航空发动机压气机旋转不稳定现象研究进展

doi:10.7527/S1000-6893.2024.29851

Abstract

Abstract:

Rotating instability is a complex flow instability phenomenon in aeroengine compressors， which often increases the tip aeroacoustic noise or induces high amplitude flow-induced vibration problem. With the aerodynamic load increase and damping decrease， the main engine companies home and abroad have encountered the flow-induced vibration problem caused by rotating instability during the development of new engines， and it is predicted that more severe challenges will arise in the future development of high performance aeroengines. This paper first reviews the development history of compressor flow instabilities in the past 80 years. Then， the research progress of rotating instability in the past 30 years home and abroad is summarized， and the research progress of rotating instability phenomenon， numerical simulation methods， experimental testing technologies， generation mechanisms， affecting factors and control methods are discussed， aiming to further the theoretical understanding of the compressor rotating instability. Finally， we propose our views and future prospects on this phenomenon.

Key words: aeroengine compressor, rotating instability phenomenon, unsteady flow, aeroelasticity, flow control

CLC Number:

V231.3

Songbai WANG, Yuyang HAO, Yadong WU, Yong CHEN, Huawei YU, Lin DU. Research progress on rotating instability of aeroengine compressor[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(16): 29851-029851.

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References 120

1	李清华，安利平，徐林，等. 高负荷轴流压气机设计与试验验证［J］. 航空学报， 2017， 38（9）： 520990.
	LI Q H， AN L P， XU L， et al. Design and test verification of high load axial-flow compressor［J］. Acta Aeronautica et Astronautica Sinica， 2017， 38（9）： 520990 （in Chinese）.
2	GARNIER V H， EPSTEIN A H， GREITZER E M. Rotating waves as a stall inception indication in axial compressors［J］. Journal of Turbomachinery， 1991， 113（2）： 290-301.
3	STENNING A H， KRIEBEL A R. Stall propagation in a cascade of airfoils［J］. Journal of Fluids Engineering， 1958， 80（4）： 777-789.
4	BULLOCK R O， FINGER H B. Compressor surge investigated by NACA［J］. SAE Journal， 1951， 59：42-45.
5	EMMONS H W， PEARSON C E， GRANT H P. Compressor surge and stall propagation［J］. Journal of Fluids Engineering， 1955， 77（4）： 455-467.
6	DAY I J. Stall， surge， and 75 years of research［J］. Journal of Turbomachinery， 2016， 138（1）： 011001.
7	GREITZER E M. Surge and rotating stall in axial flow compressors—Part I： Theoretical compression system model［J］. Journal of Engineering for Gas Turbine and Power， 1976， 98（2）： 190-198.
8	GREITZER E M. Surge and rotating stall in axial flow compressor—Part Ⅱ： Experimental results and comparison with Theory［J］. Journal of Engineering for Gas Turbine and Power， 1976， 98（2）： 199-211.
9	MOORE F K， GREITZER E M. A theory of post-stall transients in axial compression systems： Part I—Development of equations［J］. Journal of Engineering for Gas Turbines and Power， 1986， 108（1）： 68-76.
10	GREITZER E M， MOORE F K. A theory of post-stall transients in axial compression systems： Part Ⅱ—Application［J］. Journal of Engineering for Gas Turbines and Power， 1986， 108（2）：231-239.
11	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）.
12	DAY I J. Stall inception in axial flow compressors［J］. Journal of Turbomachinery， 1993， 115（1）： 1-9.
13	DAY I J. Active suppression of rotating stall and surge in axial compressors［J］. Journal of Turbomachinery， 1993， 115（1）： 40-47.
14	王昊，王牌，向宏辉，等. 压气机叶顶流动不稳定性试验和数值研究［J］. 航空动力学报， 2023， 38（3）： 674-684.
	WANG H， WANG P， XIANG H H， et al. Experiment and numerical investigation on tip flow instabilities of compressors［J］. Journal of Aerospace Power， 2023， 38（3）： 674-684 （in Chinese）.
15	王昊，屠宝锋. 叶尖泄漏流对压气机稳定性影响的数值分析［J］. 航空动力学报， 2021， 36（2）： 320-328.
