Page 209 - 3D Fibre Reinforced Polymer Composites
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198                 30 Fibre Reinforced Polymer Composites

                 The ability of  stitching to reduce the amount of  damage improves not only with  the
                 incident impact energy.  The effectiveness of stitching also improves dramatically with
                 stitching density, as shown in Figure 8.32 (Liu  1990).  In the figure the normalised
                 delamination area  defines the  amount of  impact  damage to  the  stitched composite
                 divided by the amount of damage to the equivalent unstitched laminate.  There is a rapid
                 reduction to the amount of  impact damage with increasing stitch density, and in this
                 case it is seen that stitching reduced the delamination area by as much as 40% compared
                 with the unstitched laminate.















                            0.4 -


                            0.2 -


                            0.0       l  .   I  ,  I   .  l  ,  I   ,  l  ,   I
                              0.0    0.5    1.0   1.5    2.0    2.5   3.0    3.5
                                               Stitch Density (crn-*)

                 Figure 8.32 Effect of stitch density on the amount of impact damage to a glass/epoxy
                 composite. The composite was  impacted at an energy of  about 7.5  Jlmm  (Data from
                 Liu, 1990).


                 The improved damage resistance provides stitched composites with higher post-impact
                 mechanical properties than the unstitched material.  For example, Figure 8.33 (Rossi,
                 1989) compares the  compression-after-impact strengths of  a  stitched and  unstitched
                 carbodthermoplastic composite.  It is seen the compression-after-impact strength of the
                 stitched composite is slightly higher.  The higher post-impact strength is attributed to
                 two  factors:  firstly,  the  amount  of  delamination  damage  in  lower  in  the  stitched
                 material, and secondly, the stitches suppress the growth of the delaminations and inhibit
                 sublaminate buckling under compression loading.
                    Models for estimating the compression-after-impact strength of stitched composites
                 have not  yet been  formulated because of  the complexity of  modeling the growth of
                 multiple delaminations and the subsequent multiple sublaminate buckling processes that
                 can occur under compression.  However, models have been developed for predicting the
                 compression strength of  stitched laminates containing a single delamination (Shu and
                 Mai, 1993a, 1993b). These models provide insights into the effectiveness  of stitching in
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