TY - GEN
T1 - An experimental investigation of vibration localization in bladed disks, Part II
T2 - ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1997
AU - Kruse, Marlin J.
AU - Pierre, Christophe
N1 - Publisher Copyright:
© Copyright 1997 by ASME.
PY - 1997
Y1 - 1997
N2 - The results of an experimental investigation on the effects of random blade mis tuning on the forced dynamic response of bladed disks are reported. Two experimental specimens are considered: a nominally periodic twelve-bladed disk with equal blade lengths, and the corresponding mistuned bladed disk, which features slightly different blades of random lengths. Both specimens are subject to traveling-wave excitations delivered by piezo-electric actuators. The primary aim of the experiment is 10 demonstrate the occurrence of an increase in forced response blade amplitudes due to mistuning, and to verify analytical predictions about the magnitude of these increases. In particular, the impact of localized mode shapes, engine order excitation, and disk structural coupling on the sensitivity of forced response amplitudes to blade mistuning is reported. This work reports one of the first systematic experiments carried out to demonstrate and quantify the effect of mistuning on the forced response of bladed disks.
AB - The results of an experimental investigation on the effects of random blade mis tuning on the forced dynamic response of bladed disks are reported. Two experimental specimens are considered: a nominally periodic twelve-bladed disk with equal blade lengths, and the corresponding mistuned bladed disk, which features slightly different blades of random lengths. Both specimens are subject to traveling-wave excitations delivered by piezo-electric actuators. The primary aim of the experiment is 10 demonstrate the occurrence of an increase in forced response blade amplitudes due to mistuning, and to verify analytical predictions about the magnitude of these increases. In particular, the impact of localized mode shapes, engine order excitation, and disk structural coupling on the sensitivity of forced response amplitudes to blade mistuning is reported. This work reports one of the first systematic experiments carried out to demonstrate and quantify the effect of mistuning on the forced response of bladed disks.
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U2 - 10.1115/97-GT-502
DO - 10.1115/97-GT-502
M3 - Conference contribution
AN - SCOPUS:84973664635
T3 - Proceedings of the ASME Turbo Expo
BT - Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award
Y2 - 2 June 1997 through 5 June 1997
ER -