Page 139 - Engineered Interfaces in Fiber Reinforced Composites
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122               Engineered interfaces in .fiber reinforced composites





                                  g  150
                                  e!
                                 -
                                 c
                                  rn
                                  3   100
                                  &
                                     50


                                      0
                                        0       100     200      300      4
                                 (4          Normalized axial distance, z/a

















                                                100     200      300      4
                                  (b)         Normalized axial distance, z/a
                    Fig. 4.17. Distribution of (a) normalized fiber axial stress, .;/a,  and (b) normalized interface shear stress,
                    q/u, along  the  fiber  axis,  z/a, at  a  given  applied  stress  for  different  residual  clamping  stresses
                                     qa = -7,  -10  and -13  MPa. After Kim et al. (1993b).


                    Taking the  approximate values  for the  non-dimensional  coefficients given  in  Eq.
                    (4.80), the solution for the mean fiber fragment length, 2L, is given in a closed form
                    equation







                    The mean fiber fragment length, 2L, is plotted as a function of the applied strain, E,
                    in Fig. 4.18. Similar to the results for the fully bonded interface model shown in Fig.
                    4.12, the  full frictional interface  model  predicts  that  (2L) decreases sharply  with
                    increasing  applied  strain  within  a short  range  of c.  A  high  fiber  tensile strength
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