KUANG J H,HUANG B W．Mode localization of a cracked blade disk[J]．Journal of Engineering for Gas Turbines and Power,1999,121:335-341．
[2]
MIGNOLET M P,RIVAS A J．Identification of mistuning characteristics of blade disks from free response date Part[J]．Journal of Engineering for Gas Turbines and Power,2001,123:395-403．
[3]
HUANG B W,KUANG J H．Mode localization in rotating mistuned turbo disk with coriolis effect[J]．International Journal of Mechanical Sciences 2001,43:1643-1660．
[4]
BLADH R,CASTANIER M P,PIERRE C．Effects of multistage coupling and disk flexibility on mistuned bladed disk dy- namics[J]．Journal of Engineering for Gas turbines and Power,2003,125:121-130．
[5]
EWINS D J．Vibration modes of blade mistuned blade disks[J]．Journal of Engineering for Power,1978,98:335-341．
[6]
WEI S T,PIERRE C．Localization phenomena in mistuned assemblies with cyclic symmetry part I:free vibrations[J]．Journal of Vibration,Acoustics,Stress,and Reliability in Design,1988,110:429-438．
[7]
WEI S T,PIERRE C．Localization phenomena in mistuned assemblies with cyclic symmetry partⅡ:forced vibrations．Jour- nal of Vibration,Acoustics,Stress,and Reliability in Design,1988,110:439-449．
[8]
CAPIEZ E,SOIZE C．Nonparametric modeling of random uncertainties for dynamic response of mistuned blade disks[J]．Journal of Engineering for Gas turbines and Power,2004,126:610-618．
[9]
MOYROUND F,FRANSSON T．A comparison of tow finite element reduction techniques for mistuned blade disks[J]．Journal of Engineering for Gas turbines and Power,2002,124:942-952．
