Page 107 - 3D Fibre Reinforced Polymer Composites
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96                  30 Fibre Reinforced Polymer Composites



                                          c33  1

                 c,3s =c33                       ,  C22  =NAC22AVA+NBC2FVB,



                 C,,S  = c                                     C33AC33B
                                                         NAVAC,B + NBVBC3;  ’


                 c,s  =       CMACMB               c,,s  =     C,5AC,5B
                       NAVACUB  + NBVBCMA ’              NAVAC,B + NBVBC,,A ’






                 It is worth pointing out that the principal axes of material block A and B are assumed to
                 coincide with the Cartesian coordinates,  x, y and z, for all the three assemblage schemes
                 shown in Figure 4.17.
                    As  shown in Figure 4.16,  the  woven fabrics unit  cell is  divided into four  cubic
                 blocks (see Figures 4.16(a)-(d)).  The elastic constants for the blocks in Figure 4.16(a),
                 (b)  and  (c)  can  be  evaluated  using  the  “X  assembly”  equations  and  the  stiffness
                 constants for yarns and resin.  The stiffness constants for the combined block (a) and (b)
                 and  the combined  block  (c) and  (d) can be  further evaluated using the  Y  assembly
                 equations.  The overall properties are finally obtained using the z assembly formula.
                 This was referred to as the XYZ model by Tan et al. (1998, 1999a, 199b) as assemblage
                 of micro blocks follow the sequence in x, y and z direction respectively. Similarly, three
                 other models were developed following the similar concepts and  were referred to as
                 “YXZ model”, “ZXY and ZYX models.
                    A laminate model was also proposed by  Tan et a1 (1998) to take into account the
                 contribution of the z yarn on the upper and lower surfaces of the 3D orthogonal woven
                 composite material as shown in Figure 4.13.


                 4.4.3 Applications of Finite Element Methods
                 Finite element methods  (EM) have  also been  widely  used  to  model  characteristic
                 behaviours of  3D textile composites (see Tan et al.,  1997).  FEM is a powerful and
                 versatile  numerical  tool  that  allows  detailed  modelling  of  complex  geometry  and
                 various  material  properties.  Current  research  focuses on  practical  applications of
                 existing  elements  and  solution  schemes  in  commercially  available  software  to
                 modelling of 3D composite materials of various constituents. There exists limited work
                 on formulation and development of  particular elements and solution schemes that are
                 specifically formulated and implemented for analysis of 3D composite materials.  Thus
                 we  will briefly describe the modelling concepts and  methods that are currently being
                 widely used by researchers in both materials and mechanics communities.
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