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    Estimation of Forcing Function, Mistuning, and Modal Damping in a Bladed Rotor

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 005
    Author:
    Chauhan, Arjun Singh
    ,
    Sinha, Alok
    DOI: 10.1115/1.4045086
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with the estimation of forcing function, modal damping, and mistuned modal stiffnesses in a bladed rotor. Previous research on parameter estimation in a mistuned bladed rotor relies on the knowledge of the forcing function as well as the vibration data. This paper presents two novel approaches. The first approach relies on knowledge of both the forcing and vibration data. The parameters are treated as states of the system and an augmented state space model is created. Unscented Kalman filter (UKF) is then used on the steady-state data to estimate the parameters. The second approach eliminates the dependence on forcing data. Both the forcing and parameters are now treated as states of the system to construct an augmented state space model. UKF is then used on transient vibration data for estimation. Numerical results are presented for a simple model of a mistuned bladed rotor which considers a single mode of vibration per blade.
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      Estimation of Forcing Function, Mistuning, and Modal Damping in a Bladed Rotor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4274323
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    contributor authorChauhan, Arjun Singh
    contributor authorSinha, Alok
    date accessioned2022-02-04T14:45:54Z
    date available2022-02-04T14:45:54Z
    date copyright2020/02/14/
    date issued2020
    identifier issn0742-4795
    identifier othergtp_142_05_051001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274323
    description abstractThis paper deals with the estimation of forcing function, modal damping, and mistuned modal stiffnesses in a bladed rotor. Previous research on parameter estimation in a mistuned bladed rotor relies on the knowledge of the forcing function as well as the vibration data. This paper presents two novel approaches. The first approach relies on knowledge of both the forcing and vibration data. The parameters are treated as states of the system and an augmented state space model is created. Unscented Kalman filter (UKF) is then used on the steady-state data to estimate the parameters. The second approach eliminates the dependence on forcing data. Both the forcing and parameters are now treated as states of the system to construct an augmented state space model. UKF is then used on transient vibration data for estimation. Numerical results are presented for a simple model of a mistuned bladed rotor which considers a single mode of vibration per blade.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEstimation of Forcing Function, Mistuning, and Modal Damping in a Bladed Rotor
    typeJournal Paper
    journal volume142
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4045086
    page51001
    treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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