Page 333 - Engineered Interfaces in Fiber Reinforced Composites
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314               Engineered inlerfaces in fiber reinforced composites

                                     121
                                                      Cure Temp: 177OC
                                      0-    0
                                              0                  121OC  0
                                      8-          0
                                        -0          0
                                      6-      0        0
                                                 n        0
                                      4-           0         0
                                                    C)
                                                      0         0  0
                                      2-                 cb
                                                          O0      %%
                                                         ,  *  ?o.,,   .  ,
                                                               uv



                    Fig. 7.21. Maximum deflections of [Oi/9Oi], AS4 carbon fiber-3501-6  epoxy matrix composites plotted as
                                    a function of temperature. After Crasto and Kim (1993).

                    cure temperature. The laminate returns to a completely flat sheet at a temperature
                    slightly above the cure temperature, and produces a reverse curvature with further
                    increase in temperature.  The lamination  residual stresses can be  reduced, to some
                    extent, within a given temperature range by selecting an optimum stacking sequence
                    and ply orientation  (Ishikawa et al.,  1989).

                    7.5.1.3. Other sources of residual  stresses
                      In addition to those induced thermally, there are other sources of residual stresses.
                    These include mechanical  residual  stresses, and those induced  by  phase  transfor-
                    mation  in  composites  based  mainly  on  ceramics,  and  crystallization  in  semi-
                    crystalline  thermoplastic  composites.  Mechanical  residual  stresses  are  present
                    mainly  in  ductile  metal  matrix  composites  due  to  the  difference in  flow  stress
                    between  the  components  (Metcalfe,  1974).  This  type  of  residual  stress  becomes
                    important when the composite is highly loaded to plastically deform one or both
                    components.  Phase  transformation  in  certain  ceramics  and  ceramic  composites
                    accompany  significant  volume  changes,  while  the  transforming  component  is
                    mechanically restrained. As a result, the surrounding material is locally strained by
                    this  volume  change.  A  good  example  of  the  phase  transformation  is  partially
                    stabilized zirconia (ZrOz) which contains small amounts of MgO, CaO or Y203, and
                    undergoes a 3.25%  volume expansion during cooling below approximately 1000°C
                    due to transformation  from the tetragonal  phase  to the monoclinic phase  (Porter
                    and Heuer, 1977). A very high fracture toughness can be achieved if the particle size
                    and processing conditions are carefully controlled.
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