	WANG H， TU B F. Numerical analysis of tip leakage flow effect on compressor stability［J］. Journal of Aerospace Power， 2021， 36（2）： 320-328 （in Chinese）.
16	JIN H J， ZHAO Y P， WANG Z Q. A rotating stall warning method for aero-engine compressor based on DeepESVDD-CNN［J］. Aerospace Science and Technology， 2023， 139： 108411.
17	赵红亮，张文强，邱佳慧，等. 总温畸变下跨声压气机失速过程非定常模拟［J］. 航空学报， 2023， 44（14）： 628319.
	ZHAO H L， ZHANG W Q， QIU J H， et al. Unsteady simulation of stall process in transonic compressor with total temperature distortion［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（14）： 628319 （in Chinese）.
18	许登科，董旭，徐瑞泽，等. 压气机流动稳定性自适应控制方法研究进展［J］. 力学学报， 2022， 54（3）： 559-576.
	XU D K， DONG X， XU R Z， et al. Research progress of adaptive control methods for compressor flow stability［J］. Chinese Journal of Theoretical and Applied Mechanics， 2022， 54（3）： 559-576 （in Chinese）.
19	SUN D K， NIE C Q， LIU X H， et al. Further investigation on transonic compressor stall margin enhancement with stall precursor-suppressed casing treatment［J］. Journal of Turbomachinery， 2016， 138（2）： 021001.
20	SUN DK， LI J， DONG X， et al. Foammetal casing treatment on an axial flow compressor： Stability improvement and noise reduction［J］. Journal of Turbomachinery， 2022， 144（1）： 011003.
21	MATHIOUDAKIS K， BREUGELMANS F A E. Development of small rotating stall in a single stage axial compressor［C］∥Proceedings of ASME 1985 International Gas Turbine Conference and Exhibit. New York： ASME， 1985.
22	BAUMGARTNER M， KAMEIER F， HOURMOUZIADIS J. Non-engine order blade vibration in a high pressure compressor［C］∥Proceeding of 12th International Symposium on Airbreathing Engines， 1995.
23	MAILACH R， LEHMANN I， VOGELER K. Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex［J］. Journal of Turbomachinery， 2001， 123（3）： 453-460.
24	PARDOWITZ B， TAPKEN U， ENGHARDT L. Time-resolved rotating instability waves in an annular cascade［C］∥18th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2012.
25	GAO F L， YANG M S， ZHANG Z B， et al. Experiment and theoretical analysis of a type of non-synchronous vibration in a high pressure compressor［C］∥32nd Congress of the International Council of the Aeronautical Sciences， 2021.
26	STAPELFELDT S， BRANDSTETTER C. Non-synchronous vibration in axial compressors： Lock-in mechanism and semi-analytical model［J］. Journal of Sound and Vibration， 2020， 488： 115649.
27	JUNGST M， HOLZINGER F， SCHIFFER H P， et al. Analysing non-synchronous blade vibration in a transonic compressor rotor［C］∥11th European Conference on Turbomachinery Fluid Dynamic & Thermodynamics， 2015.
28	MÄRZ J， HAH C， NEISE W. An experimental and numerical investigation into the mechanisms of rotating instability［J］. Journal of Turbomachinery， 2002， 124（3）： 367-374.
29	BESELT C， RENNINGS R， THIELE F， et al. Experimental and numerical investigations of rotating instability phenomenon in an axial compressor stator［C］∥Proceedings of the 42nd AIAA Fluid Dynamics Conference and Exhibit. Reston： AIAA， 2012.
30	KIELB R E， BARTER J W， THOMAS J P， et al. Blade excitation by aerodynamic instabilities： A compressor blade study［C］∥Proceedings of ASME Turbo Expo 2003， Collocated with the 2003 International Joint Power Generation Conference. New York： ASME， 2003.
31	HELLMICH B， SEUME J R. Causes of acoustic resonance in a high-speed axial compressor［J］. Journal of Turbomachinery， 2008， 130（3）： 031003.
32	ZHAO F T， JING X D， YANG M S， et al. Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance［J］. Chinese Journal of Aeronautics， 2020， 33（3）： 870-878.
33	赵奉同，景晓东，沙云东，等. 压气机内部噪声特征与转子叶片声固耦合机理分析［J］. 航空学报， 2019， 40（5）： 122669.
