Page 341 - Fiber Fracture
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FRACTURE OF NATURAL POLYMERIC FIBRES                                 323



















                  Fig. 10. The geometry referred to in the derivation of Eq. 6, pertaining to cylindrical fibres.

               lc''r lX'"                                                        (5)
            this distance:
                        $
                   do
                      =
                               &
              Explicit integration of Eq. 5, followed by rearrangement, leads to:


               So xuf is an increasing function of  r: an increased fibre thickness will increase the
            capacity of the interfacial surface area to transfer load to the fibre (in proportion to r),
            but will also (and even more effectively) increase the capacity of the fibre cross-section
            to carry that load (in proportion to r2).
               It follows that much of the material in the fibre is wasted, in that the tensile strength
            is not being properly exploited along almost the whole length of the fibre! This problem
            is exacerbated in thicker fibres. The load near the ends of the fibres could be carried
            adequately by  a thinner fibre cross-section, compared to the load near the middle of
            fibres. A less wasteful use of  material, and  a  more efficient exploitation of  the fibre
            properties, would  therefore be achieved if  the  fibres were to  taper from  the  middle
            towards the ends. Also, regions of the fibre having a smaller cross-section would then be
            able to undergo a larger elastic deformation, thus matching more closely the deformation
            of  the matrix; therefore, the shear stress concentration in the matrix near the fibre ends
            would be reduced. These gains have been recognised and discussed qualitatively in the
            context of sea cucumber and sea urchin collagen fibres, which are appropriately tapered
            (Trotter and Koob, 1989; Trottcr ct a]., 1994,2000b).
               It is instructive to consider how the force balance in Eq. 3 and the critical half-length
            (transfer distance) of  the fibres in  Eq.  6 are  affected by  allowing the fibres to  taper
            towards their ends. Reference should be made to Fig.  11, which  again considers the
            shear stress acting on a small length dx near the end of a fibre. The tensile stress in the
            fibre again increases by do over this distance, and the fibre radius increases by dr. From
            the geometry of Fig. 1 1,
               dr
               -dx  = tan&    i.e.  r = xtane                                    (7)
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