Page 146 - Engineered Interfaces in Fiber Reinforced Composites
P. 146

Chapter 4.  Micromechanics of  stress transfer   129
                1992b). The external stress,  0, is represented  by  00, o:, 0;  and ufr for (frictionless)
                initial  debond  stress,  partial  debond  stress,  maximum  debond  stress  and  initial
                frictional pull-out stress after complete debonding, respectively, at different stages of
                the fiber pull-out process. A typical fiber pull-out stress-displacement  ((r-6)  diagram
                along with these characteristic external stresses is schematically shown in  Fig. 3.7.
                  For  the  cylindrical  coordinates  (Y, 0,z)  in  the  fiber  pull-out  test,  the  basic
                governing  equations  and  the  mechanical  equilibrium  conditions  between  the
                composite constituents are essentially the same as those given in  Section 4.2.3, i.e.
                Eqs.  (4.8)-(4.18).  The  only  exception  is  the  equilibrium  condition  between  the
                external stress and the axial stresses in the fiber and the matrix given by  Eq. (4.1 I),
                which has to be modified to
                              1
                   cr = $(z) +  dm (z) .                                          (4.87)
                              I
                Therefore,  in  a  procedure  similar  to  that  used  in  the  fiber  fragmentation  test,
                combining Eqs. (4. lo), (4.17), (4.1 8), and  (4.87) yields a  second-order differential
                equation for the FAS

                                                                                  (4.88)


                where the coefficients A, and A2  are given in Eqs. (4.20) and (4.21). The solution of
                the FAS is subjected to the following boundary  conditions:

                   of([)   = (TI = cr - w(i7 - cr)[exp(At) - 11,   $(z)  = o  .   (4.89)

                FS~ is the crack tip debond stress at the boundary between the bonded and debonded
                regions at z = e,  as defined in Section 4.2.3. It should be noted,  however, that the
                actual values of (rt are different for different specimen geometry even for an identical
                debond length,  C.  Therefore, the solutions of  FAS, and the corresponding  MAS,
                MSS and IFSS are obtained for the bonded region  (CGzGL):

                           [i 2 atop] sinh [ fi(L -z)] - 2 cr sinh [~(Gz)]
                                                    y
                    4(z) =               sinh[fi(L  - e)]              -"%a.      (4.90)

                              b??(r+  (rp]  sinh[fi(L  -z)]  - y2asinh[fi(e  -z)]
                    d,(Z) = -1'
                                             sinh [a(L - e)]
                               2A2                                                (4.91)
                             +?/ -0,
                                 [ y 2 cr + CT~] cosh [ fi(L - z)] - y 2 CJ cash [a([
                                A1
                                                                             z)]
                                                                           -
                      zm (r, 2) = y
                                                sinh [a(L - C)]
                                                                                  (4.92)
   141   142   143   144   145   146   147   148   149   150   151