航空发动机叶片气动弹性动力响应的数值方法研究进展

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doi:10.6052/1000-0992-11-121

1.
北京航空航天大学航空发动机气动热力重点实验室, 北京 100191
2. 北京航空工程技术研究中心, 北京 100076

基金项目:国家自然科学基金重点资助项目(60934001)

详细信息

作者简介:
侯安平,1975年生,湖南常德人.2003年毕业于北航动力学院并获得博士学位.2004～2005年在北航博士后流动站作博士后研究,2005年底留校任教,2006年评为副教授.现任北航高等工程学院副院长、北航理学基础部部长,中国空气动力学会气动弹性专业委员会委员.主要研究方向为叶轮机械气动弹性、叶轮机械非定常流动机理、风扇/压气机气动设计.已经完成或正在进行的工作主要涉及压气机气动弹性、涡轮气热固耦合、压气机进气畸变及高负荷风扇/压气机气动优化设计等工作.

通讯作者:
张章

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出版历程
- 收稿日期:2011-08-29
- 修回日期:2012-05-25
- 刊出日期:2012-09-25

A REVIEW OF NUMERICAL RESEARCH ON AEROELASTIC DYNAMICAL RESPONSE OF AERO-ENGINE BLADES

1.
Chinese National Key Laboratory of Aerodynamics & Thermodynamics on Aero-engine, Beihang University, Beijing 100191, China
2. Beijing Aeronautical Technology Research Center, Beijing 100076, China

Funds:The project was supported by the National Natural Science Foundation of China (60934001).

More Information

Corresponding author:ZHANG Zhang

摘要

摘要:流动诱发振动造成的航空发动机叶片高周疲劳失效问题深受关注.对叶片的气动弹性动力响应研究的数值方法及进展进行了回顾,总结了航空发动机叶片振动响应实验研究和数值模拟研究的典型成果与特点,并对未来研究发展趋势进行展望.指出进一步的机理研究将集中于不稳定流动因素引发叶片强迫振动发作规律的探索以及更贴近流固耦合物理机制的气动弹性数值模拟方法的发展;在工程需求牵引下,建立适用于工程预测的动力响应分析模型,在设计过程中科学评价叶片气动弹性动力响应问题的潜在风险和发展流动控制基础上的气动阻尼减振技术值得进一步关注.
- 叶片/
- 气动弹性/
- 动力响应/
- 数值模拟/
- 流固耦合
Abstract:The high cycle fatigue failure of aero-engine blades occurs frequently.Aeroelastic dynamic response is a major concern in engineer applications.A review of numerical researches on blade aeroelastic dynamic response is presented in the paper,including numerical simulation,test study and possible research trends.The flow-induced vibration mechanism of blade dynamic response and the numerical method about fluid-structure interaction will be the focus in further mechanism study.For engineer applications,it is valuable to develop a prediction model for dynamic response and to evaluate its potential risks with resonance in the design process.And more attention should be paid on the aerodynamic damping technology based on flow control.
- blade/
- aeroelasticity/
- dynamic response/
- numerical simulation/
- fluid-structure interaction

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参考文献 (84)

1 胡运聪.振动叶栅非定常流动数值模拟与叶片颤振分析.[博士论文].西安:西北工业大学,2003.1-2

2 李其汉,王延荣,王建军.航空发动机叶片高循环疲劳失效研究.航空发动机,2003,29(4):16-18

3 陈桂彬,邹丛青,杨超.气动弹性设计基础.北京:北京航空航天大学出版社,2004.3-4

4 周盛.叶轮机气动弹性力学引论.北京:国防工业出版社,1989.5-6

5 Hall K C,Kielb R E,Ekici K,et al.Recent advancements in turbomachinery aeroelastic design analysis.AIAA paper 2005-14,2005

6 洪杰,张大义,马艳红.气流激励下的叶片高周疲劳寿命研究的发展.航空动力学报,2009,24(3):652-661

7 Danforth C E.Designing to avoid fatigue in long life engines.Society of Automotive Engineers Transactions,1967,75(2):248-262

