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Chapter 3.  Mechanics of a unidirectional ply    19

           3.2.4.Fracture toughness
             Fracture  toughness  is  a  very  important  characteristic  of  a  structural  material
           indicating resistance of a material to cracks and governed  by  the work  needed  to
           destroy a material (work of fracture). As known, there exist brittle and ductile metal
           alloys  whose  typical  stress-strain  diagrams  are  shown  in  Fig. 3.25.  Comparing
           alloys with one and the same basic metal  (e.g., steel alloys) we can see that  while
           brittle alloys have higher strength, 5, ductile alloys have higher ultimate elongation,
           E,  and, as a result, higher work of  fracture which is proportional to the area under
           the stress-strain  diagram. Though brittle materials have, in general, higher strength,
           they  are sensitive to cracks  which  propagating  can  cause  material  failure  under
           stress that is much  lower than the  static  strength. That is why designers usually
           prefer ductile materials with lower strength but higher fracture toughness. A typical
           dependence of fracture toughness on static strength for metals is shown in Fig. 3.26
           (line I).  For composites, this dependence is entirely different (line 2) - higher static
           strength corresponds  usually  to higher  fracture  toughness  (Mileiko,  1982). This
           phenomenon  is demonstrated  for a  unidirectional boron-aluminum  composite in
           Fig. 3.27 (Mileiko,  1982). As  can be seen, an increase in fiber volume fraction, of,












           Fig. 3.26. Typical  relations  between  fracture  toughncss  (K)  and strength  (3)for  metals  (1)  and
                                         composites (2).


















                               0
                                 0   0.1   0.2   0.3   0.4   OB
           Fig. 3.27.  Dependence of static strength (I),  work of fracture (2),and fatigue strength (3) on fiber volume
                             fraction for a  boron -aluminum composite material.
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