	ZHAO F T， JING X D， SHA Y D， et al. Analysis of noise characteristics and acoustic structure coupling mechanism of rotor blades in compressor［J］. Acta Aeronautica et Astronautica Sinica， 2019， 40（5）： 122669 （in Chinese）.
34	汪松柏，张少平，余华蔚，等. 高负荷压气机旋转不稳定诱发转子叶片非同步振动的实验研究［J］. 推进技术， 2023， 44（2）： 22010036.
	WANG S B， ZHANG S P， YU H W， et al. Experimental research on rotor blade non-synchronous vibrations induced by rotating instability of high load compressor［J］. Journal of Propulsion Technology， 2023， 44（2）： 22010036 （in Chinese）.
35	WANG W L， YANG C， HU C X， et al. Investigation of tip leakage flow unsteadiness and rotating instability in a centrifugal compressor impeller［J］. Proceedings of the Institution of Mechanical Engineers， Part D： Journal of Automobile Engineering， 2022， 236（4）： 621-638.
36	GRONDIN J， TRÉBINJAC I， ROCHUON N. Rotating instabilities versus rotating stall in a high-speed centrifugal compressor［C］∥Proceedings of ASME Turbo Expo 2018： Turbomachinery Technical Conference and Exposition. New York： ASME， 2018.
37	INOUE M， KUROUMARU M， YOSHIDA S， et al. Effect of tip clearance on stall evolution process in a low-speed axial compressor stage［C］∥Proceedings of ASME Turbo Expo 2004： Power for Land， Sea， and Air. New York： ASME， 2008.
38	RAITOR T， NEISE W. Sound generation in centrifugal compressors［J］. Journal of Sound Vibration， 2008， 314（3-5）： 738-756.
39	KAMEIER F， NEISE W. Experimental study of tip clearance losses and noise in axial turbomachines and their reduction［J］. Journal of Turbomachinery， 1997， 119（3）： 460-471.
40	MÖLLER D， SCHIFFER H P. On the mechanism of spike stall inception and near stall non-synchronous vibration in an axial compressor［C］∥Proceedings of ASME Turbo Expo 2020： Turbomachinery Technical Conference and Exposition. New York： ASME， 2020.
41	洪志亮，赵国昌，杨明绥，等. 航空发动机压气机内部流体诱发声共振研究进展［J］. 航空学报， 2019， 40（11）： 023139.
	HONG Z L， ZHAO G C， YANG M S， et al. Development of flow-induced acoustic resonance in aeroengine compressors［J］. Acta Aeronautica et Astronautica Sinica， 2019， 40（11）： 023139 （in Chinese）.
42	王昊，吴亚东，欧阳华. 低速轴流压气机旋转不稳定性数值研究［J］. 工程热物理学报， 2019， 40（3）： 551-558.
	WANG H， WU Y D， OUYANG H. Numerical investigations of rotating instability in a low speed axial compressor［J］. Journal of Engineering Thermophysics， 2019， 40（3）： 551-558 （in Chinese）.
43	王昊，吴亚东，欧阳华. 压气机叶顶泄漏流振荡周向传播特性的数值模拟［J］. 航空动力学报， 2017， 32（3）： 538-548.
	WANG H， WU Y D， OUYANG H. Numerical simulations on circumferential propagating characteristics of tip leakage flow oscillation in compressor［J］. Journal of Aerospace Power， 2017， 32（3）： 538-548 （in Chinese）.
44	王昊，吴亚东，欧阳华. 低速轴流压气机中气动旋转不稳定性和叶顶泄漏流脉动特性［J］. 航空动力学报， 2016， 31（9）： 2239-2250.
	WANG H， WU Y D， OUYANG H. Aerodynamic rotating instability and fluctuated characteristics of tip clearance flow in low speed axial flow compressor［J］. Journal of Aerospace Power， 2016， 31（9）： 2239-2250 （in Chinese）.
45	NISHIOKA T， KANNO T， HIRADATE K. Rotor-tip flow fields near inception point of rotating instability in an axial-flow fan［C］∥ASME 2011 Turbo Expo： Turbine Technical Conference and Exposition. New York： ASME， 2011.
46	VO H D. Role of tip clearance flow in rotating instabilities and nonsynchronous vibrations［J］. Journal of Propulsion and Power， 2010， 26（3）： 556-561.