8 Armstrong E K.Recent blade vibration techniques.Journal of Engineering for Power,1967,89(1):437-444

9 James A K,Douglas C R,Sanford F.Aerodynamic effects on blade vibratory stress variations.Journal of Propulsion and Power,1999,15(5):675-680

10 Sanders A J,Fleeter S.Multi-blade row interactions in a transonic axial compressor,Part II:rotor wake forcing function & stator unsteady aerodynamic response.ASMEPaper 2001-GT-0269,2001

11 Durali M,Kerrebrock J L.Stator performance and unsteady loading in transonic compressor stages.ASME Journal of Turbomachinery,1998,120:224-232

12 Mailach R,Vogeler K.Rotor-stator interactions in a fourstage low-speed axial compressor,Part I:Unsteady profile pressures and the effect of clocking.ASME Paper GT-2004-53098,2004

13 Denos R,Arts T,Paniagua G.Investigation of the unsteady rotor aerodynamics in a transonic turbine stage.ASME Journal of Turbo-machinery,2001,123:81-89

14 Buffum D H,Capece V R,King A J,et al.Oscillating cascade aerodynamics at large mean incidence.Journal of Turbomachinery,1998,120(1):122-130

15 杨秉玉,刘启洲.喘振状态下叶片振动响应的试验研究.燃气涡轮试验与研究,2002,15(2):31-35

16 张大义,马艳红,洪杰,等.双向顺序耦合法求解动力响应的试验验证.航空动力学报,2011,26(6):1266-1273

17 杜建建,李舜酩,张袁元,等.平板叶片的相关激励响应试验.实验室研究与探索,2011,30(1):14-17

18 杜少辉,陆山.航空发动机进气畸变诱导叶片振动的研究.航空发动机,2003,29(3):30-34

19 Carta F O.Coupled blade-disk-shroud flutter instabilities in turbojet engine rotors.ASME Journal of Engineering for Power,1967,89:419-427

20 Bendiksen O.Aeroelastic problems in turbo-machines.AIAA paper 1990-1157,1990

21 Lane F.System mode shapes in the flutter of compressor blade rows.Journal of the Aeronautical Sciences,1956,23:54-66

22 Lane F,Friedman M.Theoretical investigation of subsonic oscillatory blade-row aerodynamics.NASA TN-4136,1958

23 Whitehead D S.Force and moment coefficient for vibrating aerofoils in cascade.British Aeronautical Research Council,R&M 3254,1960

24 Smith S N.Discrete frequency sound generation in axial flow turbomachines.British Aeronautical Research Council,R&M 3709,1972

25 Whitehead D S.A finite-element solution of unsteady two-dimensional flow in cascades.International Journal for Numerical Methods in Fluids,1990,10(1):13-34

26 Verdon J M,Caspar J R.Development of an unsteady aerodynamic analysis for finite deflection subsonic cascades.NASA Contractor Report 3455,1981

27 Verdon J M.Linearized unsteady aerodynamics for turbomachinery aeroelastic application.AIAA paper 1990-2355,1990

28 Caspar J R.Unconditionally stable calculation of transonic potential flow through cascades using adaptive mesh for shock capture.ASME Journal of Engineering for Power,1983,105(3):504-513

29 Surampudi S P,Adamczyk J J.Unsteady transonic flow over cascade blades.AIAA Journal,1986,24(2):293-302

30 Sisto F,Wu W,Thangam S,et al.Computational aerodynamics of oscillating cascades with the evolution of stall.AIAA Journal,1989,27(4):462-471

31 张明明,李绍斌,侯安平,等.叶轮机械叶片颤振研究的进展与评述.力学进展,2011,41(1):26-38

32 Toshimitsu K,Namba M,Li P.Double linearization theory for a rotating subsonic annular cascade of oscillating blades.Memoirs of Kyusu University,1990,50(1):161-199

33 Kodama H,Namba M.Unsteady lifting surface theory for a rotating cascade of swept blades.Journal of Turbomachinery,1991,112(3):411-417

