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    Uncertain Eigenvalue Analysis of Composite Laminated Plates by the Stochastic Finite Element Method

    Source: Journal of Manufacturing Science and Engineering:;1987:;volume( 109 ):;issue: 001::page 9
    Author:
    S. Nakagiri
    ,
    H. Takabatake
    ,
    S. Tani
    DOI: 10.1115/1.3187096
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Uncertain eigenvalue problem of linear vibration is analyzed by means of the stochastic finite element method, the basis of which utilizes mean-centered second order perturbation technique. Attention is paid to the fluctuation of the stacking sequence, that is, fiber orientation and layer thickness of FRP laminated plates. The stacking sequence is expressed in terms of probabilistic variables. The eigenvalue problem is formulated based on the Kirchhoff-Love’s theory of thin plate, the stretching, coupled and bending stiffnesses of which are uncertain due to the stacking sequence. The numerical analyses deal with the vibration of simply-supported graphite/epoxy plates. The sensitivity of the input stacking sequence and the correlation coefficients of the probabilistic variables are evaluated quantitatively.
    keyword(s): Composite materials , Finite element methods , Eigenvalues , Plates (structures) , Vibration , Fiber reinforced plastics , Graphite , Thickness , Linear vibration , Numerical analysis , Fibers AND Epoxy adhesives ,
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      Uncertain Eigenvalue Analysis of Composite Laminated Plates by the Stochastic Finite Element Method

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/102696
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    contributor authorS. Nakagiri
    contributor authorH. Takabatake
    contributor authorS. Tani
    date accessioned2017-05-08T23:25:09Z
    date available2017-05-08T23:25:09Z
    date copyrightFebruary, 1987
    date issued1987
    identifier issn1087-1357
    identifier otherJMSEFK-27723#9_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/102696
    description abstractUncertain eigenvalue problem of linear vibration is analyzed by means of the stochastic finite element method, the basis of which utilizes mean-centered second order perturbation technique. Attention is paid to the fluctuation of the stacking sequence, that is, fiber orientation and layer thickness of FRP laminated plates. The stacking sequence is expressed in terms of probabilistic variables. The eigenvalue problem is formulated based on the Kirchhoff-Love’s theory of thin plate, the stretching, coupled and bending stiffnesses of which are uncertain due to the stacking sequence. The numerical analyses deal with the vibration of simply-supported graphite/epoxy plates. The sensitivity of the input stacking sequence and the correlation coefficients of the probabilistic variables are evaluated quantitatively.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUncertain Eigenvalue Analysis of Composite Laminated Plates by the Stochastic Finite Element Method
    typeJournal Paper
    journal volume109
    journal issue1
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3187096
    journal fristpage9
    journal lastpage12
    identifier eissn1528-8935
    keywordsComposite materials
    keywordsFinite element methods
    keywordsEigenvalues
    keywordsPlates (structures)
    keywordsVibration
    keywordsFiber reinforced plastics
    keywordsGraphite
    keywordsThickness
    keywordsLinear vibration
    keywordsNumerical analysis
    keywordsFibers AND Epoxy adhesives
    treeJournal of Manufacturing Science and Engineering:;1987:;volume( 109 ):;issue: 001
    contenttypeFulltext
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