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    Characterization of Damage in Triaxial Braided Composites under Tensile Loading

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003
    Author:
    Justin D. Littell
    ,
    Wieslaw K. Binienda
    ,
    Gary D. Roberts
    ,
    Robert K. Goldberg
    DOI: 10.1061/(ASCE)0893-1321(2009)22:3(270)
    Publisher: American Society of Civil Engineers
    Abstract: Carbon fiber composites that utilize flattened, large tow yarns in woven or braided forms are being used in many aerospace applications. The complex fiber architecture and large unit cell size in these materials present challenges for both understanding the deformation process and measuring reliable material properties. In this paper composites made using flattened 12k and 24k (referring to the number of fibers in the fiber tow) standard modulus carbon fiber yarns in a
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      Characterization of Damage in Triaxial Braided Composites under Tensile Loading

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/45168
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    • Journal of Aerospace Engineering

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    contributor authorJustin D. Littell
    contributor authorWieslaw K. Binienda
    contributor authorGary D. Roberts
    contributor authorRobert K. Goldberg
    date accessioned2017-05-08T21:16:27Z
    date available2017-05-08T21:16:27Z
    date copyrightJuly 2009
    date issued2009
    identifier other%28asce%290893-1321%282009%2922%3A3%28270%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45168
    description abstractCarbon fiber composites that utilize flattened, large tow yarns in woven or braided forms are being used in many aerospace applications. The complex fiber architecture and large unit cell size in these materials present challenges for both understanding the deformation process and measuring reliable material properties. In this paper composites made using flattened 12k and 24k (referring to the number of fibers in the fiber tow) standard modulus carbon fiber yarns in a
    publisherAmerican Society of Civil Engineers
    titleCharacterization of Damage in Triaxial Braided Composites under Tensile Loading
    typeJournal Paper
    journal volume22
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2009)22:3(270)
    treeJournal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003
    contenttypeFulltext
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