47	DU J， LI J C， WANG K， et al. The self-induced unsteadiness of tip leakage flow in an axial low-speed compressor with single circumferential casing groove［J］. Journal of Thermal Science， 2013， 22（6）： 565-572.
48	王年华，常兴华，赵钟，等. 非结构CFD软件MPI+OpenMP混合并行及超大规模非定常并行计算的应用［J］. 航空学报， 2020， 41（10）： 123859.
	WANG N H， CHANG X H， ZHAO Z， et al. Implementation of hybrid MPI+OpenMP parallelization on unstructured CFD solver and its applications in massive unsteady simulations［J］. Acta Aeronautica et Astronautica Sinica， 2020， 41（10）： 123859 （in Chinese）.
49	PATEL P， YANG Y C， ZHA G C. Improved delayed detached eddy simulation （IDDES） of a 1.5 stage axial compressor non-synchronous vibration［C］∥Proceedings of ASME Turbo Expo 2020： Turbomachinery Technical Conference and Exposition. New York： ASME， 2020.
50	HAH C， HATHAWAY M， KATZ J， et al. Investigation of unsteady tip clearance flow in a low-speed one and half stage axial compressor with LES and PIV［C］∥Proceedings of ASME/JSME/KSME 2015 Joint Fluids Engineering Conference. New York： ASME， 2015.
51	HAH C. Effects of double-leakage tip clearance flow on the performance of a compressor stage with a large rotor tip gap［J］. Journal of Turbomachinery， 2017， 139（6）： 061006.
52	CHEN X Y， KOPPE B， LANGE M， et al. Comparison of turbulence modeling for a compressor rotor at different tip clearances［J］. AIAA Journal， 2022， 60（2）： 1186-1198.
53	CHEN X Y， KOPPE B， LANGE M， et al. Performance of unsteady Reynolds-averaged Navier-Stokes and hybrid scale-resolving simulation approaches in simulating a low-speed axial compressor rotor［C］∥Proceedings of ASME Turbo Expo 2021： Turbomachinery Technical Conference and Exposition. New York： ASME， 2021.
54	IM H S， ZHA G C. Simulation of non-synchronous blade vibration of an axial compressor using a fully coupled fluid/structure interaction［C］∥Proceedings of ASME Turbo Expo 2012： Turbine Technical Conference and Exposition. New York： ASME， 2012.
55	GAN J Y， IM H S， ESPINAL D， et al. Investigation of a compressor rotor non-synchronous vibration with and without fluid-structure interaction［C］∥Proceedings of ASME Turbo Expo 2014： Turbine Technical Conference and Exposition. New York： ASME， 2014.
56	GAN J Y， IM H S， ZHA G C. Numerical examination of lock-In hypothesis of non-synchronous vibration in an axial compressor［C］∥Proceedings of ASME Turbo Expo 2017： Turbomachinery Technical Conference and Exposition. New York： ASME， 2017.
57	HAN L， WEI D S， WANG Y R， et al. Lock-in phenomenon of tip clearance flow and its influence on aerodynamic damping under specified vibration on an axial transonic compressor rotor［J］. Chinese Journal of Aeronautics， 2022， 35（3）： 185-200.
58	HAN L， WEI D S， WANG Y R， et al. Locked-In phenomenon between tip clearance flow instabilities and enforced blade motion in axial transonic compressor rotors［C］∥Proceedings of ASME Turbo Expo 2020： Turbomachinery Technical Conference and Exposition. New York： ASME， 2020.
59	HAN L， WEI D S， WANG Y R. Onset of tip clearance flow instabilities causing nonsynchronous vibration in an axial compressor［C］∥16th International Symposium on Unsteady Aerodynamics Aeroacoustics and Aeroelasticity of Turbomachines， 2022.
60	ZHENG Y， GAO Q Z， YANG H. Non-synchronous blade vibration analysis of a transonic fan［J］. Chinese Journal of Aeronautics， 2023， 36（1）： 178-190.
61	SCHUSTER B. Axial fan tone noise induced by separated tip flow， flutter， and forced response［C］∥Proceedings of the 11th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2005.
