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    Analysis of Nonlinear Modal Damping Due to Friction at Blade Roots in Mistuned Bladed Disks

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003::page 031019-1
    Author:
    Chen, Junjie
    ,
    Zang, Chaoping
    ,
    Zhou, Biao
    ,
    Petrov, E. P.
    DOI: 10.1115/1.4049860
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method is proposed to analyze the modal damping in mistuned bladed-disk with root joints using large finite element models and the detailed description of frictional interactions at contact interfaces. The influence of mistuning on the dissipated energy for different blades on a bladed-disk and the modal damping factors for different vibration levels for any family of modes can be investigated. The dissipated energy and damping factors due to microslip are simulated by multitude of surface-to-surface elements modeling the friction contact interactions at root joints. The analysis is performed in the time domain, and an original reduction method is developed to obtain the results with acceptable computational times. The model reduction method allows the calculation of the modal damping of the mistuned assembly by evaluation of the energy dissipated at root joint of each individual blade using small parts of bladed disk sectors. The dependency of modal damping factor on blade mode shapes, engine-order excitation numbers, nodal diameter numbers, and vibration amplitudes is studied and the distributions of amplitude and dissipated energy on the mistuned bladed-disk are investigated using a realistic blade disk model.
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      Analysis of Nonlinear Modal Damping Due to Friction at Blade Roots in Mistuned Bladed Disks

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4277354
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorChen, Junjie
    contributor authorZang, Chaoping
    contributor authorZhou, Biao
    contributor authorPetrov, E. P.
    date accessioned2022-02-05T22:19:59Z
    date available2022-02-05T22:19:59Z
    date copyright2/22/2021 12:00:00 AM
    date issued2021
    identifier issn0742-4795
    identifier othergtp_143_03_031019.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277354
    description abstractA method is proposed to analyze the modal damping in mistuned bladed-disk with root joints using large finite element models and the detailed description of frictional interactions at contact interfaces. The influence of mistuning on the dissipated energy for different blades on a bladed-disk and the modal damping factors for different vibration levels for any family of modes can be investigated. The dissipated energy and damping factors due to microslip are simulated by multitude of surface-to-surface elements modeling the friction contact interactions at root joints. The analysis is performed in the time domain, and an original reduction method is developed to obtain the results with acceptable computational times. The model reduction method allows the calculation of the modal damping of the mistuned assembly by evaluation of the energy dissipated at root joint of each individual blade using small parts of bladed disk sectors. The dependency of modal damping factor on blade mode shapes, engine-order excitation numbers, nodal diameter numbers, and vibration amplitudes is studied and the distributions of amplitude and dissipated energy on the mistuned bladed-disk are investigated using a realistic blade disk model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Nonlinear Modal Damping Due to Friction at Blade Roots in Mistuned Bladed Disks
    typeJournal Paper
    journal volume143
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4049860
    journal fristpage031019-1
    journal lastpage031019-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003
    contenttypeFulltext
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