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1
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0001759524
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Flutter and resonant vibration characteristics of engine blades
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Srinivansan, A.V.1
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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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Ewins, D.J.1
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4
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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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5
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Localization phenomena in mistuned assemblies with cyclic symmetry, part II: Forced vibrations
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Wei, S.T.1
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6
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84905734763
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Local/global effects of mistuning on the forced response of bladed disks
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International Gas Turbine Institute Turbo Expo, New Orleans, LA
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Rivas-Guerra, A. J., and Mignolet, M. P., 2001, "Local/Global Effects of Mistuning on the Forced Response of Bladed Disks," ASME Paper 2001-GT-0289, International Gas Turbine Institute Turbo Expo, New Orleans, LA.
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Rivas-Guerra, A.J.1
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7
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0020937374
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Spectral analysis of mistuned bladed disk assemblies by component mode synthesis
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Proc. ASME 9th Biennial Conference on Mechanical Vibration and Noise, Dearborn, MI
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Irretier, H.1
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Forced response of mistuned bladed disks using reduced-order modeling
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Salt Lake City, UT
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Kruse, M. J., and Pierre, C., 1996, "Forced Response of Mistuned Bladed Disks Using Reduced-Order Modeling," Proc. 37th AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference, Salt Lake City, UT, 4, pp. 1938-1950.
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Kruse, M.J.1
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9
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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., 1997, "A Reduced Order Approach for the Vibration of Mistuned Bladed Disk Assemblies," ASME J. Eng. Gas Turbines Power, 119(1), pp. 161-167.
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Yang, M.-T.1
Griffin, J.H.2
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10
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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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11
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84928563201
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A reduced order model of mistuning using a subset of nominal modes
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International Gas Turbine Institute Turbo Expo, Indianapolis, IN
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Yang, M.-T., and Griffin, J. H., 1999, "A Reduced Order Model of Mistuning Using a Subset of Nominal Modes," ASME Paper 99-GT-288, International Gas Turbine Institute Turbo Expo, Indianapolis, IN.
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(1999)
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Yang, M.-T.1
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12
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0031187030
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A normalized modal eigenvalue approach for resolving modal interaction
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Yang, M.-T., and Griffin, J. H., 1997, "A Normalized Modal Eigenvalue Approach for Resolving Modal Interaction," ASME J. Eng. Gas Turbines Power, 119(3), pp. 647-650.
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Yang, M.-T.1
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