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    Computationally Efficient Micromechanical Models for Woven Fabric Composite Elastic Moduli

    Source: Journal of Applied Mechanics:;2001:;volume( 068 ):;issue: 004::page 553
    Author:
    R. Tanov
    ,
    Graduate Research Assistant
    ,
    A. Tabiei
    ,
    Assistant Professor and Director
    DOI: 10.1115/1.1357516
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents two newly developed micromechanical models for the analysis of plain weave fabric composites. Both models utilize the representative volume cell approach. The representative unit volume of the woven lamina is divided into subcells of homogeneous material. Starting with the average strains in the representative volume cell and based on continuity requirements at the subcell interfaces, the strains and stresses in the composite fiber yarns and matrix are determined as well as the average stresses in the lamina. Equivalent homogenized material properties are also determined. In their formulation the developed micromechanical models take into consideration all components of the three-dimensional strain and stress tensors. The performance of both models is assessed through comparison with available results from other numerical, analytical, and experimental approaches for composite laminae homogenization. The very good accuracy together with the simplicity of formulation makes these models attractive for the finite element analysis of composite laminates.
    keyword(s): Yarns , Stress , Warping , Composite materials , Textiles , Geometry , Fibers , Elastic moduli , Finite element analysis AND Tensors ,
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      Computationally Efficient Micromechanical Models for Woven Fabric Composite Elastic Moduli

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/124674
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    • Journal of Applied Mechanics

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    contributor authorR. Tanov
    contributor authorGraduate Research Assistant
    contributor authorA. Tabiei
    contributor authorAssistant Professor and Director
    date accessioned2017-05-09T00:03:59Z
    date available2017-05-09T00:03:59Z
    date copyrightJuly, 2001
    date issued2001
    identifier issn0021-8936
    identifier otherJAMCAV-26518#553_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124674
    description abstractThis paper presents two newly developed micromechanical models for the analysis of plain weave fabric composites. Both models utilize the representative volume cell approach. The representative unit volume of the woven lamina is divided into subcells of homogeneous material. Starting with the average strains in the representative volume cell and based on continuity requirements at the subcell interfaces, the strains and stresses in the composite fiber yarns and matrix are determined as well as the average stresses in the lamina. Equivalent homogenized material properties are also determined. In their formulation the developed micromechanical models take into consideration all components of the three-dimensional strain and stress tensors. The performance of both models is assessed through comparison with available results from other numerical, analytical, and experimental approaches for composite laminae homogenization. The very good accuracy together with the simplicity of formulation makes these models attractive for the finite element analysis of composite laminates.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComputationally Efficient Micromechanical Models for Woven Fabric Composite Elastic Moduli
    typeJournal Paper
    journal volume68
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.1357516
    journal fristpage553
    journal lastpage560
    identifier eissn1528-9036
    keywordsYarns
    keywordsStress
    keywordsWarping
    keywordsComposite materials
    keywordsTextiles
    keywordsGeometry
    keywordsFibers
    keywordsElastic moduli
    keywordsFinite element analysis AND Tensors
    treeJournal of Applied Mechanics:;2001:;volume( 068 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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