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    Computation of Isolated Periodic Solutions for Forced Response Blade-Tip/Casing Contact Problems

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 004::page 41011-1
    Author:
    Vadcard, Thibaut
    ,
    Thouverez, Fabrice
    ,
    Batailly, Alain
    DOI: 10.1115/1.4063704
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article introduces a numerical procedure dedicated to the identification of isolated branches of solutions for nonlinear mechanical systems. Here, it is applied to a fan blade subject to rubbing interactions and harmonic forcing. Both contact, which is initiated by means of the harmonic forcing, and dry friction are accounted for. The presented procedure relies on the computation of the system's nonlinear normal modes (NNM) and their analysis through the application of an energy principle derived from the Melnikov function. The dynamic Lagrangian frequency-time strategy associated with the harmonic balance method (DLFT-HBM) is used to predict the blade's dynamics response as well as to compute the autonomous nonlinear normal modes. The open industrial fan blade NASA rotor 67 is employed in order to avoid confidentiality issues and to promote the reproducibility of the presented results. Previous publications have underlined the complexity of NASA rotor 67's dynamics response as it undergoes structural contacts, thus making it an ideal benchmark blade when searching for isolated solutions. The application of the presented procedure considering a varying amplitude of the harmonic forcing allows to predict isolated branches of solutions featuring nonlinear resonances. With the use of the Melnikov energy principle, nonlinear modal interactions are shown to be responsible for the separation of branches of solutions from the main response curve. In the end, the application of the presented procedure on an industrial blade model with contact interactions demonstrates that it is both industry-ready and applicable to highly nonlinear mechanical systems.
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      Computation of Isolated Periodic Solutions for Forced Response Blade-Tip/Casing Contact Problems

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4295205
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    contributor authorVadcard, Thibaut
    contributor authorThouverez, Fabrice
    contributor authorBatailly, Alain
    date accessioned2024-04-24T22:25:52Z
    date available2024-04-24T22:25:52Z
    date copyright12/8/2023 12:00:00 AM
    date issued2023
    identifier issn0742-4795
    identifier othergtp_146_04_041011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295205
    description abstractThis article introduces a numerical procedure dedicated to the identification of isolated branches of solutions for nonlinear mechanical systems. Here, it is applied to a fan blade subject to rubbing interactions and harmonic forcing. Both contact, which is initiated by means of the harmonic forcing, and dry friction are accounted for. The presented procedure relies on the computation of the system's nonlinear normal modes (NNM) and their analysis through the application of an energy principle derived from the Melnikov function. The dynamic Lagrangian frequency-time strategy associated with the harmonic balance method (DLFT-HBM) is used to predict the blade's dynamics response as well as to compute the autonomous nonlinear normal modes. The open industrial fan blade NASA rotor 67 is employed in order to avoid confidentiality issues and to promote the reproducibility of the presented results. Previous publications have underlined the complexity of NASA rotor 67's dynamics response as it undergoes structural contacts, thus making it an ideal benchmark blade when searching for isolated solutions. The application of the presented procedure considering a varying amplitude of the harmonic forcing allows to predict isolated branches of solutions featuring nonlinear resonances. With the use of the Melnikov energy principle, nonlinear modal interactions are shown to be responsible for the separation of branches of solutions from the main response curve. In the end, the application of the presented procedure on an industrial blade model with contact interactions demonstrates that it is both industry-ready and applicable to highly nonlinear mechanical systems.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComputation of Isolated Periodic Solutions for Forced Response Blade-Tip/Casing Contact Problems
    typeJournal Paper
    journal volume146
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4063704
    journal fristpage41011-1
    journal lastpage41011-11
    page11
    treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 004
    contenttypeFulltext
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