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Basic rock fracture mechanics  135





                                               σ max
                                          a
                                                 Stress

                                    2a
                          ρ t                   σ L



                                                            2a
              Figure 4.2 A surface crack and an internal crack in a thin plate subjected to uniform
              tension (left) and the stress concentration induced by the internal crack (right).


                 From Eq. (4.2), it is evident that the stress concentration factor can be
              considerably larger than unity for narrow holes. For a circular borehole
              (a ¼ b), the stress concentration factor is 3. However, for a very narrow hole
              (e.g., a flat crack), the stress concentration factor is 21 if a ¼ 10b. This means
              that the induced maximum stress will reach 21 times of the applied stress.
              These effects become more obvious as the ratio a/b increases, e.g., when
              a/b ¼ 1000, the maximum tension at the point A is 2001 times the applied
              tensile stress. The ellipse in this case would appear as a fine straight crack,
              and a very small pull applied to the plate across the crack would set up a
              tension at the tips sufficient to start a tear in the material. The rapidity with
              which the induced stress decreases with the distance from this edge of the
              hole is also very noticeable (Inglis, 1913).
                 The maximum stress at the crack tip can also be expressed in the
              following form:
                                                   a
                                                   ffiffiffiffi
                                                r
                                   s max ¼  1 þ 2     s L                 (4.3)
                                                   r t
              where r t is the radius of curvature at the crack tip, and a is the half length of
              an internal crack, or the length of a surface crack (Suni, 2012), as shown in
              Fig. 4.2.


              4.2 Linear-elastic fracture mechanics
              4.2.1 Griffith crack theory
              Inglis’s theory shows that the stress increase at the tip of a crack is
              dependent only on the geometrical shape of the crack and not its absolute
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