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174                               Mechanical Behaviour of Composites

                        are known to be 2540 kg/m3 and 1300 kg/m3, calculate the weight fraction of
                        fibres in the composite.

                          Solution From the rule of mixtures
                                        ~c  = PfVf + Pmvm = PfVf + Pm(l-  Vf)
                                      1950 = 2540Vf + 1300(1 - Vf)

                                       Vf = 0.52
                                                Pf      2540
                        Using equation (3.1). Wf = -Vf  = -(0.52)   = 0.68
                                                 PC     1950
                          Example 3.2 PEEK is to be  reinforced with  30% by  volume of  unidirec-
                        tional  carbon fibres and the properties of  the individual materials are given
                        below. Calculate the  density, modulus and  strength of  the composite in  the
                        fibre direction.

                                               Density         Tensile strength     Modulus
                        Material               (kdm3)            (GN/m*)            (GN/m*)

                        PEEK                    1300              0.0d                3.8
                        Carbon fibre (HM)       1800              2.1               400

                           Note that as shown below, this must be the matrix stress at the fibre fracture strain.
                          Solution From the rule of mixtures

                               ~c  = PfVf + PmVm  = 0.13(1800) + 0.7(1300) = 1450 kg/m3
                                  = CfuVf + CmVm = 0.3(2.1) + 0.7(0.058) = 0.67 GN/m2
                              E,L = EfVf + EmVm  = 0.3(400) + 0.7(3.8) = 122.7 GN/m2

                          Example 3.3 Calculate the fraction of the applied force which will be taken
                        by the fibres in the composite referred to in Example 3.2

                          Solution From  equations (3.2), (3.3)  and  (3.4), the  force in  the  fibres is
                        given by
                                              Ff = UfAf = Ef &f Vf vC
                          Similarly the force in the composite is given by

                                            F1  = EfEfVfVc + EmCmVmVc

                          Hence.
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