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172                               Mechanical Behaviour of  Composites

                       to the volume fraction as follows.

                                                                                     (3.1)

                       where p is the density and the subscripts f and c refer to fibres and composite
                       respectively  .
                         Table 3.3 indicates the extent to which the properties of plastics are influ-
                       enced by the level of fibre content. Full details of the forms in which reinforcing
                       fibres are available for inclusion in plastics are given in Chapter 4.

                                                     Table 3.3
                                  Effect of fibre content on properties of  glass reinforced nylon 66

                                                             Weight fraction, Wf
                       property               0      0.10   0.20   0.30   0.40   0.50   0.60
                       Density                 1140   1210   1280   1370   1460   1570   1700
                       Tensile strength (GN/m2)   0.07   0.09   0.13   0.18   0.21   0.23   0.24
                       96 elongation at break   60   3.5    3.5   3.0    2.5   2.5    1.5
                       Flexural modulus (GN/m2)   2.8   4.2   6.3   9.1   11.2   15.4   19.6
                       Thermal expansion pddC  90   37     32    30     29    25     22
                       Water absorption (24 tu)   1.6   1.1   0.9   0.9   0.6   0.5   0.4


                       3.5  Analysis of Continuous Fibre Composites
                       The greatest improvement in the strength and stiffness of  a plastic is achieved
                       when  it is  reinforced with  uni-directional continuous fibres. The analysis of
                       such systems is relatively straightforward.

                       (i) Longitudinal Properties
                         Consider a composite with continuous aligned fibres as shown in Fig. 3.3.
                       If  the moduli of  the matrix  and fibres are E,  and Ef  respectively then  the
                       modulus of the composite may be determined as follows.

                       Equilibrium Equation
                         The applied force on  the composite will be  shared by  the  fibres and  the
                       matrix. Hence
                                                  F1  = Ff + F,                      (3.2)

                       Geometry of Deformation Equation
                         The strain, E,  is the same in the fibres and matrix and is equal to the strain
                       in the composite.
                                                   E1  = Ef  = Em                    (3.3)
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