| Citation: | Research on excitability of the wake of stator in aero-engine to high order resonance of bladed-disk[J]. Journal of Aerospace Power, 2017, 32(4): 780-790. doi: 10.13224/j.cnki.jasp.2017.04.002
|
| [1] |
Marshall J G,Imregun M.A review of aeroelasticity methods with emphasis on turbomachinery applications［J］.Journal of Fluids and Structures,1996,10(3):237-267.
|
| [2] |
Moffatt S,He L.On decoupled and fully-coupled methods for blade forced response prediction［J］.Journal of Fluids and Structures,2005,20(2):217-234.
|
| [3] |
Ning W, He L.Computation of unsteady flows around oscillating blades using linear and nonlinear harmonic Euler methods［J］.Journal of Turbomachinery,1998,120(3):508-514.
|
| [4] |
Giles M B.An approach for multi-stage calculations incorporating unsteadiness［R］.ASME Paper 92-GT-282,1992.
|
| [5] |
Hall K C,Clark W S,Lorence C B.A linearized Euler analysis of unsteady transonic flows in turbomachinery［J］.Journal of Turbomachinery,1994,116(3):477-488.
|
| [6] |
孟越.尾流激励情况下叶片强迫响应预估技术及气动非谐研究［D］.北京:北京航空航天大学,2007.MENG Yue.Prediction of blade forcing response under stator wake and aerodynamic mistuned influence［D］.Beijing:Beijing University of Aeronautics and Astronautics,2014.(in Chinese)
|
| [7] |
孟越,李琳,李其汉.气动非谐对叶片非定常气动激振力影响［J］.航空动力学报,2007,22(7):1060-1064.MENG Yue,LI Lin,LI Qihan.Study on the influence of aerodynamic mistuned on unsteady aerodynamic force of blade［J］.Journal of Aerospace Power,2007,22(7):1060-1064.(in Chinese)
|
| [8] |
辛健强.航空发动机叶盘转子结构的典型振动问题研究［D］.北京:北京航空航天大学,2011.XIN Jianqiang.Researches on typical problems of blisk rotor vibration in turbomachinery［D］.Beijing:Beijing University of Aeronautics and Astronautics,2015.(in Chinese)
|
| [9] |
Breard C,Vahdati M,Sayma A I,et al.An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion［J］.Journal of Engineering for Gas Turbines and Power,2002,124(1):196-208.
|
| [10] |
Bréard C,Green J S,Imregun M.Low-engine-order excitation mechanisms in axial-flow turbomachinery［J］.Journal of Propulsion and Power,2003,19(4):704-712.
|
| [11] |
Bladh R,Zhuang Q,Hu J,et al.Leakage-induced compressor blade excitation due to inter-segment gaps［R］.ASME Paper GT2012-70040,2012.
|
| [12] |
Figaschewsky F,Giersch T,Kühhorn A.Forced response prediction of an axial turbine rotor with regard to aerodynamically mistuned excitation［R］.ASME Paper GT2014-25896,2014.
|
| [13] |
Li L,Wang P.Evaluation of high-order resonance of blade under wake excitation［R］.ASME Paper GT2010-23148,2010.
|
| [14] |
王培屹.航空发动机叶盘结构流致振动抑制的理论研究［D］.北京:北京航空航天大学,2014.WANG Peiyi.Research on vibration suppression theory of bladed disk of aeroengine under fluid excitation［D］.Beijing:Beijing University of Aeronautics and Astronautics,2014.(in Chinese)
|
| [15] |
马浩然.关于气动激励的设计研究［D］.北京:北京航空航天大,2015.MA Haoran.Study on the design of aerodynamic excitation［D］.Beijing:Beijing University of Aeronautics and Astronautics,2015.(in Chinese)
|
DownLoad: