:
2022-06-30
Revised:
2022-07-27
Accepted:
2022-09-23
Online:
2022-10-08
Published:
2022-09-30
Contact:
Zhenbing LUO
E-mail:luozhenbing@163.com
Supported by:
CLC Number:
Yinxin ZHU, Wenqiang PENG, Zhenbing LUO, Ying KANG, Zhijie ZHAO, Pan CHENG, Jiefu LIU. Influence of full⁃span dual synthetic jets on high⁃turning compressor cascade[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 127734-127734.
1 | 郑新前, 王钧莹, 黄维娜, 等. 航空发动机不确定性设计体系探讨[J]. 航空学报, 2023, 44(7): 027099. |
ZHENG X Q, WANG J Y, HUANG W N, et al. Uncertainty-based design system for aeroengines[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(7): 027099. | |
2 | 曹传军, 刘天一, 朱伟, 等. 民用大涵道比涡扇发动机高压压气机技术进展[J]. 航空学报, 2023, 44(12): 027824. |
CAO C J, LIU T Y, ZHU W, et al. Technology development in high pressure compressor of civil high bypass-ratio turbofan engine[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(12): 027824 (in Chinese). | |
3 | 索德军, 孙明霞, 梁春华, 等. 美国战斗机发动机技术研究与产品研制的发展特点及趋势分析[J]. 航空发动机, 2016, 42(6): 82-89. |
SUO D J, SUN M X, LIANG C H, et al. Review on technical investigation and product development of fighter engine in US[J]. Aeroengine, 2016, 42(6): 82-89 (in Chinese). | |
4 | HECKLAU M, GMELIN C, NITSCHE W, et al. Experimental and numerical results of active flow control on a highly loaded stator cascade[J]. Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2011, 225(7): 907-918. |
5 | 李仁康, 王如根, 何成, 等. 涡流发生器对高负荷压气机叶栅角区分离影响的实验研究[J]. 实验流体力学, 2017, 31(6): 22-28. |
LI R K, WANG R G, HE C, et al. Experimental investigation on the effects of vortex generator on corner separation in a high-load compressor cascade[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(6): 22-28 (in Chinese). | |
6 | 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 H J, LIU B, ZHANG B T. Slot position and structure of large camber slotted cascades[J]. Journal of Propulsion Technology, 2021, 42(12): 2675-2683 (in Chinese). | |
7 | CAO Z Y, SONG C, LIU B, et al. Influence of endwall slotted injection on performance and flow physics in a compressor cascade[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2021, 235(3): 319-334. |
8 | 刘华坪, 陈焕龙, 李德雄, 等. 射流旋涡发生器控制大折转角扩压叶栅二次流[J]. 航空动力学报, 2015, 30(4): 838-845. |
LIU H P, CHEN H L, LI D X, et al. Secondary flow control in high-turning compressor cascade using vortex generator jet[J]. Journal of Aerospace Power, 2015, 30(4): 838-845 (in Chinese). | |
9 | 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): 143-152. |
GAO L M, GUO Y C, LI R Y, et al. Flow separation of compressor cascade controlled by boundary layer suction at high subsonic velocity[J]. Journal of Propulsion Technology, 2022, 43(4): 143-152 (in Chinese). | |
10 | 安鑫, 孙小磊, 崔伟伟, 等. 端壁抽吸对跨声速转子流动特性影响研究[J]. 推进技术, 2016, 37(9): 1664-1672. |
AN X, SUN X L, CUI W W, et al. Investigation on effects of end wall boundary layer suction on transonic rotor flow characteristics[J]. Journal of Propulsion Technology, 2016, 37(9): 1664-1672 (in Chinese). | |
11 | 张海灯, 李应红, 吴云, 等. 高速压气机叶栅纳秒脉冲等离子体流动控制仿真研究[J]. 航空学报, 2014, 35(6): 1560-1570. |
ZHANG H D, LI Y H, WU Y, et al. Simulation research of nanosecond pulsed plasma actuation flow control on high speed compressor cascade[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6): 1560-1570 (in Chinese). | |
12 | 周岩, 罗振兵, 王林, 等. 等离子体合成射流激励器及其流动控制技术研究进展[J]. 航空学报, 2022, 43(3): 98-140. |
ZHOU Y, LUO Z B, WANG L, et al. Plasma synthetic jet actuator for flow control: Review[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(3): 98-140 (in Chinese). | |
13 | 孙志坤, 史志伟, 张伟麟, 等. 等离子体激励器对高速翼型升阻特性的影响[J]. 航空学报, 2022, 43(S2): 23-39. |
SUN Z K, SHI Z W, ZHANG W L, et al. Effect of plasma actuator on lift-drag characteristics of high-speed airfoil[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 23-39 (in Chinese). | |
14 | 张攀峰, 王晋军, 冯立好. 零质量射流技术及其应用研究进展[J]. 中国科学(E辑: 技术科学), 2008, 38(3): 321-349. |
ZHANG P F, WANG J J, FENG L H. Research progress of zero mass jet technology and its application[J]. Science in China (Series E: Technological Sciences), 2008, 38(3): 321-349 (in Chinese). | |
15 | 冯立好, 魏凌云, 董磊, 等. 飞翼布局飞机耦合运动失稳的主动流动控制[J]. 航空学报, 2022, 43(10): 527353. |
FENG L H, WEI L Y, DONG L, et al. Active flow control for coupled motion instability of flying-wing aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 527353 (in Chinese). | |
16 | ZANDER V, HECKLAU M, NITSCHE W, et al. Active flow control by means of synthetic jets on a highly loaded compressor cascade[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2011, 225(7): 897-908. |
17 | GMELIN C, STEGER M, ZANDER V, et al. Numerical investigations of active flow control using synthetic jets on a highly loaded compressor stator cascade[C]∥Proceedings of ASME 2010 3rd Joint US-European Fluids Engineering Summer Meeting Collocated with 8th International Conference on Nanochannels, Microchannels, and Minichannels.New York:ASME,2011: 1071-1080. |
18 | ZHENG X Q, ZHOU S, LU Y J, et al. Flow control of annular compressor cascade by synthetic jets[J]. Journal of Turbomachinery, 2008, 130(2): 021018. |
19 | 秦勇, 宋彦萍, 陈浮, 等. 合成射流控制高速扩压叶栅二次流的数值模拟[J]. 航空动力学报, 2018, 33(4): 792-802. |
QIN Y, SONG Y P, CHEN F, et al. Numerical simulation of secondary flow control on high-speed compressor cascade with synthetic jets[J]. Journal of Aerospace Power, 2018, 33(4): 792-802 (in Chinese). | |
20 | 蔡乐, 周逊, 卢少鹏, 等. 合成射流控制高负荷扩压叶栅分离数值研究[J]. 工程热物理学报, 2013, 34(4): 632-636. |
CAI L, ZHOU X, LU S P, et al. Numerical investigation on effectiveness of flow separation control in high-load compressor cascade by synthetic jet[J]. Journal of Engineering Thermophysics, 2013, 34(4): 632-636 (in Chinese). | |
21 | GIORGI M G, LUCA C G, FICARELLA A, et al. Comparison between synthetic jets and continuous jets for active flow control: Application on a NACA 0015 and a compressor stator cascade[J]. Aerospace Science and Technology, 2015, 43: 256-280. |
22 | BENINI E, BIOLLO R, PONZA R. Efficiency enhancement in transonic compressor rotor blades using synthetic jets: A numerical investigation[J]. Applied Energy, 2011, 88(3): 953-962. |
23 | 刘强, 罗振兵, 邓雄, 等. 基于POD方法的合成双射流流场模态分析[J]. 空气动力学学报, 2020, 38(6): 1027-1033. |
LIU Q, LUO Z B, DENG X, et al. Modal analysis of dual syntehtic jets based on POD method[J]. Acta Aerodynamica Sinica, 2020, 38(6): 1027-1033 (in Chinese). | |
24 | 罗振兵, 夏智勋, 邓雄, 等. 合成双射流及其流动控制技术研究进展[J]. 空气动力学学报, 2017, 35(2): 252-264. |
LUO Z B, XIA Z X, DENG X, et al. Research progress of dual synthetic jets and its flow control technology[J]. Acta Aerodynamica Sinica, 2017, 35(2): 252-264 (in Chinese). | |
25 | 王林, 罗振兵, 夏智勋, 等. 合成双射流控制翼型分离流动的数值研究[J]. 空气动力学学报, 2012, 30(3): 353-357. |
WANG L, LUO Z B, XIA Z X, et al. Numerical simulation of separated flow control on an airfoil using dual synthetic jets[J]. Acta Aerodynamica Sinica, 2012, 30(3): 353-357 (in Chinese). | |
26 | 李玉杰, 罗振兵, 邓雄, 等. 合成双射流控制NACA0015翼型大攻角流动分离试验研究[J]. 航空学报, 2016, 37(3): 817-825. |
LI Y J, LUO Z B, DENG X, et al. Experimental investigation on flow separation control of stalled NACA0015 airfoil using dual synthetic jet actuator[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3): 817-825 (in Chinese). | |
27 | LUO Z B, ZHAO Z J, LIU J F, et al. Novel roll effector based on zero-mass-flux dual synthetic jets and its flight test[J]. Chinese Journal of Aeronautics, 2022, 35(8): 1-6. |
28 | 刘火星, 李凌, 蒋浩康, 等. 二维NACA65叶型前缘几何形状对气动性能的影响[J]. 工程热物理学报, 2003, 24(2): 231-233. |
LIU H X, LI L, JIANG H K, et al. Effect of leading-edge geometry on separation bubble on a NACA65 compressor blade[J]. Journal of Engineering Thermophysics, 2003, 24(2): 231-233 (in Chinese). | |
29 | BOGDONOFF H E. Blade design data for axial-flow fans and compressors: NACA-WR-L-635[R]. Washington, D.C.: NACA, 1945. |
30 | BESELT C, ECK M, PEITSCH D. Three-dimensional flow field in highly loaded compressor cascade[J]. Journal of Turbomachinery, 2014, 136(10): 101007. |
31 | GBADEBO S A, CUMPSTY N A, HYNES T P. Three-dimensional separations in axial compressors[J]. Journal of Turbomachinery, 2005, 127(2): 331-339. |
32 | LEI V M, SPAKOVSZKY Z S, GREITZER E M. A criterion for axial compressor hub-corner stall[J]. Journal of Turbomachinery, 2008, 130(3): 031006. |
33 | NERGER D, SAATHOFF H, RADESPIEL R, et al. Experimental investigation of endwall and suction side blowing in a highly loaded compressor stator cascade[J]. Journal of Turbomachinery, 2012, 134(2): 021010. |
34 | JEONG J, HUSSAIN F. On the identification of a vortex[J]. Journal of Fluid Mechanics, 1995, 285: 69-94. |
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