Page 81 - Mechanics Analysis Composite Materials
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66                 Mechanics and analysis of composite materials

             Table 3.2
             Strength of bundles consisting of fibers with different strength.

             Fiber no.    Bundle no.
                          1             2            3             4            5

                           0.6           0.7          0.85         0.9          0.95
                           0.8           0.9          0.9          0.85         0.95
                           1.o           1.2          1.1          1.o          0.95
                           1.6           1.4          1.15         1.05         0.95
                           3.0           I .6         1.4          1.1          0.95
                           1.4           1.16         1 .os        I .o         0.95
             *"I
             r,  (%I      95.0          66.0         22.0          7.8          0
             F             3.2           3.6          4.25         4.5          4.75



             relatively low stiffness changes the mechanism of fibers interaction and considerably
             increases their effective strength. To show this, the strength of dry fiber bundles can be
             compared with the strength of the same bundles after they were impregnated with
             epoxy resin and cured. The results are listed in Table 3.3. As can be seen, composite
             bundles  in  which fibers are joined  together  with  matrix  demonstrate significantly
             higher  strength, and  the  higher  the  fiber  sensitivity to damage,  the higher  is  the
             difference in strength of dry and composite bundles. The influence of matrix on the
             variation of strength is even more significant. As follows from Table 3.4, variation
             coefficientsof composite bundles are by an order lower than those of individual fibers.
               To clarify the role of matrix in composite materials consider a simple model of a
             unidirectional ply shown in Fig. 3.15 and  apply the method  of analysis developed
             for stringer panels (Goodey,  1946).
               Let the ply of thickness 6 consist of 2k  fibers symmetrically distributed  on both
             sides  of  the  central  fiber  n = 0.  The fibers  are joined  with  layers  of  the  matrix
             material, and the fiber volume fraction is

                                                                               (3.17)



             Table 3.3
             Strength of dry bundles and composite bundles.

             Fibers       Sensitivity of fibers   Ultimate tensile load P (N)   Strength
                          to damage                                         increase (X)
                                            Dry bundle   Composite bundle
             Carbon       High              14           26                 85.7
             Glass        Moderate          21           36                 71.4
             Aramid       Low               66           84                21.3
   76   77   78   79   80   81   82   83   84   85   86