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118                   30 Fibre Reinforced Polymer Composites
                  orthogonal  woven  CFRP  (as shown  in  Figure 5.6) and  a  3D  orthogonal woven E-
                  glasdepoxy composite.   Figure 5.12 shows micrographs of  the fiacture surface for
                  specimens loaded in the stuffer yam and filler direction, respectively.  The breakage of
                  z-binders shown in Figures 5.12(a) and (b) indicate that stuffer yams break at a cross
                  section between two adjacent six filler yams.  The separation of a z-binder shown in
                  Figures 5.12(c) and (d) clearly indicates that filler yarns break at a cross section along a
                  z-binder  .











                                        0
                                        0
                       -      t         b          0
                       .-
                       a,
                                                   W
                       E  0.75                      a                       0
                       ?                9,
                                       3D Interlock CarbonEpoxy (Ding et al., 1993)
                                       3D Orthogonal Glass/Epoxy (Arendts et al., 1989)
                                       30 Interlock GlasdEpoxy (Arendts et al., 1989)
                                       3D Orthogonal GlassNinyl Ester (Lee et al., 2002)
                                    A  3D Interlock Kevlar/Epxy (Guess and Reedy, 1985)
                          0.00   '   I   '   I   '   I   "
                                                      '
                              0    2    4    6     8    10   12   14   16    18   20
                                              Z-Binder Content (%)
                  Figure 5.11 Plot of normalised tensile strength against z-binder content for various 3D
                  woven composites.



                  Table  5.3  presents  a  comparison between  the  experimental and  predicted  in-plane
                  tensile strengths in both the stuffer and filler yam directions.  The subscript 1 and 2
                  refer to the stuffer and  filler yarn direction respectively.  The predicted results are
                  obtained  by  using  the  rule  of  mixture  method  and  the  laminate block  models  in
                  conjunction with maximum stress criterion.  Both analytical method and finite element
                  method are employed in the block laminate model.  It is noted that there exists a good
                  correlation between  the  predicted  and  measured tensile strength in  the  stuffer yarn
                  direction.  However, there is a large difference between the predicted and measured
                  tensile strength in the filler yam direction.  This is due to the misalignment in the filler
                  yam direction as shown in Figure 5.6(b).  Although the filler yam is 20% more than the
                  stuffer yarn, the average tensile strength in the filler yarn direction is only slightly larger
                  than that in the stuffer yarn direction.  The misalignment of filler yarns is shown in
                  Figure 5.6(b) and  is believed  to be  the  major  contributing factor to  the low tensile
                  strength in the filler yarn direction.
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