Page 263 - Engineered Interfaces in Fiber Reinforced Composites
P. 263

244               Engineered interfaces in fiber  reinforced composites

                    debonding frictional work. The pull-out energy (Cottrell,  1964; Kelly, 1970) is the
                    work done against sliding friction in extracting the broken fiber. Based on the work
                    done by the frictional shear stress, zf which is assumed to be constant over a pull-out
                    distance, e,,,  the fiber pull-out toughness, R,,,  is given by





                    Since fiber pull-out length, e,,,  is difficult to measure with any accuracy from the
                    fracture surface of composite specimens containing high &, R,,  is often expressed in
                    terms of the inherent properties of the composite constituents. There are three cases
                    considered here depending on the fiber length relative to the critical transfer length.
                      (i)  If  the  fiber  length  is  less  than  the  critical  transfer  length,  e < e,,  all  the
                    debonded fibers are pulled out. Assuming the pull-out length, epo, varies between 0
                    and el2 with a mean value of &/4 (Kelly and Tyson, 1965; Cooper and Kelly, 1969),
                    R,,  becomes





                      (ii) R,,  is maximum when e = e,,






                    In Eq. (6.8) an upper bound estimate of zf is made by the apparent bond strength z,
                    for the critical transfer length, i.e., e,  x  ord/2zf, based  on the early work  of  Kelly
                    and  Tyson  (1965).  Therefore,  R,,  is  shown  directly  proportional  to  the  critical
                    transfer  length.
                      (iii) If the composite contains fibers of lengths greater than the critical transfer
                    length, e > e,, then the fraction of fibers that can be pulled out is &/C  on the basis of
                    normal probability, and e,,  ranges from 0 to &/2. Thus, R,,  becomes





                    Graphical presentation of Eqs. (6.7H6.9) are given in Fig. 6.2 where the fiber pull-
                    out toughness, R,,  is plotted as a function of fiber length, e. It is worth noting that
                    for most polymer matrix composites reinforced with carbon, glass and aramid fibers,
                    the  estimated  fiber pull-out  toughness  values  are approximately  the  same as the
                    measured  composite fracture  toughness  (Harris  et  al.,  1971,  1975; Atkins,  1975;
                    Gershon and Marom,  1975; Kim and Mai,  1991a, b).
   258   259   260   261   262   263   264   265   266   267   268