Page 99 - 3D Fibre Reinforced Polymer Composites
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88                  30 Fibre Reinforced Polymer Composites
                        C13 = N ACAV A  + N 'C&V '       c;~ N~C~V~ N'C~V~
                                                                       +
                                                             =
                                     +
                        c; = N~C:V~ N~C:V'                C5,S  =     c55"55"
                                                                         +
                                                                NAVACSSB NBVBC55A
                        C6,S  =     C66AC66B                                       (4.47)
                              NAVAC,,B + NBVBCGGA

                  where N" and NB are the number of micro-blocks A and B within a strip, respectively,
                    and   are the volume fractions of a micro-block A and micro-block B, respectively,
                  Ct. Ct, Ci are the stiffness constants for micro-block A, micro-block B and a strip,
                  respectively.
                     When the micro-blocks are assembled in  the weft or y direction to form the weft
                  stripes,  equations  for  the  average properties  for  a  weft  stripe  can  be  obtained by
                  exchanging 1 and 4 with 2 and 5, respectively, in equation (4.47).
                     The overall effective properties of the unit cell can be calculated by assembling the
                  warp or  weft  stripes via employing the equations for properties of  the  weft or warp
                  stripes, respectively.
                     The 3D model proposed by Tan et al (1997b) can be extended to take into account
                  the fibre undulation by employing a large number of micro-blocks.

                  4.3.4 Applications of Finite Element Methods
                     Finite element methods (EM) have been  used  almost universally during the past
                  forty-five years to  solve very  complex structural engineering problems (Zienkiewicz
                  and  Taylor,  1989). When  applied to  characterise textile composites, FEM visualises
                  them as an assemblage of unit cells interconnected at a discrete number of nodal points.
                  The  unit  cell  is  a periodic  square array of  fibres embedded regularly  in  the  matrix.
                  Hence, if  the force-displacement relationship for an individual unit cell is known, it is
                  possible, by  using various well-known theories and techniques of  elasticity theory, to
                  evaluate its mechanical properties and study the mechanical behaviour of the assembled
                  composite structure.
                     The general procedure to predict the mechanical properties of  a textile composite
                  using FEM consists of  1) dividing the textile composite structure into a number of unit
                  cells  and  analysing  the  mechanical  properties  of  a  unit  cell  using  FEM,  and  2)
                  reconstructing the  entire  reinforcement  geometry  by  assembling the  unit  cells  for
                  predicting mechanical properties of textile composites. Thus, the ability of a FEA model
                  to  predict  mechanical properties  depends upon  the  accuracy of  modelling the  fibre
                  geometry  in  a  unit  cell.  For  the  theoretical  method,  analytical  models  for  elastic
                  properties of composites are generally developed based on classical laminate theory and
                  rule of  mixture. Tan et al. (1997a) provided an overview on  modelling of  mechanical
                  properties of textile composites using the finite element method.
                     Whitcomb  (1989)  analysed  plain  weave  composites  using  3D  finite  element
                  analysis, and studied the effect of tow waviness on the effective moduli, Poisson's ratio
                  and internal strain distributions. It was found that the in-plane moduli decreased almost
                  linearly  with  increasing tow  waviness, which  was  found to create large normal and
                  shear strain concentrations in the composites when subject to a uniaxial loading.
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