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30 Woven Composites                           123

            5.3.2 Compressive Properties
            The compressive properties and failure mechanisms of 3D woven composites have been
            investigated in great detail because of their potential application in aerospace structures.
            Most attention has been given to 3D carbordepoxy composites because of their use in
            aircraft,  although  3D  carbodbismaleimide  and  3D  Kevlar/epoxy  have  also  been
            examined.  Most studies find that the compressive modulus of 3D woven composites is
            lower than 2D prepreg tape or  woven laminate with  a  similar fibre volume content
            (Brandt et al., 1996; Guess and Reedy, 1986; Farley et al., 1992). The reduced modulus
            is due to crimping and increased waviness of the load-bearing fibres caused by the z-
            binders.
               The effect of z-binder reinforcement on the axial compressive strength of 3D woven
            composites is  complex,  with  both  improvements  and  reductions to  strength being
            observed.  Figure  5.14  presents  compressive strength  data  for  three  types  of  3D
            composites with different z-binder contents.  The normalised compressive strength is
            defined as the compressive strength of the 3D woven composite divided by the strength
            of  an 2D woven laminate with  nominally the same fibre content.  The data plotted in
            Figure 5.14  shows no  clear effect; with  both  an  increase and  reduction  to  strength
            occurring. The data does reveal, however, that the compressive strength of a 3D woven
            composites is usually improved or degraded by less than 20%, which is the same effect
            observed for the tensile properties shown in Figures 5.8 and 5.1 1.



                           -
                        1.50


                        1.25  -
                                0
                                    0        0
                           -
                        1.00
                           -
                        0.75
                           -
                        0.50
                           -        3D Orthogonal GlasdEpoxy (Arendts et al., 1989)
                        0.25
                                 0  3D Interlock Glass/Epoxy (Arendts et al., 1989)
                                 A 3D Interlock KevlarlEpoxy (Guess and Reedy, 1985)
                        0.00' -   I  .  '  '  '  '   I   *  '  *   I  -  '   a  '  '  '  '  '
                           0   2    4   6    8   10   12   14   16   18   20
                                         Z-Binder Content (%)

            Figure 5.14 Plot of compressive strength against z-binder content for various 3D woven
            composites.


            The cause for the improved compressive strength of  the 3D woven composites is not
            clear.  Those studies that report an  improvement to the strength do not describe the
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