Page 108 - 3D Fibre Reinforced Polymer Composites
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Micromechanics Models for Mechanical Properties       97
            Similar to unidirectional prepreg, woven composites have fibres or fibre tows embedded
            in  resin  matrix  in  specific  patterns,  which  can  be  different  depending  on  the
            manufacturing  procedure used  and  the  selected  processing  parameters.  The  basic
            constituents are  fibre  and  resin,  which  can  be  treated  as  being  homogeneous  and
            orthotropic.  However,  finite  element  modelling  of  each  individual  fibre  and  its
            interaction  with  resin and  adjacent fibres in  3D composite materials makes the task
            extremely  expensive  and  difficult,  if  not  impossible,  and  even  unnecessary  for
            evaluating macroscopic properties  of  the  materials.  This  is  a  natural  and  intrinsic
            modelling level without any assumptions or  with limited assumptions with respect to
            fibre paths only.
               The next possible modelling level is to treat the fibre tows or bundles as a whole
            large  ‘fibre’ or  yarn, in  which  all  fibres are  aligned or closely aligned  following a
            specific pattern.  In this model, a number of assumptions must be introduced to define
            the geometry and material properties of each yam.  The definition of the yarn geometry
            can include the cross sectional shape and size of the yarn, path of the centreline of the
            yam, and fibre distribution across the cross-section of the yarn.  As all fibres in a yarn
            are aligned or closely aligned in one direction at a cross-section, the material properties
            of a unidirectional composite can be used in conjunction with coordinate transformation
            to determine the properties of a spatial yarn.  Finite element methods have been widely
            used to model the interaction between the fibre yarns and resin.
               The general procedure to predict the mechanical properties of a 3D textile composite
            using FEM is the same as that described in Section 4.3.4.


            4.4.3.1 30 Finite Element Modelling Scheme
            In  the  3D  finite  element  modelling  scheme,  three-dimensional  brick,  wedge  and
            tetrahedral elements are usually utilised to generate a mesh that models all the yarns and
            matrix in a unit cell. It is possible to model in detail the true geometric shape of all the
            yarns  and  the  yarn-matrix interfacial  surfaces.  Such a  model  depends on  accurate
            measurement of yarn geometry in a unit cell, and may not be cost-effective.  Accurate
            measurement  of  yarn  geometry  can  also  be  difficult due  to  limitations of  current
            measurement  techniques,  and  may  not  even  be  necessary  due  to  geometrical
            irregularities found in  all textile composites, including inconsistency in  tow  spacing,
            tow waviness and tow pinching.
               As  an  approximation, the cross-sectional shape of  a yarn  is often assumed to be
            uniform along an idealised centreline of the yarn path.  Typical cross-sectional shape of
            a yarn can be rectangular, circular, elliptical and lenticular.  For an idealised yarn with a
            uniform cross-section and  a defined centreline path, it is easy to develop a computer
            program that automatically generates the mesh  for a unit cell of  a woven composite
            material manufactured following a selected weaving process.  Figures 4.18 and  4.19
            depict  a  full  3D  finite element model  for  a  unit  cell  and  a  laminate block  of  a  3D
            orthogonal woven composite material.
               The  mechanical properties  of  the  composite constitutes  in  the  unit  cell of  a  3D
            woven composite material can be  assumed to be homogeneous and  isotropic for the
            matrix and orthotropic for the impregnated yarns with respect  to  their corresponding
            principle material axes.  The  mechanical properties of  each  yarn  can be determined
            using the properties of the fibre and matrix, the fibre volume fraction as well as the fibre
            direction and equations (4.6), (4.39) and (4.46).
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