Page 363 - Failure Analysis Case Studies II
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              Fig. 3.  The fracture surface of one of the four fractures of cylinder B. The photograph  has been marked to
              highlight beachmarks caused either by damage during hydrotests of the cylinder or indicating changes to the
              crack growth mechanism. Some growth stages might leave no clear beachmark.
              a        Area of different morphology indicating initial defect.
              a-b      Area of growth which is mainly intergranular which is consistent with SMIE. Note that in this
                       region some grains are very large because of recrystallisation during the heat treatment cycle
                 c-c'
              k,  Faster area of growth, plastic areas mixed with SMIE.
              After c, c'   Plastic rupture, surface approaches 45" to other fracture plane.



          bottle broke into two. Figure 3 shows one of the cracks in the neck region. It appears that there is
          a region of quite different crack growth prior to the final failure which is indicated by regions of 45"
          shear. There are at least two visible beach marks, indicating crack growth stopped for a time, on
          this specimen.
            The characteristics  of the  growth  observed by  examining beachmarks  in  both the  specimens
          indicate fairly stable growth for a time moving mainly up the threaded portion but then there is a
          tendency to move more quickly without penetrating  the outer  surface with  some growth  totally
          interior to the cylinder.



                                3.  MODELS  OF  CRACK  GROWTH
          3.1.  Existing means of calculation of crack growth rate
            Crack propagation due to SMIE in small specimens under different imposed K, values has been
          studied previously by Ibrahim [l]. One set of specimens was cut from aluminium ingots with an
          assay of  lOOppm  Pb. The lowest value of KI used  for this  series of  tests was  13MPaJm.  The
          following equation was determined for crack growth rate in mm/h:
                                    log,,(da/dt)  = 0.234KI-7.719.
            Ibrahim and Stark [lo] present additional studies on some specimens cut from Australian pressure
          vessels and tested at room temperature. The alloys used in these gas cylinders had very low levels
          of lead present, probably less than 10ppm. The growth was much slower and the equation derived
          for crack growth rate in mm/h was
                                   log,,(da/dt)  = 0.20164K1- 8.889.               (2)
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