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    On the Interaction of Multiple Traveling Wave Modes in the Flutter Vibrations of Friction-Damped Tuned Bladed Disks

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 004::page 42501
    Author:
    Krack, Malte
    ,
    Panning-von Scheidt, Lars
    ,
    Wallaschek, Jörg
    DOI: 10.1115/1.4034650
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is well-known that flutter vibrations of bladed disks can be saturated by dry friction. Previous theoretical investigations indicated that the steady-state, friction-damped flutter vibrations of tuned bladed disks are always dominated by a single traveling wave component, even if multiple traveling wave forms are unstable. This contrasts recent experimental investigations where multiple traveling wave forms were found to participate at steady state. In this paper, we demonstrate that this phenomenon can be explained by nonlinear frictional interblade coupling. To this end, we consider a simple phenomenological model of a bladed disk with frictional intersector coupling and two unstable traveling waves forms. Vibrations occur not only in the form of limit cycle oscillations (periodic) but also in the form of limit torus oscillations (quasi-periodic). It is shown how the limit state depends on the initial conditions, and that the occurrence of multiwave flutter depends on the proximity of the complex eigenvalues of the associated unstable waves. Finally, by computing the limit torus oscillation with a frequency-domain method, we lay the cornerstone for the systematic prediction of friction-saturated flutter vibrations of state-of-the-art bladed disk models.
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      On the Interaction of Multiple Traveling Wave Modes in the Flutter Vibrations of Friction-Damped Tuned Bladed Disks

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4233667
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorKrack, Malte
    contributor authorPanning-von Scheidt, Lars
    contributor authorWallaschek, Jörg
    date accessioned2017-11-25T07:15:47Z
    date available2017-11-25T07:15:47Z
    date copyright2016/18/10
    date issued2017
    identifier issn0742-4795
    identifier othergtp_139_04_042501.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233667
    description abstractIt is well-known that flutter vibrations of bladed disks can be saturated by dry friction. Previous theoretical investigations indicated that the steady-state, friction-damped flutter vibrations of tuned bladed disks are always dominated by a single traveling wave component, even if multiple traveling wave forms are unstable. This contrasts recent experimental investigations where multiple traveling wave forms were found to participate at steady state. In this paper, we demonstrate that this phenomenon can be explained by nonlinear frictional interblade coupling. To this end, we consider a simple phenomenological model of a bladed disk with frictional intersector coupling and two unstable traveling waves forms. Vibrations occur not only in the form of limit cycle oscillations (periodic) but also in the form of limit torus oscillations (quasi-periodic). It is shown how the limit state depends on the initial conditions, and that the occurrence of multiwave flutter depends on the proximity of the complex eigenvalues of the associated unstable waves. Finally, by computing the limit torus oscillation with a frequency-domain method, we lay the cornerstone for the systematic prediction of friction-saturated flutter vibrations of state-of-the-art bladed disk models.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Interaction of Multiple Traveling Wave Modes in the Flutter Vibrations of Friction-Damped Tuned Bladed Disks
    typeJournal Paper
    journal volume139
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4034650
    journal fristpage42501
    journal lastpage042501-9
    treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 004
    contenttypeFulltext
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