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    A Micro-Mechanics Model for In-Situ Compression Strength of Fiber Composite Laminates

    Source: Journal of Engineering Materials and Technology:;1992:;volume( 114 ):;issue: 001::page 8
    Author:
    S. R. Swanson
    DOI: 10.1115/1.2904147
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compression failure in fiber composites is of much interest, and is often a limiting factor in applications because of the lower compressive strength relative to tensile strength. In the present work a model for compression failure of fiber composite laminates is developed. This model is based on the assumption of fiber microbuckling similar to other models in the literature, but in addition includes the support offered by the plies in the overall laminate that are adjacent to the critical axial plies. The result is that the apparent strength of the axial plies depends on the total laminate layup. The model predictions are seen to be in reasonable agreement with recent experimental data. Initial fiber waviness is included and seen to be a dominant factor in the results.
    keyword(s): Composite materials , Fibers , Laminates , Micromechanics (Engineering) , Compressive strength , Compression , Failure AND Tensile strength ,
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      A Micro-Mechanics Model for In-Situ Compression Strength of Fiber Composite Laminates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/110348
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    contributor authorS. R. Swanson
    date accessioned2017-05-08T23:38:36Z
    date available2017-05-08T23:38:36Z
    date copyrightJanuary, 1992
    date issued1992
    identifier issn0094-4289
    identifier otherJEMTA8-26946#8_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110348
    description abstractCompression failure in fiber composites is of much interest, and is often a limiting factor in applications because of the lower compressive strength relative to tensile strength. In the present work a model for compression failure of fiber composite laminates is developed. This model is based on the assumption of fiber microbuckling similar to other models in the literature, but in addition includes the support offered by the plies in the overall laminate that are adjacent to the critical axial plies. The result is that the apparent strength of the axial plies depends on the total laminate layup. The model predictions are seen to be in reasonable agreement with recent experimental data. Initial fiber waviness is included and seen to be a dominant factor in the results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Micro-Mechanics Model for In-Situ Compression Strength of Fiber Composite Laminates
    typeJournal Paper
    journal volume114
    journal issue1
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2904147
    journal fristpage8
    journal lastpage12
    identifier eissn1528-8889
    keywordsComposite materials
    keywordsFibers
    keywordsLaminates
    keywordsMicromechanics (Engineering)
    keywordsCompressive strength
    keywordsCompression
    keywordsFailure AND Tensile strength
    treeJournal of Engineering Materials and Technology:;1992:;volume( 114 ):;issue: 001
    contenttypeFulltext
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