Page 251 - T. Anderson-Fracture Mechanics - Fundamentals and Applns.-CRC (2005)
P. 251

1656_C005.fm  Page 231  Monday, May 23, 2005  5:47 PM





                       Fracture Mechanisms in Metals                                               231
















                                                               FIGURE 5.12 The limit-load model for void insta-
                                                               bility. Failure is assumed to occur when the net sec-
                                                               tion stress between voids reaches a critical value.





                       and fracture occurs when

                                                              d
                                                        σ        = σ                            (5.16b)
                                                              +
                                                          nc()  db  1
                       where σ  is the maximum remote principal stress. As with Equation (5.15), the Thomason model
                             1
                       is of limited practical value. The void interactions leading to ductile failure are far too complex to
                       be captured by a simple area reduction model. Moreover, the final stage in failure is very abrupt,
                       as discussed earlier. Once the void fraction reaches 10 to 20%, failure occurs with only a minimal
                       increase in the nominal strain.


                       5.1.3 DUCTILE CRACK GROWTH

                       Figure 5.13 schematically illustrates microvoid initiation, growth, and coalescence at the tip of a
                       preexisting crack. As the cracked structure is loaded, local strains and stresses at the crack tip
                       become sufficient to nucleate voids. These voids grow as the crack blunts, and they eventually link
                       with the main crack. As this process continues, the crack grows.
                          Figure 5.14 is a plot of stress and strain near the tip of a blunted crack [21]. The strain exhibits
                       a singularity near the crack tip, but the stress reaches a peak at approximately two times the crack-
                                                   1
                       tip-opening displacement (CTOD).  In most materials, the triaxiality ahead of the crack tip provides
                       sufficient stress elevation for void nucleation; thus the growth and coalescence of microvoids are
                       usually the critical steps in ductile crack growth. Nucleation typically occurs when a particle is
                       ∼2δ from the crack tip, while most of the void growth occurs much closer to the crack tip, relative
                       to CTOD. (Note that although a void remains approximately fixed in absolute space, its distance
                       from the crack tip, relative to CTOD, decreases as the crack blunts; the absolute distance from the
                       crack tip also decreases as the crack grows.)
                          Ductile crack growth is usually stable because it produces a rising resistance curve, at least
                       during the early stages of crack growth. Stable crack growth and R curves are discussed in detail
                       in Chapter 3 and Chapter 7.
                          When an edge crack in a plate grows by microvoid coalescence, the crack exhibits a tunneling
                       effect, where it grows faster at the center of the plate, due to the higher stress triaxiality.


                       1  Finite element analysis and slip line analysis of blunted crack tips predict a stress singularity very close to the crack tip
                       (∼0.1 CTOD), but it is not clear whether or not this actually occurs in real materials because the continuum assumptions
                       break down at such fine scales.
   246   247   248   249   250   251   252   253   254   255   256