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    A Linearized Theory on Ground-Based Vibration Response of Rotating Asymmetric Flexible Structures

    Source: Journal of Vibration and Acoustics:;2006:;volume( 128 ):;issue: 003::page 375
    Author:
    I. Y. Shen
    ,
    Hyunchul Kim
    DOI: 10.1115/1.2172265
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is to develop a unified algorithm to predict vibration of spinning asymmetric rotors with arbitrary geometry and complexity. Specifically, the algorithm is to predict vibration response of spinning rotors from a ground-based observer. As a first approximation, the effects of housings and bearings are not included in this analysis. The unified algorithm consists of three steps. The first step is to conduct a finite element analysis on the corresponding stationary rotor to extract natural frequencies and mode shapes. The second step is to represent the vibration of the spinning rotor in terms of the mode shapes and their modal response in a coordinate system that is rotating with the spinning rotor. The equation of motion governing the modal response is derived through use of the Lagrange equation. To construct the equation of motion, explicitly, the results from the finite element analysis will be used to calculate the gyroscopic matrix, centrifugal stiffening (or softening) matrix, and generalized modal excitation vector. The third step is to solve the equation of motion to obtain the modal response, which, in turn, will lead to physical response of the rotor for a rotor-based observer or for a ground-based observer through a coordinate transformation. Results of the algorithm indicate that Campbell diagrams of spinning asymmetric rotors will not only have traditional forward and backward primary resonances as in axisymmetric rotors, but also have secondary resonances caused by higher harmonics resulting from the mode shapes. Finally, the algorithm is validated through a calibrated experiment using rotating disks with evenly spaced radial slots. Qualitatively, all measured vibration spectra show significant forward and backward primary resonances as well as secondary resonances as predicted in the theoretical analysis. Quantitatively, measured primary and secondary resonance frequencies agree extremely well with those predicted from the algorithm with mostly <3.5% difference.
    keyword(s): Force , Spin (Aerodynamics) , Equations of motion , Algorithms , Rotors , Vibration , Disks , Frequency , Shapes , Geometry , Resonance AND Finite element analysis ,
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      A Linearized Theory on Ground-Based Vibration Response of Rotating Asymmetric Flexible Structures

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    http://yetl.yabesh.ir/yetl1/handle/yetl/134952
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    contributor authorI. Y. Shen
    contributor authorHyunchul Kim
    date accessioned2017-05-09T00:22:13Z
    date available2017-05-09T00:22:13Z
    date copyrightJune, 2006
    date issued2006
    identifier issn1048-9002
    identifier otherJVACEK-28880#375_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/134952
    description abstractThis paper is to develop a unified algorithm to predict vibration of spinning asymmetric rotors with arbitrary geometry and complexity. Specifically, the algorithm is to predict vibration response of spinning rotors from a ground-based observer. As a first approximation, the effects of housings and bearings are not included in this analysis. The unified algorithm consists of three steps. The first step is to conduct a finite element analysis on the corresponding stationary rotor to extract natural frequencies and mode shapes. The second step is to represent the vibration of the spinning rotor in terms of the mode shapes and their modal response in a coordinate system that is rotating with the spinning rotor. The equation of motion governing the modal response is derived through use of the Lagrange equation. To construct the equation of motion, explicitly, the results from the finite element analysis will be used to calculate the gyroscopic matrix, centrifugal stiffening (or softening) matrix, and generalized modal excitation vector. The third step is to solve the equation of motion to obtain the modal response, which, in turn, will lead to physical response of the rotor for a rotor-based observer or for a ground-based observer through a coordinate transformation. Results of the algorithm indicate that Campbell diagrams of spinning asymmetric rotors will not only have traditional forward and backward primary resonances as in axisymmetric rotors, but also have secondary resonances caused by higher harmonics resulting from the mode shapes. Finally, the algorithm is validated through a calibrated experiment using rotating disks with evenly spaced radial slots. Qualitatively, all measured vibration spectra show significant forward and backward primary resonances as well as secondary resonances as predicted in the theoretical analysis. Quantitatively, measured primary and secondary resonance frequencies agree extremely well with those predicted from the algorithm with mostly <3.5% difference.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Linearized Theory on Ground-Based Vibration Response of Rotating Asymmetric Flexible Structures
    typeJournal Paper
    journal volume128
    journal issue3
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.2172265
    journal fristpage375
    journal lastpage384
    identifier eissn1528-8927
    keywordsForce
    keywordsSpin (Aerodynamics)
    keywordsEquations of motion
    keywordsAlgorithms
    keywordsRotors
    keywordsVibration
    keywordsDisks
    keywordsFrequency
    keywordsShapes
    keywordsGeometry
    keywordsResonance AND Finite element analysis
    treeJournal of Vibration and Acoustics:;2006:;volume( 128 ):;issue: 003
    contenttypeFulltext
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