Page 129 - Mechanics Analysis Composite Materials
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114                 Mechanics and analysis of composite materials
              hybrid  composites, the plies can include fibers of two, or may be more types, e.g.,
              carbon  and  glass, glass  and aramid  and  so on.  Hybrid  composites provide  wider
              possibilities to control material stiffness, strength and cost. A promising application
              of these materials is associated with the so-called thermostable  structures that do
              not change their dimensions under heating or cooling. For some composites, e.g.,
              with glass of boron fibers, longitudinal coefficient of thermal expansion is positive,
              while  for  other  materials,  e.g.,  with  carbon  or  aramid  fibers,  it  is  negative  (see
              Table 7.1 and Section 7.1.2 of Chapter 7). So, the proper combination of fibers with
              positive and negative coefficients can result in material with zero thermal expansion.
                Consider the problem of micromechanics for a unidirectional ply reinforced with
              two types of fibers. Naturally, the stiffness of these fibers should be different, and we
              assume that E:') > E?).  The first-order model of the ply that generalizes the model
              in Fig. 3.34 is presented in Fig. 3.66. For tension in the fiber direction, the apparent
              stress and strain, 01  and E', are linked by Hooke's  law




              in which the effective modulus is specified by the following equation generalizing
              Eq. (3.76)

                  El  = E~l)u~')+E,(2)  (2) +Emu,  .                           (3.125)

              Here, v!')  and up) are volume fractions of the fibers of the first and of the second
              type and om is the matrix volume fraction, so that




              We also introduce the total volume fraction of the fibers




              and normalized volume fractions of fibers as

















                       Fig. 3.66.  A first-order microstructural model  of a hybrid unidirectional ply.
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