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0001759524
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Flutter and resonant vibration characteristics of engine blades
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Vibration amplitudes of compressor blades resulting from scatter in blade natural frequencies
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Dye, R.C.F.1
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The effects of detuning upon the forced vibrations of bladed disks
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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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Localization phenomena in mistuned assemblei 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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ASME Paper 2001-GT-0289
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Rivas-Guerra, A.J.1
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Spectral analysis of mistuned bladed disk assemblies by component mode synthesis
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8
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Forced response of mistuned bladed disks using reduced-order modeling
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A reduced order approach for the vibration of mistuned bladed disk assemblies
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A reduced order modeling technique for mistuned bladed disks
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Castanier, M.P.1
Ottarson, G.2
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11
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-
0003436729
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A reduced order model of mistuning using a subset of nominal modes
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ASME Paper 99-GT-288
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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, Indiana.
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(1999)
International Gas Turbine Institute Turbo Expo, Indianapolis, Indiana
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Yang, M.-T.1
Griffin, J.H.2
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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.1
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