Page 202 - 3D Fibre Reinforced Polymer Composites
P. 202

Stitched Composites                        191
            The  toughening mechanisms responsible for  the  high  mode  I1 interlaminar  fracture
            toughness of stitched composites are complex, with a number of different mechanisms
            operating along the length of a delamination crack.  The shear tractions generated in
            stitches with  increasing sliding displacement between  the  opposing crack  faces  are
            shown in Figure 8.26.  This figure by Cox (1999) shows typical sliding displacement
            and  stress levels associated  with  the  various mechanisms during shear loading of  a
            stitched composite up  to  the  point  of  failure.  The  sliding displacement (2~1) is  the
            distance the two crack faces have separated under mode I1 loading.  The vertical scales
            show  the  average bridging traction  across the  stitches,  q,.  (left-hand  side)  and  the
            bridging traction for a single stitch, T (right-hand side).  The values shown for q, are
            representative, and  will  vary  depending on  the  volume fraction of  stitching and  the
            mechanical properties of the threads.




                                          ploughing, debonding, and slip
                                       /

















                                     0               -1
                                      sliding displacement, 2u (mm)



            Figure 8.26  Schematic of  the  shear tractions for  mode I1  loading of  a  stitch  under
            increasing crack sliding distance (from Cox, 1999).


            It  is  generally acknowledged that  when  an  interlaminar shear stress is  applied to  a
            stitched composite containing a delamination then the stitches ahead of the crack front
            are not damaged or deformed.  When the crack tip reaches the stitches, however, the
            delamination causes the stitches to debond from the surrounding composite material.
            The stitches are usually completely debonded from the composite when the total sliding
            displacement  (2~~) exceeds about 0.2 mm. As the opposing crack faces continue to slide
            pass each other the stitches become permanently deformed.  Plastic deformation of the
            stitches can occur immediately behind the crack tip due to the low shear yield stress of
            the thread material.  It is estimated that permanent deformation in stitches begins when
            the  sliding displacement distance exceeds about  0.1  mm.  The  stitches experience
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