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    The Fiber Composite With Nonlinear Interface—Part II: Antiplane Shear

    Source: Journal of Applied Mechanics:;2000:;volume( 067 ):;issue: 004::page 733
    Author:
    A. J. Levy
    DOI: 10.1115/1.1329320
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper treats the effective antiplane shear response of a composite consisting of fibers that interact with the matrix through nonlinear Needleman-type cohesive zones. The first paper (Part I) examines effective axial tension response. The composite cylinders representation of a representative volume element (RVE) is employed throughout. For antiplane shear loading the elastic field solution for a single composite cylinder is found in the form of a series expansion whose coefficients are governed by an infinite set of nonlinear equations. Bounds on the total potential energy and the total complementary energy of an RVE do not coincide although they are shown to differ by a term of order O(c4) where c is the fiber volume concentration. Interaction effects due to finite volume concentration, coupled with nonlinear interface characterization, are shown to precipitate instability in composite response. [S0021-8936(00)02104-8]
    keyword(s): Shear (Mechanics) , Boundary-value problems , Cylinders , Displacement , Composite materials , Fibers , Traction AND Stress ,
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      The Fiber Composite With Nonlinear Interface—Part II: Antiplane Shear

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    http://yetl.yabesh.ir/yetl1/handle/yetl/123206
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    contributor authorA. J. Levy
    date accessioned2017-05-09T00:01:38Z
    date available2017-05-09T00:01:38Z
    date copyrightDecember, 2000
    date issued2000
    identifier issn0021-8936
    identifier otherJAMCAV-26501#733_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123206
    description abstractThis paper treats the effective antiplane shear response of a composite consisting of fibers that interact with the matrix through nonlinear Needleman-type cohesive zones. The first paper (Part I) examines effective axial tension response. The composite cylinders representation of a representative volume element (RVE) is employed throughout. For antiplane shear loading the elastic field solution for a single composite cylinder is found in the form of a series expansion whose coefficients are governed by an infinite set of nonlinear equations. Bounds on the total potential energy and the total complementary energy of an RVE do not coincide although they are shown to differ by a term of order O(c4) where c is the fiber volume concentration. Interaction effects due to finite volume concentration, coupled with nonlinear interface characterization, are shown to precipitate instability in composite response. [S0021-8936(00)02104-8]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Fiber Composite With Nonlinear Interface—Part II: Antiplane Shear
    typeJournal Paper
    journal volume67
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.1329320
    journal fristpage733
    journal lastpage739
    identifier eissn1528-9036
    keywordsShear (Mechanics)
    keywordsBoundary-value problems
    keywordsCylinders
    keywordsDisplacement
    keywordsComposite materials
    keywordsFibers
    keywordsTraction AND Stress
    treeJournal of Applied Mechanics:;2000:;volume( 067 ):;issue: 004
    contenttypeFulltext
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