Page 186 - Handbook of Materials Failure Analysis
P. 186

182    CHAPTER 7 Investigation of failure behavior of tubular components




                                                                      2            3
                                                     ð
                                                                              ð
                               ð
                              Ca=WÞ ¼  0:01752 + 0:10473 a=WÞ 0:20424 a=WÞ +0:13573 a=WÞ  (7.9)
                                                                 ð
                         The final load-displacement pair corresponding to the end of loading is also normal-
                         ized using the same equations as described above except that the final measured
                                   0
                         crack size a (after the specimen is break-open) is used instead of the crack size eval-
                                   f
                         uated using the normalization curve.
                            The normalized load-displacement data for all the six specimens have been
                         obtained using the above-mentioned approach and these are presented in
                         Figure 7.22. The data points to the right-hand side of the anchor point are excluded
                         as these data points corresponds to that of crack propagation and the crack growth
                         data at each point needs to be subsequently evaluated. The data with v   0:001
                                                                                    0
                                                                                    pli
                         are also discarded due to absence of crack growth at this very small amount of plastic
                         displacement. The remaining data points are fitted with the following analytical nor-
                         malization function, that is,
                                                            0    2
                                                        a + bv + cv0
                                                            pl   pl
                                                    P N ¼                               (7.10)
                                                           d + v 0 pl
                         where a, b, c, and d are fitting constants. Using these values of the constants, the
                         crack growth information of the remaining data points are evaluated.
                            The process of estimation of crack growth using load-normalization technique
                         involves an iterative procedure. The crack growth at a point is guessed and the normal-
                         ized load and displacement data are recalculated using Equations 7.6 and 7.8,respec-
                         tively. The procedure is repeated with update in the crack growth information till the
                         data point falls on the curve defined by Equation 7.10 within a predefined tolerance.
                         In this way, the crack extensions at all the points of the load-displacement diagram
                         are estimated. Using this information of crack growth as a function of loading, the

                                                                     Sp4
                                       250                                  Sp6
                                            Sp1                    Sp3   Sp5
                                     Normalized load (MPa)  200  Sp2









                                       150


                                         0.00      0.05       0.10      0.15
                                                     Normalized displacement
                         FIGURE 7.22
                         Fitted curves for normalized load-displacement data for all the six specimens used in the
                         fracture test.
   181   182   183   184   185   186   187   188   189   190   191