Page 335 - Mechanics Analysis Composite Materials
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320                 Mechanics and analysis of composite materials

                        El  ,%
                        1.5              Q, = 600 MPa
                                                        03
                                         6,= 450 MPa
                                                        02
                         1
                                         6,= 300 MPa
                                                        01
                        0.5


                         0                              '  t,  Days  (24 hours)
                          0    200   400   600   800   1000
              Fig. 7.1 1.  Creep strain response of unidirectional aramid-epoxy composite under tension in longitudinal
                                    direction with three constant stresses.

              by  Skudra  et al.  (1989).  An  important  characteristic  of  the  material  can  be
             established  if  we  plot  the  so-called  isochrone  stress-strain  diagrams  shown  in
              Fig. 7.12.  Three curves in this Figure are plotted for t = 0, t = 100, and t = 1000
             days, and the points on these curves correspond to points 1,2,3 in Fig. 7.1 1. As can
             be  seen, the initial parts of  the isochrone diagrams are linear which means that
             under moderate stress, material under study can be classified as linear-viscoelastic
             material. To characterize such a material, we need to have only one creep diagram,
             while the other curves can be plotted increasing strains in proportion to stress. For
              example,  the  creep  curve  corresponding  to  51 = 450 MPa  in  Fig. 7.11  can  be
              obtained if we multiply strains corresponding to cq  = 300 MPa by  1.5.
                Linear-viscoelastic material behavior is described with  reasonable accuracy by
              the  hereditary  theory  according to  which  the  dependence of  strain  on  time  is
              expressed as
                                              1
                       4 ii
                 ~(t)= - ~(t)+  C(t - T)CT(T)~T  .                             (7.31)



















                                     0     0.5   1     1.5
                   Fig. 7.12.  Isochrone stress-strain  diagrams corresponding to creep curves in  Fig. 7.1 1
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