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1
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Coupling of turbomachine blade vibrations through the rotor
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Wagner, J.T.1
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2
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Vibration amplitudes of compressor blades resulting from scatter in blade natural frequencies
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The effects of detuning upon the forced vibrations of bladed disks
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A study of resonance coincidence in bladed discs
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5
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Influence of mistuning on rotor-blade vibrations
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El-Bayoumy, L. E. and Srinivasan, A. V., "Influence of Mistuning on Rotor-Blade Vibrations," AIAA Journal, Vol. 13, No. 4, 1975, pp. 460-464.
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Model development and statistical investigation of turbine blade mistuning
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Griffin, J.H.1
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7
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Localization phenomena in mistuned assemblies with cyclic symmetry, part I: Free vibrations
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Wei, S.T.1
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Localization phenomena in mistuned assemblies with cyclic symmetry, part II: Forced vibrations
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Wei, S. T. and Pierre, C., "Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry, Part II: Forced Vibrations," ASME Journal of Vibration, Acoustics, Stress, and Reliability in Design, Vol. 110, No. 4, 1988, pp. 439-449.
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(1988)
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Wei, S.T.1
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9
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0002455070
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An adaptive perturbation scheme for the analysis of mistuned bladed disks
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Lin, C.-C. and Mignolet, M. P., "An Adaptive Perturbation Scheme for the Analysis of Mistuned Bladed Disks," ASME Journal of Engineering for Gas Turbines and Power, Vol. 119, No. 1, 1997, pp. 153-160.
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Lin, C.-C.1
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10
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Spectral analysis of mistuned bladed disk assemblies by component mode synthesis
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Irretier, H., "Spectral Analysis of Mistuned Bladed Disk Assemblies by Component Mode Synthesis," in Vibrations of Bladed Disk Assemblies, Proceedings of the ASME 9th Biennial Conference on Mechanical Vibration and Noise, Dearborn, Michigan, 1983, pp. 115-125.
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Irretier, H.1
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11
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Forced response of mistuned bladed disks using reduced-order modeling
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Kruse, M. J. and Pierre, C., "Forced Response of Mistuned Bladed Disks Using Reduced-Order Modeling," Proceedings of the 37th AIAA/ASME Structures, Structural Dynamics, and Materials Conference, Salt Lake City, Utah, 1996.
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Kruse, M.J.1
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12
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Dynamic response of an industrial turbomachinery rotor
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Kruse, M. J. and Pierre, C., "Dynamic Response of an Industrial Turbomachinery Rotor," Proceedings of the 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Lake Buena Vista, Florida, 1996.
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Kruse, M.J.1
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13
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0031187042
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A reduced-order modeling technique for mistuned bladed disks
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Castanier, M.P.1
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14
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0032641536
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Reduced order modeling and vibration analysis of mistuned bladed disk assemblies with shrouds
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Bladh, R., Castanier, M. P., and Pierre, C., "Reduced Order Modeling and Vibration Analysis of Mistuned Bladed Disk Assemblies with Shrouds," ASME Journal of Engineering for Gas Turbines and Power, Vol. 121, No. 3, 1999, pp. 515-522.
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Bladh, R.1
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Component-mode-based reduced order modeling techniques for mistuned bladed disks-part I: Theoretical models
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Bladh, R., Castanier, M. P., and Pierre, C., "Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks-Part I: Theoretical Models," ASME Journal of Engineering for Gas Turbines and Power, Vol. 123, No. 1, 2001, pp. 89-99.
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16
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Component-mode-based reduced order modeling techniques for mistuned bladed disks-part II: Application
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Bladh, R., Castanier, M. P., and Pierre, C., "Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks-Part II: Application," ASME Journal of Engineering for Gas Turbines and Power, Vol. 123, No. 1, 2001, pp. 100-108.
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A comparison of two finite element reduction techniques for mistuned bladed-disks
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Moyroud, F., Jacquet-Richardet, G., and Fransson, T., "A Comparison of Two Finite Element Reduction Techniques for Mistuned Bladed-Disks," Proceedings of the 45th ASME Gas Turbine and Aeroengine Technical Congress, Exposition and Users Symposium, Munich, Germany, 2000.
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Moyroud, F.1
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18
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0000494175
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A reduced order approach for the vibration of mistuned bladed disk assemblies
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Yang, M.-T. and Griffin, J. H., "A Reduced Order Approach for the Vibration of Mistuned Bladed Disk Assemblies," ASME Journal of Engineering for Gas Turbines and Power, Vol. 119, 1997, pp. 161-167.
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Yang, M.-T.1
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0035482548
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A reduced order model of mistuning using a subset of nominal system modes
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Yang, M.-T. and Griffin, J. H., "A Reduced Order Model of Mistuning Using a Subset of Nominal System Modes," ASME Journal of Engineering for Gas Turbines and Power, Vol. 123, 2001, pp. 893-900.
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A new method for dynamic analysis of mistuned bladed disks based on the exact relationship between tuned and mistuned systems
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Petrov, E.P.1
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Aeroelastic modal characteristics of mistuned blade assemblies: Mode localization and loss of eigenstructure
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A normalized modal eigenvalue approach for resolving modal interaction
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Yang, M.-T. and Griffin, J. H., "A Normalized Modal Eigenvalue Approach for Resolving Modal Interaction," ASME Journal of Engineering for Gas Turbines and Power, Vol. 119, 1997, pp. 647-650.
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Yang, M.-T.1
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Dynamic response predictions for a mistuned industrial turbomachinery rotor using reduced order modeling
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Bladh, R., Castanier, M. P., Pierre, C., and Kruse, M. J., "Dynamic Response Predictions for a Mistuned Industrial Turbomachinery Rotor Using Reduced Order Modeling," ASME Journal of Engineering for Gas Turbines and Power, Vol. 124, No. 2, 2002, pp. 311-324.
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Bladh, R.1
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