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Bibliographie[ 1] T.J. Anderson, B. Balachandran, and A. H. Nayfeh. Nonlinear resonances in a flexiblecantilever beam. Journal of Sound and Vibration, 158(3) :497-515, 1992.P.A. Atkins, G.R. Tomlinson, and J.R. Wright. Force appropriation of simple nonlinearsystems. In 13th Internationnal Modal Analysis Congress, pages 146-157, 1995.E. Bakker and H.B. Pacejka. Tyre modelling for use in vehicle dynamics studies. Societyof Automotive Studies, SAE-P 89 0087 :119-158, 1989.R. Balagangadhar and J.C. Slater. On the convergence of nonlinear modes in a finite elementmodel. In 16th Internationnal Modal Analysis Congress, volume 2, pages 1460-1466, 1998.S. Belizzi and R. Bouc. Analysis of multi-degree of freedom strongly non-linear mechanicalsystems with random input, part i : Non-linear modes and stochastic averaging. ProbalisticEngineering Mechanics, 14 :229-244, 1999.S. Belizzi, P. Guillemain, and R. Kronland-Martinet. Extraction par transformation degabor des modes non-linéaires d'un système mécanique à plusieurs degrés de liberté. In 1eCongès Français de Me'canique, page Réf.579, 1999.N. Boivin, S. W. Shaw, and C. Pierre. Non-linear modal analysis of structural systemsfeaturing internal resonances. Journal of Sound and Vibration, 182(2) :336-341, 1995.J.P. Boudot. Modélisation des bruits de freinage des véhicules industriels. PhD thesis, EcoleCentrale de Lyon, 1995.A. El Boukili and A. Marroco. Arclength continuation for semiconductor equation. Rapportde Recherche INRIA, RR-2546.T.D. Burton. Describing function analysis of nonlinear gear shimmy. In Winter AnnualMeeting, ASME, Washington, pages 1-9, 1981.H.R. Busby, C. Nopporn, and R. Singh. Experimental modal analysis of non-linear systems:a feasibility study. Journal of Sound and Vibration, 180(3) :415-427, 1986.J. Carr. Applications of Centre Manifold Theory. Springer-Verlag, New York, 1981.T. Caughey. Equivalent linearisation techniques. Journal of the Acoustics Society of America,35 :1706-1711, 1963.T.K. Caughey and A.F. Vakakis. A method for examining steady state solutions of forceddiscrete systems with strong non-linearity. International Journal of Non-linear Mechanics,26 :89-103, 1991.C. F. Chang. The dynamic finite element modeling of aircraft landing system. In DE- Vol.8-1, ASME: Design Engineering Technical Conferences, volume 3-Part A, pages 1217-1227,1995.162
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ECOLE CENTRALE DE LYONAnnée 2001 N
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ECOLE CENTRALE DE LYONListe des per
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ECOLE CENTRALE DE LYONListe des per
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RemerciementsCe travail a été ré
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4TITRE et RESUME en anglais:Expéri
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6 TABLE DES MATIÈRES2.5.1 Introduc
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8 INTRODUCTIONIntroductionDans le c
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10 INTRODUCTIONsont proposés pour
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12 CHAPITRE 1. LES MODES NORMAUX DE
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ji28 CHAPITRE 1. LES MODES NORMAUX
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30 CHAPITRE 2. APPROXIMATION DES MO
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32 CHAPITRE 2.APPROXIMATION DESMODE
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m2x2+c2x2+k2(x2xl)+k3(x2x3)+a2(x2--
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68 CHAPITRE 3. SYSTÈMES DISSIPATIF
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70 CHAPITRE 3. SYSTÈMES DISSIPA TI
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Chapitre 4Analyse des phénomènesn
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78 CHAPITRE 4. ANALYSE DES PHÉNOM
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Chapitre 5Identification non-linéa
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98 CHAPITRE 5. IDENTIFICATION NON-L
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102 CHAPITRE 5. IDENTIFICATION NON-
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