62	BRANDSTETTER C， PAOLETTI B， OTTAVY X. Acoustic and convective mechanism contributing to non-synchronous vibrations in a multistage compressor［C］∥ASME Turbo Expo 2019： Turbomachinery Technical Conference and Exposition. New York： ASME， 2019.
63	HOLZINGER F， WARTZEK F， SCHIFFER H P， et al. Self-excited blade vibration experimentally investigated in transonic compressors： Acoustic resonance［J］. Journal of Turbomachinery， 2016， 138（4）： 041001.
64	MÖLLER D， JÜNGST M， HOLZINGER F， et al. Mechanism of nonsynchronous blade vibration in a transonic compressor rig［J］. Journal of Turbomachinery， 2017， 139（1）： 011002.
65	汪松柏，陈勇，吴亚东，等. 轴流压气机转子叶片非同步振动研究进展［J］. 航空学报， 2023， 44（17）： 028044.
	WANG S B， CHEN Y， WU Y D， et al. Research progress on non-synchronous vibration of axial compressor rotor blade［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（17）： 028044 （in Chinese）.
66	HOLZINGER F， WARTZEK F， JÜNGST M， et al. Self-excited blade vibration experimentally investigated in transonic compressors： Rotating instabilities and flutter［J］. Journal of Turbomachinery， 2016， 138（4）： 041006.
67	MA H W， WANG Z Z， HE X， et al. Investigation of tip leakage flow in spatial and temporal scales of axial isolated compressor rotor near stall［J］. Journal of the Brazilian Society of Mechanical Sciences and Engineering， 2023， 45（7）： 384.
68	陈雷，乔百杰，敖春燕，等. 基于叶端定时的转子叶片动应变重构不确定性量化［J］. 航空动力学报， 2022， 37（7）： 1456-1468.
	CHEN L， QIAO B J， AO C Y， et al. Uncertainty quantification of rotor blade dynamic strain reconstruction based on blade tip timing［J］. Journal of Aerospace Power， 2022， 37（7）： 1456-1468 （in Chinese）.
69	刘美茹，朱靖，梁恩波，等. 基于叶尖定时的航空发动机压气机叶片振动测量［J］. 航空动力学报， 2019， 34（9）： 1895-1904.
	LIU M R， ZHU J， LIANG E B， et al. Vibration measurement on compressor rotor blades of aero-engine based on tip-timing［J］. Journal of Aerospace Power， 2019， 34（9）： 1895-1904 （in Chinese）.
70	REN S Q， XIANG X R， ZHAO W， et al. An error correction blade tip-timing method to improve the measured accuracy of blade vibration displacement during unstable rotation speed［J］. Mechanical Systems and Signal Processing， 2022， 162： 108030.
71	FAN C W， WU Y D， RUSSHARD P， et al. A blade tip-timing method without once-per-revolution sensor for blade vibration measurement in gas turbine engines［J］. Transactions of the Canadian Society for Mechanical Engineering， 2021， 45（3）： 396-410.
72	FAN C W， WU Y D， RUSSHARD P， et al. An improved blade tip-timing method for vibration measurement of rotating blades during transient operating conditions［J］. Journal of Vibration Engineering & Technologies， 2020， 8（6）： 859-868.
73	DONOHO D L. Compressed sensing［J］. IEEE Transactions on Information Theory， 2006， 52（4）： 1289-1306.
74	许敬晖，乔百杰，刘美茹，等. 基于叶端定时的转子叶片裂纹监测与诊断［J］. 推进技术， 2022， 43（2）： 210537.
	XU J H， QIAO B J， LIU M R， et al. Crack monitoring and diagnosis of rotor blades using blade tip timing［J］. Journal of Propulsion Technology， 2022， 43（2）： 210537 （in Chinese）.
75	FIQUET A L， AUBERT S， BRANDSTETTER C， et al. Acoustic resonance in an axial multistage compressor leading to non-synchronous blade vibration［J］. Journal of Turbomachinery， 2021， 143（9）： 091014.
76	CAMP T R. A study of acoustic resonance in a low-speed multistage compressor［J］. Journal of Turbomachinery， 1999， 121（1）： 36-43.
77	文璧，乔百杰，李泽芃，等. 基于声模态分解的风扇叶盘同步振动辨识［J］. 航空学报， 2023， 44（6）： 227066.