34 陈佐一.流体激振.北京:清华大学出版社,1998.82-101

35 Bell D L,He L.Three-dimensional unsteady flow for an oscillating turbine blade and the influence of tip leakage.Journal of Turbomachinery,2000,122(1):93-101

36 Murthy M R,Joshi A M.Free vibration characteristics of multiple load path blades by transfer matrix method.Journal of the American Helicopter Rotor Society,1986,31(5):561-568

37 Bhat M M,Ramamurti V,Sujatha C.Studies of the determination of natural frequency of industrial turbine blades.Journal of Sound and Vibration,1996,196 (5):681-703

38 Choura S,Jayasuriya S,Medick M A.On the modeling and open-loop conteil of a rotating flexible beam.Journal of Dynamic Systems,Measurement,and Control,1991,113(1):26-33

39 Wanger L F,Griffin J H.Forced harmonic response of grouped blade systems:part I-discrete theory.Journal of Engineering for Gas Turbines and Power,1996,118(1):130-136

40 Shipman W C,Palazotto A N.The consideration of high cycle fatigue in a turbine blade.AIAA paper 2002-1537,2002

41 Lin S M.Pretwisted nonuniform beams with time dependent elastic boundary conditions.AIAA Journal,1998,36(1):1516-1523

42 Bendiksen O O,Friedman P P.Coupled bending-torsion flutter in a supersonic cascade.AIAA Journal,1981,19(1):774-781

43 Stuart M,Li H.Blade forced response prediction for industrial gas turbines part 1:methodologies.ASME paper 2003:407-414,2003

44 Adamczyk J J,Goldstein M E.Unsteady flow in a supersonic cascade with subsonic leading-edge locus.AIAA Journal,1978,16(12):1248-1254

45 郭恩民,周盛,陆亚钧.叶片排干涉对叶片颤振和强迫相应影响的研究.航空学报,1999,20(4):343-347

46 王梅.非定常流场分析结果向结构载荷压力场转化问题的解决.燃气涡轮试验与研究,2005,18(3):15-22

47 张锦,刘晓平.叶轮机振动模态分析理论及数值方法.北京:国防工业出版社,2001.20-22

48 Dowell E H,Hall K C.Modeling of fluid-structure interaction.Annual Review of Fluid Mechanics,2001,33:445-490

49 刘晓燕,杨超,吴志刚.基于小波的非定常气动力降阶模型.见:中国空气动力学学会空气弹性力学专业委员会编.第十一届全国空气弹性学术交流会会议论文集,昆明市,2009.206-211

50 Silva W A.Reduced-order models based on linear and nonlinear aerodynamic impulse responses.AIAA paper 1999-1262,1999

51 Grewal A,Zimcik D.Application of reduced order modelling to fluid-structure interaction analysis.AIAA paper 2008-5961,2008

52 Raveh D E.Reduced order models for nonlinear unsteadyaerodynamics.AIAA paper 2000-4785,2000

53 Cowan T J,Arena A S Jr,Gupta K K.Accelerating computational fluid dynamics based aeroelastic predicition using system identification.Journal of Aircraft,2001,38(1):81-87

54 Lai K L,Lum K.Reduced-order based flutter analysis for complex aeroelastic systems.AIAA paper 2008-6240,2008

55 Marques F D.Identification and prediction of unsteady transonic aerodynamic locals by multi-layer functions.Journal of Fluid and Structures,2001,15:83-106

56 Carlson H A,Roveda R.Models for controlling airfoil lift and drag.AIAA paper 2004-579,2004

57 Pettit C L,Beran P S.Reduced-order modeling for flutter prediction.AIAA paper 2000-1446,2000

58 Hall K C,Thomas J P,Dowell E H.Reduced-order modeling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique.AIAA Journal,2000,38(10):1853-1862

59 Thomas J P,Dowell E H,Hall K C.Three-dimensional transonic aeroelasticity using proper orthogonal decomposition based reduced order models.AIAA paper 2001-1526,2001

