[1] |
Ewins D J,Imregun M.Vibration modes of packeted bladed disks[J].Journal of Vibration,Acoustics,Stress and Reliability in Design,1984,106(2):175-180.
|
[2] |
Wei S T,Pierre C.Localization phenomena in mistuned assemblies with cyclic symmetry:Part 2 forced vibrations[J].Journal of Vibration,Acoustics,Stress and Reliability in Design,1988,110(4):439-449.
|
[3] |
Pierrre C,Murthy D V.Aeroelastic modal characteristics of mistuned blade assemblies: mode localization and loss of eigenstructure[J].AIAA Journal,1992,30(10):2483-2496.
|
[4] |
Ottarsson G,Pierre C.A Transfer matrix approach to free vibration localization in mistuned bladed assemblies[J].Journal of Sound and Vibration,1996,197(5):589-618.
|
[5] |
Petrov E P,Ewins D J.Analysis of the worst mistuning patterns in bladed disk assemblies[J].Journal of Turbomachinery,2003,125(4):623-631.
|
[6] |
Petrov E P,Sanliturk K Y ,Ewins D.J.A new method for dynamic analysis of mistuned bladed disks based on exact relationship between tuned and mistuned systems[J].Journal of Engineering for Gas Turbines and Power,2002,122(3):586-597.
|
[7] |
Petrov E P,Sayma A I.Forced response variation of aerodynamically and structurally mistuned turbo-machinery rotors[R].ASME Paper GT2006-90948,2006.
|
[8] |
Sever I A,Petrov E P,Ewins D J.Experimental and numerical investigation of rotating bladed disk forced response using underplatform friction dampers[J].Journal of Engineering for Gas Turbines and Power,2008,130(4):042503.1-042503.11.
|
[9] |
Nikolic M,Petrov E P,Ewins D J.Robust strategies for forced response reduction of bladed disks based on large mistuning concept[J].Journal of Engineering for Gas Turbines and Power,2008,130(2):022501.1-022501.11.
|
[10] |
Petrov E P.Reduction of forced response levels for bladed discs by mistuning:overview of the phenomenon[R].ASME Paper GT2010-23299,2010.
|
[11] |
Petrov E P.A method for forced response analysis of mistuned bladed disks with aerodynamic effects included[J].Journal of Engineering for Gas Turbines and Power,2010,132(6):062502.1-062502.10.
|
[12] |
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.
|
[13] |
廖海涛,王建军,李其汉.随机失谐叶盘结构失谐特性分析[J].航空动力学报,2010,25(1):160-168.LIAO Haitao,WANG Jianjun,LI Qihan.Mistuning characteristics analysis of mistuned bladed disk assemblies [J].Journal of Aerospace Power,2010,25(1):160-168.(in Chinese)
|
[14] |
白斌,白广忱,童晓晨,等.整体叶盘结构失谐振动的国内外研究状况[J].航空动力学报,2014,29(1):91-103.BAI Bin,BAI Guangchen,TONG Xiaochen,et al.Research on vibration problem of integral mistuned balded disk assemblies at home and abroad[J].Journal of Aerospace Power,2014,29(1):91-103.(in Chinese)
|
[15] |
王红建,贺尔铭,余仕侠.具有干摩擦散乱失谐的叶盘受迫响应特性[J].航空动力学报,2006,21(4):711-715.WANG Hongjian,HE Erming,YU Shixia.Forced response characteristics of bladed disks with disordered dry friction[J].Journal of Aerospace Power,2006,21(4):711-715.(in Chinese)
|
[16] |
袁惠群,张亮.基于蚁群算法的航空发动机失谐叶片减振排布优化分析[J].振动与冲击,2012,31(11):169-172.YUAN Huiqun,ZHANG Liang.Optimization of mistuning blades arrangement for vibration absorption in an aero-engine based on artificial ant colony algorithm[J].Journal of Vibration and Shock,2012,31(11):169-172.(in Chinese)
|
[17] |
袁惠群,杨少明.基于蚁群算法和模态局部化参数的失谐叶盘减振研究[J].东北大学学报(自然科学版),2010,31(11):1611-1614.YUAN Huiqun ,YANG Shaoming.Vibration reduction of mistuned blade disc by ant colony algorithm and modal localization parameter[J].Journal of Northeastern University (Natural Science),2010,31(11):1611-1614.(in Chinese)
|
[18] |
袁惠群,张亮.航空发动机转子失谐叶片减振安装优化分析[J].振动、测试与诊断,2011,31(5):647-651.YUAN Huiqun,ZHANG Liang.Optimization analysis on mistuning blades of vibration absorption in aero-engine [J].Journal of Vibration,Measurement and Diagnosis,2011,31(5):647-651.(in Chinese)
|