TY - GEN
T1 - A novel limit distribution for the analysis of randomly mistuned bladed disks
AU - Mignolet, Marc
AU - Lin, Chung Chih
N1 - Publisher Copyright:
Copyright © 1998 by ASME.
PY - 1996
Y1 - 1996
N2 - A recently introduced perturbation technique is employed to derive a novel closed form model for the probability density function of the resonant and near-resonant, steady state amplitude of blade response in randomly mistuned disks. In its most general form, this model is shown to involve six parameters but, in the important practical case of a pure stiffness (or frequency) mistiming, only three parameters are usually sufficient to completely specify this distribution. A series of numerical examples are presented that demonstrate the extreme reliability of this three-parameter model in accurately predicting the entire probability density function of the amplitude of response, and in particular the large amplitude tail of this distribution which is the most critical effect of mistuning.
AB - A recently introduced perturbation technique is employed to derive a novel closed form model for the probability density function of the resonant and near-resonant, steady state amplitude of blade response in randomly mistuned disks. In its most general form, this model is shown to involve six parameters but, in the important practical case of a pure stiffness (or frequency) mistiming, only three parameters are usually sufficient to completely specify this distribution. A series of numerical examples are presented that demonstrate the extreme reliability of this three-parameter model in accurately predicting the entire probability density function of the amplitude of response, and in particular the large amplitude tail of this distribution which is the most critical effect of mistuning.
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U2 - 10.1115/96-GT-414
DO - 10.1115/96-GT-414
M3 - Conference contribution
AN - SCOPUS:84930424565
T3 - ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996
BT - Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General
PB - American Society of Mechanical Engineers
T2 - ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996
Y2 - 10 June 1996 through 13 June 1996
ER -