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    Vibration of Clamped Circular Symmetric Laminates

    Source: Journal of Vibration and Acoustics:;1994:;volume( 116 ):;issue: 002::page 141
    Author:
    K. M. Liew
    DOI: 10.1115/1.2930404
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Treated in this paper is the free-flexural vibration analysis of symmetrically laminated thin circular plates. The total energy functional for the laminated plates is formulated where the pb -2 Ritz method is applied for the solution. The assumed displacement is defined as the product of (1) a two-dimensional complete polynomial function and (2) a basic boundary function. The simplicity and accuracy of the numerical procedure will be demonstrated by solving some plate examples. In the present study, the effects of material properties, number of layers and fiber stacking sequences upon the vibration frequency parameters are investigated. Selected mode shapes by means of contour plots for several 16-ply laminated plates with different fiber stacking sequences and composite materials are presented. This study may provide valuable information for researchers and engineers in design applications. In addition, the present solution plays an important role in increasing the existing data base for future references.
    keyword(s): Composite materials , Fibers , Engineers , Laminates , Oscillating frequencies , Materials properties , Design , Plates (structures) , Vibration , Databases , Displacement , Polynomials , Shapes AND Vibration analysis ,
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      Vibration of Clamped Circular Symmetric Laminates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/114654
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    contributor authorK. M. Liew
    date accessioned2017-05-08T23:46:03Z
    date available2017-05-08T23:46:03Z
    date copyrightApril, 1994
    date issued1994
    identifier issn1048-9002
    identifier otherJVACEK-28814#141_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114654
    description abstractTreated in this paper is the free-flexural vibration analysis of symmetrically laminated thin circular plates. The total energy functional for the laminated plates is formulated where the pb -2 Ritz method is applied for the solution. The assumed displacement is defined as the product of (1) a two-dimensional complete polynomial function and (2) a basic boundary function. The simplicity and accuracy of the numerical procedure will be demonstrated by solving some plate examples. In the present study, the effects of material properties, number of layers and fiber stacking sequences upon the vibration frequency parameters are investigated. Selected mode shapes by means of contour plots for several 16-ply laminated plates with different fiber stacking sequences and composite materials are presented. This study may provide valuable information for researchers and engineers in design applications. In addition, the present solution plays an important role in increasing the existing data base for future references.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleVibration of Clamped Circular Symmetric Laminates
    typeJournal Paper
    journal volume116
    journal issue2
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.2930404
    journal fristpage141
    journal lastpage145
    identifier eissn1528-8927
    keywordsComposite materials
    keywordsFibers
    keywordsEngineers
    keywordsLaminates
    keywordsOscillating frequencies
    keywordsMaterials properties
    keywordsDesign
    keywordsPlates (structures)
    keywordsVibration
    keywordsDatabases
    keywordsDisplacement
    keywordsPolynomials
    keywordsShapes AND Vibration analysis
    treeJournal of Vibration and Acoustics:;1994:;volume( 116 ):;issue: 002
    contenttypeFulltext
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