Page 334 - Mechanics Analysis Composite Materials
P. 334

Chapter 7.  Environmental, special loading, and manufacturing effects   3 19
            effect of aging, test under  transverse  bending  (see Fig. 4.95) is usually performed.
            Thus found flexural strength

                    3Pl
                ijf = -
                    2bh'
            allows  for  both  fiber  and  matrix  material  degradation  in  the  process  of  aging.
            Experimental results of G.M. Gunyaev et al. showing dependence of the normalized
            flexural strength on time for advanced composites are presented in Fig. 7.10.


            7.3.  Time and timedependent loading effects

            7.3.I.  Viscoelastisity

              Polymeric  matrices  are  characterized  with  pronounced  viscoelastic  properties
            resulting in time-dependent  behavior of polymeric composites that manifests itself
            in  creep  (see Section  ].I),  stress  relaxation,  and dependence  of  the  stress-strain
            diagram on the rate of loading. It should be emphasized that in composite materials,
            viscoelastic deformation  of the polymeric matrix is restricted by fibers that usually
            are  linear  elastic  and  do  not  demonstrate  time-dependent  behavior.  The  one
            exception  to  existing  fibers  is  represented  by  aramid  fibers  that  are  actually
            polymeric  themselves  by  their  nature.  Properties  of  metal  matrix,  ceramic,  and
            carbon-carbon  composites  under  normal  conditions  do  not  depend  on  time.
            Rheologic  (time-dependent)  characteristics of  structural materials are revealed  in
            creep  tests  allowing us  to plot  the dependence  of  strain  on  time  under  constant
            stress. Such diagrams are shown in Fig. 7. I 1 for aramid-poxy  composite described






                                                           1
                                                           2
                                                           3
                                                           4
                             0.6
                                -
                             0.4
                                -
                             0.2
                              o                             t,year
                                0    1    2     3    4    5
            Fig. 7.10.  Dependence of the normalized flexural strength on the time of aging for boron (I),carbon (2).
                                 aramid (3). and glass (4)epoxy composites.
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