Page 74 - Mechanics Analysis Composite Materials
P. 74

Chapter 3.  Mechanics qf a unidirectionalply     59

            be used to make fibers with the strength exceeding the strength of such traditional
            structural materials as aluminum or steel (see Table 1.1). The general answer is well
            known:  strength  of  a thin  wire  is  usually  much  higher  than  the  strength  of  the
            corresponding bulk material. This is demonstrated in Fig. 3.7 showing that the wire
            strength increases while the wire diameter is reduced.
              In  connection  with  this,  two  questions  arise.  First,  what  is  the  upper  limit  of
            strength that can be predicted for an infinitely thin wire or fiber? And second, what
            is the nature of  this phenomenon?
              The  answer  for  the  first  question  is  given  in  Physics  of  Solids.  Consider  an
            idealized model of a solid, namely a regular  system of atoms located  as shown in
            Fig. 3.8 and find the stress,  6,that destroys this system. Dependence  of  G on the
            atomic spacing following from  Physics of Solids is presented  in Fig.  3.9. Point  0
            of  the curve corresponds  to the equilibrium  of the  unloaded  system, while point
            U specifies the ultimate theoretical  stress, 0,.Initial tangent angle, u, characterizes
            material  modulus  of  elasticity,  E. To evaluate at, we  can  use  the  following sine
            approximation  (Gilman,  1959) for OU segment of the curve
                           a - ao
                fJ= a, sin 2n-   .
                            a0















                                                         '   d,mm
                                       0.4   0.8   1.2   1.6
                     Fig. 3.7.  Dependence of high-carbon steel wire strength on the wire diameter.



                                            0









                                            0

                                       Fig. 3.8.  Material model.
   69   70   71   72   73   74   75   76   77   78   79