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    Boundary-Layer Effects in Composite Laminates: Part 1—Free-Edge Stress Singularities

    Source: Journal of Applied Mechanics:;1982:;volume( 049 ):;issue: 003::page 541
    Author:
    S. S. Wang
    ,
    I. Choi
    DOI: 10.1115/1.3162514
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A study of boundary-layer stress singularities in multilayered fiber-reinforced composite laminates is presented. Based on Lekhnitskii’s stress potentials and the theory of anisotropic elasticity, formulation of the problem leads to a pair of coupled governing partial differential equations (P.D.E.’s). An eigenfunction expansion method is developed to obtain the homogeneous solution for the governing P.D.E. ’s. The order or strength of boundary-layer stress singularity is determined by solving the transcendental characteristic equation obtained from the homogeneous solution for the problem. Numerical examples of the singular strength (or singular eigenvalues) of boundary-layer stresses are given for angle-ply and cross-ply composites as well as the cases of more general composite lamination.
    keyword(s): Composite materials , Laminates , Boundary layers , Stress singularity , Stress , Eigenfunctions , Fiber reinforced composites , Eigenvalues , Equations , Laminations , Partial differential equations AND Elasticity ,
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      Boundary-Layer Effects in Composite Laminates: Part 1—Free-Edge Stress Singularities

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    http://yetl.yabesh.ir/yetl1/handle/yetl/95338
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    • Journal of Applied Mechanics

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    contributor authorS. S. Wang
    contributor authorI. Choi
    date accessioned2017-05-08T23:12:27Z
    date available2017-05-08T23:12:27Z
    date copyrightSeptember, 1982
    date issued1982
    identifier issn0021-8936
    identifier otherJAMCAV-26204#541_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95338
    description abstractA study of boundary-layer stress singularities in multilayered fiber-reinforced composite laminates is presented. Based on Lekhnitskii’s stress potentials and the theory of anisotropic elasticity, formulation of the problem leads to a pair of coupled governing partial differential equations (P.D.E.’s). An eigenfunction expansion method is developed to obtain the homogeneous solution for the governing P.D.E. ’s. The order or strength of boundary-layer stress singularity is determined by solving the transcendental characteristic equation obtained from the homogeneous solution for the problem. Numerical examples of the singular strength (or singular eigenvalues) of boundary-layer stresses are given for angle-ply and cross-ply composites as well as the cases of more general composite lamination.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBoundary-Layer Effects in Composite Laminates: Part 1—Free-Edge Stress Singularities
    typeJournal Paper
    journal volume49
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3162514
    journal fristpage541
    journal lastpage548
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsLaminates
    keywordsBoundary layers
    keywordsStress singularity
    keywordsStress
    keywordsEigenfunctions
    keywordsFiber reinforced composites
    keywordsEigenvalues
    keywordsEquations
    keywordsLaminations
    keywordsPartial differential equations AND Elasticity
    treeJournal of Applied Mechanics:;1982:;volume( 049 ):;issue: 003
    contenttypeFulltext
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