An efficient technique for the computation of eigenvalue and eigenvector derivatives of cyclic structures, Computers & Structures, vol.81, issue.24-25, pp.2395-2400, 2003. ,
DOI : 10.1016/S0045-7949(03)00302-X
Nonparametric Modeling of Random Uncertainties for Dynamic Response of Mistuned Bladed Disks, Journal of Engineering for Gas Turbines and Power, vol.126, issue.3, pp.610-618, 2004. ,
DOI : 10.1115/1.1760527
URL : https://hal.archives-ouvertes.fr/hal-00686199
Consideration on the Benefits of Intentional Blade Mistuning for the Forced Response of Turbomachinery Rotors, Proceedings of the ASME Aerospace Division, pp.419-425, 1997. ,
Using Intentional Mistuning in the Design of Turbomachinery Rotors, AIAA Journal, vol.40, issue.10, pp.2077-2086, 2002. ,
DOI : 10.2514/2.1542
Optimization of Intentional Mistuning Patterns for the Reduction of the Forced Response Effects of Unintentional Mistuning: Formulation and Assessment, Journal of Engineering for Gas Turbines and Power, vol.125, issue.1, pp.131-140, 2003. ,
DOI : 10.1115/1.1498270
Eigenvector derivatives with repeated eigenvalues, AIAA Journal, vol.27, issue.4, pp.486-491, 1989. ,
DOI : 10.2514/3.10137
Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies, Journal of Engineering for Gas Turbines and Power, vol.91, issue.3, pp.182-188, 1969. ,
DOI : 10.1115/1.3574726
Influence of Mistuning on Rotor-Blade Vibrations, AIAA Journal, vol.13, issue.4, pp.460-464, 1975. ,
DOI : 10.2514/3.49731
The effects of detuning upon the forced vibrations of bladed disks, Journal of Sound and Vibration, vol.9, issue.1, pp.65-79, 1969. ,
DOI : 10.1016/0022-460X(69)90264-8
Vibration Modes of Mistuned Bladed Discs, ASME Journal of Engineering for Power, pp.349-355, 1976. ,
A reduction technique for mistuned bladed disks with superposition of large geometric mistuning and small model uncertainties, Proceedings of the 12?th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2008. ,
URL : https://hal.archives-ouvertes.fr/hal-01393687
Vibration Modeling of Bladed Disks Subject to Geometric Mistuning and Design Changes, 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, pp.2004-1686, 2004. ,
DOI : 10.2514/6.2004-1686
Dynamic Substructuring of Damped Structures Using Singular Value Decomposition, Journal of Applied Mechanics, vol.64, issue.2, pp.292-298, 1997. ,
DOI : 10.1115/1.2787306
URL : https://hal.archives-ouvertes.fr/hal-00770023
Efficient computation of modal sensitivities for systems with repeated frequencies, AIAA Journal, vol.26, issue.3, pp.1386-1390, 1988. ,
DOI : 10.2514/3.9897
Fatigue life estimates of mistuned blades via a stochastic approach, AIAA Journal, vol.18, issue.3, pp.318-323, 1980. ,
DOI : 10.2514/3.7654
Effect of mistuning on the vibration of turbo???machine blades induced by wakes, ARCHIVE: Journal of Mechanical Engineering Science 1959-1982 (vols 1-23), vol.8, issue.1, pp.15-21, 1966. ,
DOI : 10.1243/JMES_JOUR_1966_008_004_02
A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes, Journal of Engineering for Gas Turbines and Power, vol.123, issue.4, pp.893-900, 2001. ,
DOI : 10.1115/1.1385197
On the Forced Response of Harmonically and Partially Mistuned Bladed Disks. Part I: Harmonic Mistuning, International Journal of Rotating Machinery, vol.6, issue.1, pp.29-41, 2000. ,
DOI : 10.1155/S1023621X0000004X
A Reduced Order Modeling Technique for Mistuned Bladed Disks, Journal of Vibration and Acoustics, vol.119, issue.3, pp.439-447, 1997. ,
DOI : 10.1115/1.2889743
A Comparison of Two Finite Element Reduction Techniques for Mistuned Bladed Disks, Journal of Engineering for Gas Turbines and Power, vol.124, issue.4, pp.942-952, 2002. ,
DOI : 10.1115/1.1415741
URL : https://hal.archives-ouvertes.fr/hal-00508201