60 Dowell E H,Thomas J P,Hall K C.Transonic limit cycle oscillation analysis using reduced order aerodynamic models.Journal of Fluids and Structures,2004,19:17-27

61 Hall K C,Thomas J P,Dowell E H.Reduced-order modeling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique.AIAA paper 1999-0655,1999

62 Clark W S,Hall K C.A time-linearized navier-stokes analysis of stall flutter.Journal of Turbomachinery,2000,122(3):467-476

63 Morton S A,Melville R B,Visbal M R.Accuracy and coupling issues of aeroelastic navier-stokes solutions on deforming meshes.AIAA paper 1997-1085,1997

64 陈精一.ANSYS 工程分析实例教程.北京:中国铁道出版社,2007.102-107

65 He L.An Euler solution for unsteady flows around oscillating blades.Journal of Turbomachinery,1990,112(4):714-722

66 He L,Denton J D.Three-dimensional time-marching inviscid and viscous solutions for unsteady flows around vibrating blades.Journal of Turbo machinery,1994,116(1):469-476

67 Huff D L.Numerical simulations of unsteady viscous,transonic flow over isolated and cascaded airfoils using a deforming grid.ASME paper 92-GT-171,1992

68 Sayma A I,Vahati M,Imregun M.An Integrated nonlinear approach for turbomachinery forced response prediction.Part I:formulation.Journal of Fluids and Structures,2000,14(1):87-101

69 Carstens V,Kennne R,Schmitt S B.Coupled simulation of flow-structure interaction in turbo-machinery.Aerospace Science and Technology,2003,7:298-306

70 Cinnella P,De P P,Pascazio G,et al.A numerical method for turbomachinery aeroelasticity.Journal of Turbomachinery,2004,126(2):310-316

71 Chuang H A,Verdon J M.A Nonlinear numerical simulation for three dimensional flows through vibrating blade rows.ASME paper 98-GT-18,1998

72 Mcbean I,Hourigan K,Thompson M,et al.Prediction of flutter of turbine blades in a transonic annular cascade.Journal of Fluid Engineering,2005,127(6):1053-1058

73 Rzadkowski R,Gnesin V.3-D Inviscid self-excited vibrations of a blade row in the last stage turbine.Journal of Fluids and Structures,2007,23(6):858-873

74 金琰.叶轮机械中若干气流激振问题的流固耦合数值研究:[博士论文].北京:清华大学热能工程系,2002.90-103

75 张小伟,王延荣,张潇,等.涡轮机械叶片的流固耦合数值计算方法.航空动力学报,2009,24(7):1622-1626

76 Hirt C W,Amsden A A,Cook J L.An arbitrary Lagrangian-Eulerian computing method for all flow speeds.Journal of Comp.Phys.,1974,14:227-253

77 谢浩.三维非线性动态流体-结构耦合数值方法及其应用研究:[博士论文].西安:西安交通大学,2003.37-82

78 黄典贵.理想流场中流固耦合作用下叶片的动态特性研究.汽轮机技术,1998,40(4):235-238

79 陈晓明,赵成璧,林慰.浸入边界法的发展现状及应用.广东造船,2009,1(1):44-47

80 Peskin C S.Numerical analysis of blood flow in the heart.Journal of Computational Physics,1977,25(3):220-252

81 Saiki E M,Biringen S.Numerical simulation of a cylinder in uniform flow:application of a virtual boundary method.Journal of Computational Physics,1996,123(2):450-465

82 Zhong G H,Sun X F.A new simulation strategy for an oscillating cascade in turbomachinery using immersed boundary method.AIAA Journal of Propulsion and Power,2009,25(2):312-321

83 Liang A,Jing X,Sun X.Constructing spectral schemes of the immersed interface method via a global description of discontinuous functions.Journal of Computational Physics,2008,227(18):8341-8366

84 Danforth C E.Distortion-induced vibration in fan and compressor blade.Journal of Aircraft,1975,12(4):45-49

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