2018
DOI: 10.1115/1.4040898
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Intentional Response Reduction by Harmonic Mistuning of Bladed Disks With Aerodynamic Damping

Abstract: A harmonic mistuning concept for bladed disks is analyzed in order to intentionally reduce the forced response of specific modes below their tuned amplitude level. By splitting a mode pair associated with a specific nodal diameter pattern, the lightly damped traveling wave mode of the nominally tuned blisk is superposed with its counter-rotating complement. Consequently, a standing wave is formed in which the former wave train benefits from an increase in aerodynamic damping. Unlike previous analyses of random… Show more

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Cited by 6 publications
(4 citation statements)
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“…Besides, the SW modes defined by Eq. (3) are modified as [14]: (12) where the angle  depends on the constants K and M and is referred to as mode clocking.…”
Section: Kk ψψmentioning
confidence: 99%
“…Besides, the SW modes defined by Eq. (3) are modified as [14]: (12) where the angle  depends on the constants K and M and is referred to as mode clocking.…”
Section: Kk ψψmentioning
confidence: 99%
“…Willeks et al [38] studied the response reduction of the bladed disks with the aerodynamic damping by using the harmonic mistuning. Gao et al [39] gave the application of the hard-coating damper to the mistuned blisk for the passive vibration reduction.…”
Section: Introductionmentioning
confidence: 99%
“…Han and Mignolet [37] predicted the forced dynamic responses of the damped mistuned disk. Willeks et al [38] studied the response reduction of the bladed disks with the aerodynamic damping by using the harmonic mistuning. Gao et al [39] gave the application of the hard-coating damper to the mistuned blisk for the passive vibration reduction.…”
Section: Introductionmentioning
confidence: 99%