Page 336 - Mechanical Behavior of Materials
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Section 8.2  Preliminary Discussion                                        337


            presence of a crack.) Repairs necessitated by cracks may involve replacing a part or modifying it,
            as by machining away a small crack to leave a smooth surface, or by reinforcing the cracked region
            in some manner.
               In this chapter, we will introduce fracture mechanics and study its application to failure under
            static loading. Later, in Chapter 11, we will consider growth of cracks due to cyclic loading.


            8.2 PRELIMINARY DISCUSSION

            Before introducing the details of fracture mechanics, it is useful to make some observations
            concerning the general nature of cracks and their effects.


            8.2.1 Cracks as Stress Raisers
            Consider an elliptical hole in a plate of material, as illustrated in Fig. 8.3(a). For purposes of
            discussion, the hole is assumed to be small compared with the width of the plate and to be aligned
            with its major axis perpendicular to the direction of a uniform stress, S, applied remotely. The
            uniform stress field is altered in the neighborhood of the hole, as illustrated for one particular case
            in Fig. 8.3(b).
               The most notable effect of the hole is its influence on the stress σ y parallel to S. Far from the
            hole, this stress is equal to S. If examined along the x-axis of (b), the value of σ y rises sharply near
            the hole and has a maximum value at the edge of the hole. This maximum value depends on the
            proportions of the ellipse and its tip radius ρ:

                                                 c             c
                                                             !
                                     σ y = S 1 + 2  = S 1 + 2                          (8.1)
                                                d              ρ


                                                   8
                                                                      y
                                    S                   k   = 7
                                                         t
                                               σ                          σ y
                          2                    S   6                              x
                     ρ =  d                                                  σ x
                         c
                                h
                                                   4    σ y      c/d = 3
                                     t
                    d
                         c
                                b                  2    σ
                                                         x
                                                   0
                                                          1     2     3      4     5
                           (a)                (b)                 x/ρ

            Figure 8.3 Elliptical hole in a wide plate under remote uniform tension, and the stress
            distribution along the x-axis near the hole for one particular case.
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