Journal of the Japan Society for Composite Materials
Online ISSN : 1884-8559
Print ISSN : 0385-2563
ISSN-L : 0385-2563
Volume 34, Issue 5
Displaying 1-2 of 2 articles from this issue
Research paper
  • Kazumasa KAWABE, Hideki SASAYAMA, Kazuro KAGEYAMA, Nobuo OGATA
    2008Volume 34Issue 5 Pages 173-181
    Published: 2008
    Released on J-STAGE: June 21, 2010
    JOURNAL FREE ACCESS
    A new fiber spreading technology (FUKUI method) to obtain the continuously wide and thin reinforcing fiber tow was developed. Thin prepreg sheet less than 0.05 mm in thickness can be prepared by using this method. In the previous study, the tensile tests were conducted on the Carbon/Epoxy quasi-isotropic laminates which were composed of stacking these prepreg sheets. As a result, the thin-ply effect was found, that is, the initial failure stress increases with decreasing ply thickness. This effect was previously predicted by Kageyama et al. In this work, the thin-ply effects on the compressive properties have been studied. As a result, the thin-ply effect was found not only in tensile tests but also in compression tests. This result implies that the design strength of composites can be improved by the use of thin prepreg sheets. In other words, this result means that the weight saving and reliability can be achieved using thin prepreg sheets as a composite materials.
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  • Akinori YOSHIMURA, Tomoaki NAKAO, Nobuo TAKEDA
    2008Volume 34Issue 5 Pages 182-188
    Published: 2008
    Released on J-STAGE: June 21, 2010
    JOURNAL FREE ACCESS
    The present study investigated the improvement of low-velocity impact damage resistance of CFRP laminates due to the through-the-thickness stitching experimentally and numerically. First, we conducted drop-weight impact tests for stitched and unstitched laminates. The results of damage inspection confirmed that stitching did improve the impact damage resistance, and revealed that the improvement effect became greater as the impact energy increased. Moreover, the stitching affected the through-the-thickness damage distribution. Then we performed FEM analysis and calculated the energy release rate of the delamination by using Virtual Crack Closure Technique (VCCT). The numerical results revealed that the stitching affected the through-the-thickness damage distribution because the stitch threads particularly decreased the mode I energy release rate around the bottom of the laminate. Comparison of the results of models which contain delamination of various size revealed that the energy release rate became smaller as delamination size increased, therefore the stitching improved the impact resistance more effectively when the impact energy was larger.
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