	WEN B， QIAO B J， LI Z P， et al. Synchronous vibration identification of fan blisk based on acoustic mode decomposition［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（6）： 227066 （in Chinese）.
78	李泽芃，乔百杰，文璧，等. 基于声阵列信号的风扇喘振先兆特征识别［J］. 航空动力学报， 2021， 36（5）： 923-934.
	LI Z P， QIAO B J， WEN B， et al. Identification of fan surge precursors based on acoustic array signals［J］. Journal of Aerospace Power， 2021， 36（5）： 923-934 （in Chinese）.
79	YANG Z Y， WU Y D， OUYANG H. Investigation on mode characteristics of rotating instability and rotating stall in an axial compressor［J］. Journal of Turbomachinery， 2022， 144（6）： 061010.
80	YANG Z Y， MING L L， WU S， et al. On the mode characteristics of rotating instability with different tip clearances［C］∥Proceedings of ASME Turbo Expo 2022： Turbomachinery Technical Conference and Exposition. New York： ASME， 2022.
81	TIAN J， YAO D， WU Y D， et al. Experimental study on rotating instability mode characteristics of axial compressor tip flow［J］. Experiments in Fluids， 2018， 59（4）： 63.
82	BIELA C， MÜLLER M W， SCHIFFER H P， et al. Unsteady pressure measurement in a single stage axial transonic compressor near the stability limit［C］∥Proceedings of ASME Turbo Expo 2008： Power for Land， Sea， and Air. New York： ASME， 2008.
83	付磊，袁巍，宋西镇，等. 跨声速压气机转子叶尖流场旋转不稳定现象的数值研究［J］. 航空动力学报， 2014， 29（5）： 1145-1153.
	FU L， YUAN W， SONG X Z， et al. Numerical investigation on rotating instability phenomenon in tip flow field of transonic compressor rotor［J］. Journal of Aerospace Power， 2014， 29（5）： 1145-1153 （in Chinese）.
84	陈智洋，吴艳辉，安光耀，等. 轴流压气机转子旋转不稳定性检测及机理探讨［J］. 推进技术， 2017， 38（11）： 2401-2410.
	CHEN Z Y， WU Y H， AN G Y， et al. Experimental detection of rotating instability and exploration of its flow mechanism in an axial flow compressor rotor［J］. Journal of Propulsion Technology， 2017， 38（11）： 2401-2410 （in Chinese）.
85	WANG H， WU Y D， WANG Y G， et al. Evolution of the flow instabilities in an axial compressor rotor with large tip clearance： An experimental and URANS study［J］. Aerospace Science and Technology， 2020， 96： 105557.
86	PARDOWITZ B， MOREAU A， TAPKEN U， et al. Experimental identification of rotating instability of an axial fan with shrouded rotor［J］. Proceedings of the Institution of Mechanical Engineers， Part A： Journal of Power and Energy， 2015， 229（5）： 520-528.
87	ZHANG M， LI J， DONG X， et al. Experimental study on different tip clearance of low-speed axial fan［C］∥ASME Turbo Expo 2021： Turbomachinery Technical Conference and Exposition. New York： ASME， 2021.
88	YAMADA K， KIKUTA H， FURUKAWA M， et al. Effects of tip clearance on the stall inception process in an axial compressor rotor［C］∥Proceedings of ASME Turbo Expo 2013： Turbine Technical Conference and Exposition. New York： ASME， 2013.
89	SEKI R， AZUMA T， IWATANI J， et al. Investigation of tip leakage vortex breakdown in a high-speed multistage axial compressor［J］. Journal of Turbomachinery， 2023， 145（7）： 071017.
90	ESPINAL D， IM H S， ZHA G C. Full-annulus simulation of nonsynchronous blade vibration excitation of an axial compressor［J］. Journal of Turbomachinery， 2018， 140（3）： 031008.
91	IM H S， ZHA G C. Effects of rotor tip clearance on tip clearance flow potentially leading to NSV in an axial compressor［C］∥Proceedings of ASME Turbo Expo 2012： Turbine Technical Conference and Exposition. New York： ASME， 2012.
92	WU Y， LI Q， CHU W， et al. Numerical investigation of the unsteady behaviour of tip clearance flow and its possible link to stall inception［J］. Proceedings of the Institution of Mechanical Engineers， Part A： Journal of Power and Energy， 2010， 224（1）： 85-96.
