Page 102 - Mechanics Analysis Composite Materials
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Chapter 3.  Mechanics of  a unidirectional p1.v   87

              Only two of the foregoing expressions, namely Eq. (3.76) for E, and Eq. (3.80)
            for vz1, both following from the rule of mixtures, demonstrate good agreement with
            experimental  results.  Moreover,  expressions  analogous  to  Eqs. (3.76) and  (3.80)
            follow practically  from  all  numerous studies based  on  different micromechanical
            models.  Comparison  of  predicted  and  experimental  results  is  presented  in
            Figs. 3.35-3.37,  where theoretical  dependencies of normalized  moduli on the fiber
            volume fraction  are shown with lines. The circles correspond  to the test  data for
            epoxy composites reinforced with different fibers that were obtained by the authors
            or taken  from publications  of  Tarnopol'skii  and Roze  (1969),  Kondo  and  Aoki
            (1982), Lee et al.  (1995).  As can be seen in Fig. 3.35, not only first-order  model,
            Eq. (3.76), but zero-order model, Eqs. (3.61), as well, provide fair prediction for E,,
            while Figs. 3.36 and 3.37 for E2  and Gl2 call for the improvement of the first-order
            model (the corresponding results are shown with solid lines).
              Second-order models allow for the fiber shape and distribution, but in contrast to
            higher-order models ignore complicated stressed state of fibers and matrix under the
            ply loading shown in Fig. 3.29. To demonstrate this approach, consider a layer-wise
            fiber distribution  (see Fig.  3.5) and assume that the fibers are absolutely rigid and
            the matrix  is in  the simplest uniaxial  stressed state under  transverse  tension. The
            typical element of this model  is shown in Fig. 3.38 from which we can obtain  the
            following equation

                   nR2  nR
               q=-=-.                                                         (3.82)
                   2Ra   2a
            Because 2R  < a, vf < n/4 = 0.785. Equilibrium condition yields
                        R
               2R02 = / crndx3 ,                                              (3.83)
                      -R
            where x3 =Rcosa and  02 is some average  transverse  stress that induces  average
            strain




                                  0.8
                                  0.6

                                  0.4

                                  0.2

                                   0
                                    0    0.2   0.4   0.6   0.8
            Fig. 3.35.  Dependence of the normalized longitudinal modulus on fiber volume fraction: (- -- -)  zero-
                 order model, Eqs. (3.61); (-)  first-order model, Eqs. (3.76); (*) experimental data.
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