Boundary Value Problems with Symmetry and Their Approximation by Finite Elements, SIAM Journal on Applied Mathematics, vol.53, issue.5, pp.53-58, 1985. ,
DOI : 10.1137/0153064
Structural Dynamics and Vibration On Substructuring Technique: Application of Lagrange Multiplier Method on Cyclic Structures, Journal of Sound and Vibration, pp.247-252, 1998. ,
Effects of Mistuning on the Vibration of Turbomachine Blades induced by Wakes, Journal of Mechanical Engineering Science, pp.8-9, 1966. ,
Vibration Amplitudes of Compressor Blades Resulting from Scatter in Blade Natural Frequencies, ASME Journal of Engineering for Power, pp.91-94, 1969. ,
The Effects of Detuning upon the Forced Vibrations of Bladed Disks, Journal of Sound and Vibration, pp.9-10, 1969. ,
Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry Part II: Forced Vibrations, Journal of Vibration Acoustics Stress and Reliability in Design, vol.110, issue.4, pp.110-114, 1988. ,
DOI : 10.1115/1.3269548
An Adaptative Perturbation Scheme for the Analysis of Mistuned Bladed Disks, ASME Journal of Engineering for Gas Turbines and Power, pp.119-120, 1997. ,
A Novel Limit Distribution for the Analysis of Randomly Mistuned Bladed Disks, Journal of Engineering for Gas Turbines and Power, vol.123, issue.2, pp.123-125, 2001. ,
DOI : 10.1115/1.1339001
Model Development and Statistical Investigation of Turbine Blade Mistuning, Journal of Vibration Acoustics Stress and Reliability in Design, vol.106, issue.2, pp.106-108, 1984. ,
DOI : 10.1115/1.3269170
A higher order technique to compute the statistics of forced response of a mistuned bladed disk assembly, Journal of Sound and Vibration, vol.130, issue.2, pp.130-132, 1989. ,
DOI : 10.1016/0022-460X(89)90550-6
A Reduced-Order Model of Mistuning Using a Subset of Nominal Modes, ASME Journal of Engineering for Gas Turbines and Power, pp.123-126, 2001. ,
Component-Mode-Based Reduced order Modeling Techniques for Mistuned Bladed Disks-Part 1: Theoretical Models, ASME Journal of Engineering for Gas Turbines and Power, pp.123-124, 2001. ,
A New Aeroelastic Model For Mistuned Bladed Disks, 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, p.1533, 2002. ,
DOI : 10.2514/6.2002-1533
Identification of Mistuning Characteristics of Bladed Disks From Free Response Data???Part I, Journal of Engineering for Gas Turbines and Power, vol.123, issue.2, pp.123-125, 2001. ,
DOI : 10.1115/1.1338949
Identification of Mistuning Characteristics of Bladed Disks From Free Response Data??? Part II, Journal of Engineering for Gas Turbines and Power, vol.123, issue.2, pp.123-125, 2001. ,
DOI : 10.1115/1.1338950
Une approche probabiliste non paramétrique du phénomène de désaccordage des structuresàtures`turesà géométrie cyclique. Séminaire Descartes du Polytechnicum de Marne-La-Vallée, pp.65-74, 2002. ,
Maximum Amplification of Blade Response due to Mistuning: Localization and Mode Shapes Aspect of the Worst Disks, Proceedings of the ASME Turbo Expo, 2002. ,
A nonparametric model of random uncertainties for reduced matrix models in structural dynamics, Probabilistic Engineering Mechanics, 15£ 3¤, pp.277-294, 2000. ,
DOI : 10.1016/S0266-8920(99)00028-4
URL : https://hal.archives-ouvertes.fr/hal-00686293
Maximum Entropy Approach for Modeling Random Uncertainties in Transient Elastodynamics, Journal of the Acoustical Society of America, pp.109-114, 2001. ,
Vibration analysis of mistuned bladed-disk assemblies - inverse approach, AIAA Journal, vol.32, issue.4, pp.32-36, 1994. ,
DOI : 10.2514/3.12064
Coupling of Substructures for Dynamic Analyses, AIAA Journal, pp.6-7, 1968. ,
Nonlinear Dynamical Systems with Nonparametric Model of Random Uncertainties, Uncertainties in Engineering Mechanics, 1£ 1¤, pp.1-38, 2001. ,
Random Uncertainties Model in Dynamic Substructuring Using a Non-Parametric Probabilistic Model, ASCE Journal of Engineering Mechanics, 2002. ,
Mode localization and eigenvalue loci veering phenomena in disordered structures, Journal of Sound and Vibration, vol.126, issue.3, pp.126-129, 1988. ,
DOI : 10.1016/0022-460X(88)90226-X