93	ECK M， GEIST S， PEITSCH D. Physics of prestall propagating disturbances in axial compressors and their potential as a stall warning indicator［J］. Applied Sciences， 2017， 7（3）： 285.
94	ZHANG K， PARK W G. The investigation of rotating instability under distortion based on a compressor rotor［J］. International Journal of Aeronautical and Space Sciences， 2022， 23（3）： 471-483.
95	LI T， WU Y D， TIAN J， et al. Modal analysis of axial compressor tip rotating instability under varying operating conditions［J］. Journal of Thermal Science， 2023， 32（4）： 1345-1356.
96	赖生智，吴亚东，田杰，等. 不同叶顶间隙下压气机旋转不稳定性特性［J］. 上海交通大学学报， 2020， 54（3）： 265-276.
	LAI S Z， WU Y D， TIAN J， et al. Rotating instability characteristics in compressor with different tip clearances［J］. Journal of Shanghai Jiao Tong University， 2020， 54（3）： 265-276 （in Chinese）.
97	WU Y D， LI T， LAI S， et al. Investigation of rotating instability characteristics in an axial compressor with different tip clearances［J］. Proceedings of the Institution of Mechanical Engineers， Part G： Journal of Aerospace Engineering， 2021， 235（15）： 2225-2239.
98	ZHANG B T， LIU B， MAO X C， et al. Combined control of variant clearance and casing aspiration on tip flow field and instability of a transonic compressor［J］. Aerospace Science and Technology， 2022， 127： 107702.
99	陈颖秀，侯安平，张明明，等. 轴流压气机机匣变形对多排转子流场特性的影响［J］. 航空学报， 2016， 37（11）： 3284-3295.
	CHEN Y X， HOU A P， ZHANG M M， et al. Effects of casing deformation on blade rows flow field characteristics in an axialflow compressor［J］. Acta Aeronautica et Astronautica Sinica， 2016， 37（11）： 3284-3295 （in Chinese）.
100	IM H， ZHA G C. Investigation of flow instability mechanism causing compressor rotor-blade nonsynchronous vibration［J］. AIAA Journal， 2014， 52（9）： 2019-2031.
101	姜超，王志宽，乐贵高，等. 周向非均匀叶尖间隙对某转子旋转不稳定现象影响的数值模拟［J/OL］. 航空动力学报，（2023-07-17）［2024-01-03］. .
	JIANG C， WANG Z K， LE G G， et al. Numerical simulation of the effect of circumferential non-uniform tip clearance on rotating instability in a rotor［J/OL］. Journal of Aerospace Power，（2023-07-17）［2024-01-03］. （in Chinese）.
102	WANG Z Q， LU B， LIU J X， et al. Numerical simulation of unsteady tip clearance flow in a transonic compressor rotor［J］. Aerospace Science and Technology， 2018， 72： 193-203.
103	程荣辉，余华蔚，汪松柏，等. 多级压气机转子负荷系数对叶片非同步振动的影响［J］. 航空学报， 2023， 44（14）： 628722.
	CHENG R H， YU H W， WANG S B， et al. Effect of aerodynamic loading coefficient on occurrence of nonsynchronous vibration in a multi-stage compressor［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（14）： 628722 （in Chinese）.
104	XU R， HU J， WANG X G， et al. Experimental investigation of rotating instability in an axial compressor with a steady swirl distortion inlet［J］. Energies， 2021， 14（23）： 8057.
105	杨加寿，冀国锋. 高空低雷诺数风扇/增压级气动设计［J］. 推进技术， 2020， 41（10）： 2190-2196.
	YANG J S， JI G F. Aerodynamic design of fan-booster under condition of high altitude and low Reynolds number［J］. Journal of Propulsion Technology， 2020， 41（10）： 2190-2196 （in Chinese）.
106	赵胜丰，卢新根，朱俊强. 雷诺数对跨声速压气机转子内部流动失稳触发机理的影响［J］. 推进技术， 2013， 34（1）： 25-30.
	ZHAO S F， LU X G， ZHU J Q. Effects of Reynolds number on the instability inception mechanism of a transonic compressor［J］. Journal of Propulsion Technology， 2013， 34（1）： 25-30 （in Chinese）.
