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    On the Logarithmic Singularity of Free-Edge Stress in Laminated Composites Under Uniform Extension

    Source: Journal of Applied Mechanics:;1982:;volume( 049 ):;issue: 003::page 561
    Author:
    R. I. Zwiers
    ,
    T. C. T. Ting
    ,
    R. L. Spilker
    DOI: 10.1115/1.3162526
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The stress singularities at the free edge of an interface between adjacent layers in a laminated composite are studied. Each layer of the composite is assumed to be of the same orthotropic material with one of the principal axes being the fiber direction. The angle θ, however, which is the fiber orientation, varies from layer to layer. The composite is subjected to uniform extension in the plane of the layers. At the interface between adjacent layers having fiber angles (0/90), (θ/θ′ ), and a family of special combinations of (θ/θ′ ) shown in the paper, the singularity of the type k*rδ (δ<0), seems to be the only possibility. For an interface with other combinations of fiber orientations in the the adjacent layers, it is shown that an additional singularity of the form k(ln r) exists. Since the constant k* depends on the stacking sequence of the layers and the complete boundary conditions, and may vanish in some cases, the existence of a k*rδ singularity at a free edge is not certain until a complete problem is solved. In contrast, the constant k, which is called the logarithmic stress-intensity factor, is independent of the stacking sequence of the layers and the complete boundary conditions. Its value is determined once the fiber orientations on both sides of the interface are known. Therefore, at the interface between adjacent layers for which k≠0, the free-edge stress is inherently singular. Moreover, the singularity is logarithmic.
    keyword(s): Composite materials , Stress , Fibers , Boundary-value problems AND Stress singularity ,
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      On the Logarithmic Singularity of Free-Edge Stress in Laminated Composites Under Uniform Extension

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    contributor authorR. I. Zwiers
    contributor authorT. C. T. Ting
    contributor authorR. L. Spilker
    date accessioned2017-05-08T23:12:27Z
    date available2017-05-08T23:12:27Z
    date copyrightSeptember, 1982
    date issued1982
    identifier issn0021-8936
    identifier otherJAMCAV-26204#561_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95340
    description abstractThe stress singularities at the free edge of an interface between adjacent layers in a laminated composite are studied. Each layer of the composite is assumed to be of the same orthotropic material with one of the principal axes being the fiber direction. The angle θ, however, which is the fiber orientation, varies from layer to layer. The composite is subjected to uniform extension in the plane of the layers. At the interface between adjacent layers having fiber angles (0/90), (θ/θ′ ), and a family of special combinations of (θ/θ′ ) shown in the paper, the singularity of the type k*rδ (δ<0), seems to be the only possibility. For an interface with other combinations of fiber orientations in the the adjacent layers, it is shown that an additional singularity of the form k(ln r) exists. Since the constant k* depends on the stacking sequence of the layers and the complete boundary conditions, and may vanish in some cases, the existence of a k*rδ singularity at a free edge is not certain until a complete problem is solved. In contrast, the constant k, which is called the logarithmic stress-intensity factor, is independent of the stacking sequence of the layers and the complete boundary conditions. Its value is determined once the fiber orientations on both sides of the interface are known. Therefore, at the interface between adjacent layers for which k≠0, the free-edge stress is inherently singular. Moreover, the singularity is logarithmic.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Logarithmic Singularity of Free-Edge Stress in Laminated Composites Under Uniform Extension
    typeJournal Paper
    journal volume49
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3162526
    journal fristpage561
    journal lastpage569
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsStress
    keywordsFibers
    keywordsBoundary-value problems AND Stress singularity
    treeJournal of Applied Mechanics:;1982:;volume( 049 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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