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Chapter 7.  improvement of transverse fracture  toughness with interface control   307




















                                          Number  of  nylon sheets

                                           and
               Fig. 7.16. Impact fracture toughness (0) interlaminar shear strength (ILSS, 0) of carbon fiber-epoxy
               matrix composites with varying number of nylon sheets as delamination promoters. After Favre (1977).

               increased successfully by three times with embedded nylon sheets, at the expense of
               some 25%  reduction in ILSS (Favre, 1977) (Fig. 7.16). Perforated films were found
                to  be  more  effective than  unperforated  films because  the  perforated  films  could
               provide  both the weak  and strong bonding in the regions of film and perforation,
                respectively,  similar  to  the  intermittent  interlaminar  bond  concept  (Mai  et  al.,
                1982a). The failure mechanisms underlying the delamination promoter concept are
                schematically  shown  in  Fig.  7.17.  In  the  weak  regions,  delamination  occurred
               allowing  the  main  crack  front  to be  bifurcated  and  the  sub-cracks  to propagate
               along  the  laminar  interfaces.  These  mechanisms  promote  energy  absorption,  as
               envisaged from the tensile debonding theory  (Cook and Gordon, 1964). However,
               excessive delamination was effectively discouraged and the shear stress transfer was
               permitted between laminae in the strong regions, enabling the original bond strength
               to be maintained. While the tensile strength dropped about 20%, and the Young’s
               modulus remained the same, the transverse fracture toughness of CFRPs increased a





                                     I nterlarninar        -Strong   bonding
                                    subrrack  shown

                                  : I transverse crack


                                     (a)                  I  bl
                Fig. 7.17. Schematic illustrations of sub-crack propagation along the laminar interface of the composite
                          intermittently bonded with perforated films. After Jea and Felbeck (1980).
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