Page 54 - Fiber Fracture
P. 54

MODELS OF FIBRE FRACTURE                                             39

             it is possible, in principle, to calculate the variability of the fracture strength. Without
             it, one has to resort to statistical methods. The statistical variation of strength of brittle
             solids is usually described using a Weibull distribution. Coleman (1958) gave reasons
             why such a distribution of strength is plausible for fibres whose strength is independent
             of the rate of loading, and he computed the mean fibre strength as:




             where L  is the fibre length, m the Weibull modulus, 00  is the characteristic strength,
             defined as the stress at which the failure probability of a fibre of length Lo is 0.63 and r
             the gamma function.
               The Weibull approach, although useful when comparing fibres, does not take account
             of  the  failure  mechanism.  On  the  other  hand,  the  deterministic  theory  of  LEFM
             overcomes some of the limitations of the Weibull method but is applicable only when
             the  initial  crack  geometry is  known.  There  are  intermediate cases  where  the  crack
             geometry is known but not its precise location, as, for example, inner circular cracks
             located randomly.  In  these  circumstances, LEFM  can  provide answers to  questions
             such as: what is the maximum rupture stress for a postulated maximum defect size of
             unknown location?
               Some of these questions have been answered in a recent paper (Guinea et a]., 2002b)
             for a very  simple family of  defects: inner circular cracks and surface circular cracks,
             both in planes normal to the fibre axis. The main result is plotted in Fig. 5, showing
             the dependence of  minimum rupture stress uc on crack radius. This plot may be used
             to set boundaries for some problems in brittle fibre fracture analysis, Le.:  to evaluate
             the maximum circular defect size when the rupture stress is known or, conversely, to
            estimate the  rupture stress when  defects, of  unknown  location, can  be  modelled as
             circular cracks.
               The way of modelling brittle fracture of fibres is paved by  LEFM, and good agree-
             ment between experimental results has been found. Future refinements will improve the
             accuracy of the predictions, in particular for anisotropic fibres where cracks propagate
             in mixed mode. More inputs from fractography and physical aspects of fracture will be
            helpful in modelling defects able to initiate cracks.

             Ductile Behaviour

             Modelling fibre ductile fracture is  an  involved problem, even for homogeneous and
             macro-defect-free fibres.  Under  tensile loading, fibres eventually reach an  instability
             point, where strain hardening cannot keep pace with loss in cross-sectional area, and a
             necked region forms beyond the maximum load. A central crack is nucleated, spreads
            radially and finally, when approaching the fibre surface, propagates along localised shear
            planes, at roughly 45" to the axis, to form the  'cone'  part of the fracture. This is the
             typical cup-and-cone fracture of a ductile failure after a tensile test.
               Exceptions to this form  of  ductile fracture appear in microstructurally clean high-
            purity metal fibres, which sometimes neck down to a point. On the contrary, in ductile
            fibres containing large defects, or deep surface notches, necking is absent and a brittle
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