| Citation: | XIN Jian-qiang, WANG Jian-jun. Forced response characteristic of bladed disk with aerodynamic mistuning[J]. Journal of Aerospace Power, 2012, 27(4): 801-810.
|
| [1] |
宋兆泓.航空燃气涡轮发动机强度设计[M].北京:北京航空航天大学出版社,1988.
|
| [2] |
王建军,李其汉.航空发动机失谐叶盘振动减缩模型与应用[M].北京:国防工业出版社,2009.
|
| [3] |
Castanier M P,Pierre C.Modeling and analysis of mistuned bladed disk vibration:status and emerging directions [J].Journal of Propulsion and Power,2006, 22(2):384-396.
|
| [4] |
王建军,李其汉,朱梓根. 失谐叶片-轮盘结构系统振动局部化问题的研究 进展[J].力学进展,2000,30(4):517-528. WANG Jianjun,LI Qihan,ZHU Zigen.Vibatory localization of mistuned bladed disk assemblies:a reviwe[J].Advances in Mechnics,2000,30(4):517-528.(in Chinese)
|
| [5] |
YAO Jianyao,WANG Jianjun,LI Qihan.Robustness analysis of mistuned bladed disk using the upper bound of structured singular value[J].ASME Journal of Engineering for Gas Turbines and Power, 2009,131(3):032501(7 pages).
|
| [6] |
于长波.失谐叶盘结构的建模方法与振动特性研究.北京:北京航空航天大学,2010. YU Changbo.Investigation on the modeling method and vibratory characteristics of mistuned blades disk structures.Beijing: Beijng University of Aeronautics and Astronautics,2010.
|
| [7] |
王帅.整体叶盘结构失谐识别方法和动态特性实验研究.北京:北京航空航天大学,2010. WANG Shuai.Mistuning identification theory and dynamic characteristic experiment for integrally bladed disk.Beijing: Beijng University of Aeronautics and Astronautics,2010.
|
| [8] |
Kemp R H,Hirschberg M H.Theoretical and experimental analysis of the reduction of rotor blade vibration in turbomachinery through the use of modified stator vane spacing.NACA-TN-4373,1958.
|
| [9] |
Gottfried D A,Fleeter S.Passive detuning for HCF reduction.AIAA 2002-3634,2002
|
| [10] |
Kaneko Y,Mori K,Okui H.Study on the effect of asymmetric vane spacing on vibratory stress of blade.ASME paper GT-2004-53023,2004.
|
| [11] |
孟越,李林,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.Unsteady aerodynamic force of blade under aerodynamic mistuned influence[J].Journal of Aerospce Power,2007,22(7):1060-1064.(in Chinese)
|
| [12] |
孟越,李林,李其汉.不对称静子叶片非谐方案研究[J].航空动力学报,2007,22(12):2083-2088. MENG Yue,LI Lin,LI Qihan.Asymmetry stator mistuned blade design and research[J].Journal of Aerospace Power,2007,22(12):2083-2088.(in Chinese)
|
| [13] |
姚建尧.流体激励下谐调和失谐叶盘结构响应分析.北京:北京航空航天大学,2010. YAO Jianyao.Response analysis for tuned and mistuned bladed disk Under fluid excitation.Beijing: Beijng University of Aeronautics and Astronautics,2010.
|
| [14] |
钟万勰.应用力学对偶体系[M].北京:科学出版社,2002.
|
| [15] |
Seinturier E,Lombard J P,Dumas M,et al.Forced response prediction methodology for the design of HP compressors bladed disks.ASME paper GT-2004-53372, 2004.
|
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