107	CHEN Z Y， WU Y H， ZHANG Y W， et al. Circumferential propagation characteristic of unsteady flow in a subsonic axial flow compressor rotor at different Reynolds numbers［C］∥Proceedings of ASME Turbo Expo 2019： Turbomachinery Technical Conference and Exposition. New York： ASME， 2019.
108	陈智洋，吴艳辉，安近怀远，等. 雷诺数对轴流压气机转子非定常流动的影响［J］. 航空动力学报， 2019， 34（12）： 2706-2718.
	CHEN Z Y， WU Y H， AN J H Y， et al. Impact of Reynolds number on unsteady flow in axial flow compressor rotor［J］. Journal of Aerospace Power， 2019， 34（12）： 2706-2718 （in Chinese）.
109	CHENG H Z， LU X G， ZHAO S F， et al. Effect of tip clearance variation in the transonic axial compressor of a miniature gas turbine at different Reynolds numbers［J］. Aerospace Science and Technology， 2022， 128： 107793.
110	CHEN X Y， KOPPE B， LANGE M， et al. Influence of casing groove on rotating instabilities in a low-speed axial compressor［J］. Journal of Turbomachinery， 2023， 145（7）： 071015.
111	陈智洋. 轴流压气机旋转不稳定流动控制及流动控制策略研究［D］. 西安：西北工业大学，2021.
	CHEN Z Y. The flow mechanism and flow control strategy of rotating instability in axial flow compressor［D］. Xi’an： Northwestern Polytechnical University， 2021 （in Chinese）.
112	YE S B， ZHAO Q J， ZHOU X Y， et al. The impact of circumferential casing grooves on rotating instability in a transonic axial compressor［J］. Proceedings of the Institution of Mechanical Engineers， Part G： Journal of Aerospace Engineering， 2019， 233（8）： 2868-2893.
113	LI T， WU Y D， OUYANG H. Influence of axial skewed slots on the rotating instability of a low-speed axial compressor［J］. Proceedings of the Institution of Mechanical Engineers， Part G： Journal of Aerospace Engineering， 2021， 235（3）： 385-401.
114	MÖLLER D， JÜNGST M， SCHIFFER H P， et al. Influence of rotor tip blockage on near stall blade vibrations in an axial compressor rig［J］. Journal of Turbomachinery， 2018， 140（2）： 021007.
115	FRANKE D， FORET J， KLAUSMANN F， et al. Aerodynamic and aeroelastic effects of inlet guide vane mistuning in a transonic compressor［C］∥Proceedings of ASME Turbo Expo 2022： Turbomachinery Technical Conference and Exposition. New York： ASME， 2022.
116	黄玉薇，侯安平，吴杰，等. 压气机叶片非同步振动机理及气动布局优化研究［J］. 推进技术， 2023， 44（5）： 2205064.
	HUANG Y W， HOU A P， WU J， et al. Non-synchronous vibration mechanism and aerodynamic layout optimization of compressor blades［J］. Journal of Propulsion Technology， 2023， 44（5）： 2205064 （in Chinese）.
117	NEUHAUS L， NEISE W. Active control to improve the aerodynamic performance and reduce the tip clearance noise of axial turbomachines［C］∥Proceedings of the 11th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2005.
118	CHEN J P， JOHNSON B， HATHAWAY M， et al. Flow characteristics of tip-injection on compressor rotating instability via time-accurate simulation［C］∥Proceedings of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston： AIAA， 2010.
119	张健，杜娟，陈泽，等. 高负荷压气机叶栅流动分离的主动控制方法综述［J］. 工程热物理学报， 2022， 43（5）： 1190-1202.
	ZHANG J， DU J， CHEN Z， et al. Active flow control concepts of secondary flow on a highly loaded compressor cascade［J］. Journal of Engineering Thermophysics， 2022， 43（5）： 1190-1202 （in Chinese）.
120	吴云，李应红. 等离子体流动控制研究进展与展望［J］. 航空学报， 2015， 36（2）： 381-405.
	WU Y， LI Y H. Progress and outlook of plasma flow control［J］. Acta Aeronautica et Astronautica Sinica， 2015， 36（2）： 381-405 （in Chinese）.

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Research progress on rotating instability of aeroengine compressor

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