Page 149 - Plastics Engineering
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132                                   Mechanical Behaviour of Plastics

                       are insensitive to notch condition, other thermoplastics will exhibit brittle failure
                       if they contain sharp cracks of significant dimensions.
                         Polycarbonate is perhaps the most notoriously notch-sensitive of all thermo-
                       plastics,  although nylons  are also susceptible to  ductilehrittle  transitions in
                       failure behaviour caused by  notch sharpening. Other plastics such as acrylic,
                       polystyrene and thermosets are always brittle - whatever the crack condition.
                         For brittle failures we may use the fracture mechanics analysis introduced
                       in the previous sections. From equations (2.96) and (2.99) we may write
                                                 K%  m2a
                                            G --=-          =constant              (2.110)
                                             c-
                                                 E      E
                         From this therefore it is evident that the failure stress, af, is proportional to
                       u-'j2.  This relationship is plotted as line B on Fig. 2.68. This diagram is now
                       very  useful because it  illustrates the type of  ductilehrittle  transitions which
                       may be observed in plastics. According to line B, as the flaw size decreases
                       the  failure stress tends towards infinity. Clearly this  is  not  the  case and  in
                       practice what happens is that  at  some defect size (w) the material fails by
                       yielding (line A) rather than brittle fracture.
                         This diagram also helps to illustrate why  the inherent fracture toughness of
                       a material is not the whole story in relation to brittle fracture. For example,
                       Table 2.2 shows that  polystyrene, which  is  known  to  be  a  brittle  material,
                       has a K value of about 1 MN m-3/2. However, LDPE which has a very high
                       resistance to  crack  growth  also has  a  K  value  of  about  1 MN m-3/2.  The
                       explanation is that polyethylene resists crack growth not because it is tough but
                       because it has a low yield strength. If a material has a low yield stress then its
                       yield locus (line A in Fig. 2.68) will be pulled down, possibly below the brittle
                       locus as happens for polyethylene. Fig. 2.69 illustrates some of the variations
                       which are possible in order to alter the ductilehrittle characteristics of plastics.
                       The brittle failure line can be shifted by changes in chemical structure, use of
                       alloying techniques, changes in processing conditions, etc. The yield locus line
                       can be  shifted by  the use of  additives or changes in the ambient temperature
                       or straining rate.
                         It is apparent therefore that a materials resistance to crack growth is defined
                       not just by  its inherent toughness but by  its ratio of toughness to yield stress.
                       Some typical values of Kl,/a,  are given in Table 2.2.
                         Another approach to the question of resistance to crack growth is to consider
                       the extent to which yielding occurs prior to fracture. In a ductile material it
                       has been found that yielding occurs at the crack tip and this has the effect of
                       blunting the crack. The extent of the plastic zone (see Fig. 2.70) is given by
                                                              2
                                                       1
                                                 rp = - (E)                        (2.111)
                                                      27t  ar
                       for plane stress. The plane strain value is about one third of this.
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