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    Perturbations Methods in Structural Dynamics and Applications to Cyclic Symmetric Domains

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003::page 654
    Author:
    Bernard Lalanne
    DOI: 10.1115/1.1924430
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design of components must take into account the irregularities inherent to the manufacturing process. When the structures have close eigenvalues, small mass and stiffness variations or the damping generate strong variations of the eigenmodes: these structures are then not robust. Here, their dynamics has been analyzed by perturbation method, in the dissipative cases and with coupling within a light fluid. A new perturbation method allows first order developments whatever the spectral density may be. Applications to many different vibration problems are presented: aeroelasticity, mode veering problem, maximum amplitude of forced response in cyclic symmetric domains, with detuning and/or mistuning, i.e., the most important reliability problem in turbomachinery. The results of this study provide a new estimation of the amplification factor and damping due to mistuning and aerodynamic coupling.
    keyword(s): Stability , Resonance , Waves , Damping , Vibration , Disks , Eigenvalues , Structural dynamics , Aeroelasticity , Stiffness , Spectral energy distribution , Fluids , Force , Turbomachinery , Frequency , Acoustics , Manufacturing , Dynamics (Mechanics) AND Flutter (Aerodynamics) ,
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      Perturbations Methods in Structural Dynamics and Applications to Cyclic Symmetric Domains

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    https://yetl.yabesh.ir/yetl1/handle/yetl/131780
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    contributor authorBernard Lalanne
    date accessioned2017-05-09T00:16:09Z
    date available2017-05-09T00:16:09Z
    date copyrightJuly, 2005
    date issued2005
    identifier issn1528-8919
    identifier otherJETPEZ-26871#654_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131780
    description abstractThe design of components must take into account the irregularities inherent to the manufacturing process. When the structures have close eigenvalues, small mass and stiffness variations or the damping generate strong variations of the eigenmodes: these structures are then not robust. Here, their dynamics has been analyzed by perturbation method, in the dissipative cases and with coupling within a light fluid. A new perturbation method allows first order developments whatever the spectral density may be. Applications to many different vibration problems are presented: aeroelasticity, mode veering problem, maximum amplitude of forced response in cyclic symmetric domains, with detuning and/or mistuning, i.e., the most important reliability problem in turbomachinery. The results of this study provide a new estimation of the amplification factor and damping due to mistuning and aerodynamic coupling.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerturbations Methods in Structural Dynamics and Applications to Cyclic Symmetric Domains
    typeJournal Paper
    journal volume127
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1924430
    journal fristpage654
    journal lastpage662
    identifier eissn0742-4795
    keywordsStability
    keywordsResonance
    keywordsWaves
    keywordsDamping
    keywordsVibration
    keywordsDisks
    keywordsEigenvalues
    keywordsStructural dynamics
    keywordsAeroelasticity
    keywordsStiffness
    keywordsSpectral energy distribution
    keywordsFluids
    keywordsForce
    keywordsTurbomachinery
    keywordsFrequency
    keywordsAcoustics
    keywordsManufacturing
    keywordsDynamics (Mechanics) AND Flutter (Aerodynamics)
    treeJournal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003
    contenttypeFulltext
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