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    Combined Methodology for Analysis of Rotary Systems

    Source: Journal of Vibration and Acoustics:;2001:;volume( 123 ):;issue: 004::page 428
    Author:
    Yuan Mao Huang
    ,
    Chin-Ming Wang
    ,
    Research Assistant
    DOI: 10.1115/1.1385204
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study develops a numerical method for analyzing the unbalanced effect of rotary systems by combining the finite element method, the transfer matrix method, the time marching numerical integration method and the Houbolt numerical method. Previous studies of the individual effects associated with the rotary inertia, gyroscopic phenomenon, shear deformation, axial loading and internal damping on the dynamic behavior of rotary systems are all incorporated and examined in this study. The calculated transient and steady displacements of components in two systems are comparable with the available data. The results show that maximum displacements occur in the transient states at some critical speeds to assure the importance for analyzing the unbalanced effect of the rotary systems. Compared with existing methods, this presently combined methodology provides a faster converging speed. In addition, this model should improve the predicted results for the transient dynamic analysis of rotary systems than those obtained from existing models.
    keyword(s): Force , Stress , Rotational inertia , Finite element methods , Numerical analysis , Disks , Displacement , Bearings , Damping , Finite element model , Shear deformation , Steady state , Degrees of freedom , Dynamic analysis AND Equations ,
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      Combined Methodology for Analysis of Rotary Systems

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/126100
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    • Journal of Vibration and Acoustics

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    contributor authorYuan Mao Huang
    contributor authorChin-Ming Wang
    contributor authorResearch Assistant
    date accessioned2017-05-09T00:06:21Z
    date available2017-05-09T00:06:21Z
    date copyrightOctober, 2001
    date issued2001
    identifier issn1048-9002
    identifier otherJVACEK-28859#428_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126100
    description abstractThis study develops a numerical method for analyzing the unbalanced effect of rotary systems by combining the finite element method, the transfer matrix method, the time marching numerical integration method and the Houbolt numerical method. Previous studies of the individual effects associated with the rotary inertia, gyroscopic phenomenon, shear deformation, axial loading and internal damping on the dynamic behavior of rotary systems are all incorporated and examined in this study. The calculated transient and steady displacements of components in two systems are comparable with the available data. The results show that maximum displacements occur in the transient states at some critical speeds to assure the importance for analyzing the unbalanced effect of the rotary systems. Compared with existing methods, this presently combined methodology provides a faster converging speed. In addition, this model should improve the predicted results for the transient dynamic analysis of rotary systems than those obtained from existing models.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCombined Methodology for Analysis of Rotary Systems
    typeJournal Paper
    journal volume123
    journal issue4
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.1385204
    journal fristpage428
    journal lastpage434
    identifier eissn1528-8927
    keywordsForce
    keywordsStress
    keywordsRotational inertia
    keywordsFinite element methods
    keywordsNumerical analysis
    keywordsDisks
    keywordsDisplacement
    keywordsBearings
    keywordsDamping
    keywordsFinite element model
    keywordsShear deformation
    keywordsSteady state
    keywordsDegrees of freedom
    keywordsDynamic analysis AND Equations
    treeJournal of Vibration and Acoustics:;2001:;volume( 123 ):;issue: 004
    contenttypeFulltext
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