Volume 22, Issue 1 (October 2000)

    Failure Initiation in Translaminar Reinforced Composites


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    A translaminar-reinforced (TLR) composite is an otherwise two-dimensional laminate with through-thickness or Z-direction fibrous reinforcement across the lamina. Only small amounts (less than 5% volume) of TLR are necessary to substantially improve compression-after-impact response, increase fracture toughness, and severely restrict the size and growth of delamination. These improvements have been documented repeatedly in the literature, and it is generally accepted that TLR restricts the size and growth of delamination. In this paper we report a detailed investigation of whether TLR delays the initiation of delamination via finite-element analysis and a strength-of-materials approach. The various parameters investigated include TLR material, diameter, spacing, volume fraction, and through-thickness angle. In addition, the unavoidable microstructural features of curved in-plane fibers and resin pockets were examined. Our conclusion is that TLR does not delay damage initiation, even though it has been shown experimentally to restrict damage progression.

    Author Information:

    Farley, GL
    Army Research Laboratory, Vehicle Structures Directorate, NASA-LaRC, Hampton, VA

    Dickinson, LC
    3TEX, Inc., Cary, NC

    Hinders, MK
    College of William and Mary, Williamsburg, VA

    Stock #: CTR10621J

    ISSN: 0884-6804

    DOI: 10.1520/CTR10621J

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    Title Failure Initiation in Translaminar Reinforced Composites
    Symposium , 0000-00-00
    Committee D30