Page 236 - Plastics Engineering
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Mechanical Behaviour of  Composites                            219

                   If  the diameter of the bottle is 160 mm, calculate the hoop and axial strains
                 in the bottle wall when an internal pressure of 200 kN/m2 is applied. Calculate
                 also the stresses in the individual layers.
                   Solution Although the composite wall  is  curved, the  (r/h) value  is  large
                 and so it can be  analysed using the method illustrated for laminates. In  this
                case, each ply  is isotropic and so the properties do not vary with 6. It is thus
                 necessary to get Q for each ply relative to the centre line of the wall thickness

                         h~ = 0.6,  hl  = -0.2,   h2  =O,  h3 =0.2,   h4 = 0.6
                 ie the wall section is treated as if  it has four plies
                               [material A (0.4 mm)/material B (0.2 mm)],

                 Also
                                            pr   0.2 x 80
                            hoop stress, cy = - =        = 13.33 MN/m2
                                            h       1.2
                 (or N, = cyh = 16 N/mm)
                                            pr    0.2 x  80
                             axial stress, a,  = - =      = 6.67 MN/m2
                                            2h    2 x  1.2
                 (or NR = a~h = 8 N/mm)
                         -    [3,mOx io3  1.244  103        0
                            =  1.244 x  io3  3.444 x  io3   0     1  N/mm2,
                                                  ]
                         -  [ 956.5  376.7  ;           1.103 x  lo3
                                                0
                         Q2 =  376.7  956.5         N/I-M12
                                 0      0    285.8
                 Also,
                                                and
                 Then the Extensional Stiffness Matrix is given by
                               4
                          A =     ef(hf  - hf-,),   u = A-'  (since [BI = 0).
                              f =1
                 The strains are related to the forces (or stresses) by
                                          [;!yl       Nx




                 Therefore the axial and hoop strains are
                           Ex  = 7.932          Ey = 4.809   10-~(~,, = 01
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