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                       Linear Elastic Fracture Mechanics                                            41


                       it is possible to obtain a significant amount of stable crack growth. If an instability occurs during
                       the test, the R curve cannot be defined beyond the point of ultimate failure.



                       EXAMPLE 2.3


                         Evaluate the relative stability of a DCB specimen (Figure 2.9) in load control and displacement control.

                         Solution: From the result derived in Example 2.2, the slope of the driving force curve in load control
                         is given by

                                                                2
                                                        dG   =  2 Pa  =  2 G
                                                        da   P  BEI  a

                         In order to evaluate displacement control, it is necessary to express G in terms of ∆ and a. From beam
                         theory, load is related to displacement as follows:

                                                          P =  3 ∆ EI
                                                              2 a 3
                         Substituting the above equation into expression for energy release rate gives

                                                                2
                                                          G =  9 ∆ EI
                                                              4Ba 4
                         Thus

                                                      dG   =−  9 ∆ 2 EI  =−  4 G
                                                      da  ∆  Ba 5    a

                         Therefore, the driving force increases with crack growth in load control and decreases in displacement
                         control. For a flat R curve, crack growth in load control is always unstable, while displacement control
                         is always stable.



                       2.5.3 STRUCTURES WITH FINITE COMPLIANCE

                       Most real structures are subject to conditions between load control and pure displacement
                       control. This intermediate situation can be schematically represented by a spring in series with
                       the flawed structure (Figure 2.12). The structure is fixed at a constant remote displacement ∆ ;
                                                                                                    T
                       the spring represents the system compliance C . Pure displacement control corresponds to an
                                                              m
                       infinitely stiff spring, where  C .  = 0. Load control (dead loading) implies an infinitely soft
                                                 m
                       spring, i.e., C . = ∞.
                                  m
                          When the system compliance is finite, the point of fracture instability obviously lies somewhere
                       between the extremes of pure load control and pure displacement control. However, determining
                       the precise point of instability requires a rather complex analysis.
                          At the moment of instability, the following conditions are satisfied:

                                                            G = R                               (2.34a)
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