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264   •  Chapter 8  /  Failure


                         are desired. On the basis of this                                 s
                         criterion, rank the metal alloys
                         listed in Table B.5, Appendix
                         B, as to critical crack size, from
                         longest to shortest.                                                 2a
                         (b) An alternative design that is        p
                         also often utilized with pressure   t  p     p
                         vessels is termed leak-before-               r
                         break. On the basis of principles   p         p
                         of fracture mechanics, allow-
                         ance is made for the growth of      p        p                       s
                         a crack through the thickness            p
                         of the vessel wall prior to the
                           occurrence of rapid crack prop-
                         agation (Figure 8.11). Thus, the   Figure 8.11  Schematic diagram showing the cross section
                         crack will completely penetrate   of a spherical tank that is subjected to an internal pressure p
                         the wall without catastrophic  and that has a radial crack of length 2a in its wall.
                         failure, allowing for its detection by the leaking of pressurized fluid. With this criterion the
                         critical crack length a c  (i.e., one-half the total internal crack length) is taken to be equal to the
                         pressure vessel thickness t. Allowance for a c    t instead of a c    t/2 ensures that fluid leakage
                         will occur prior to the buildup of dangerously high pressures. Using this criterion, rank the
                         metal alloys in Table B.5, Appendix B, as to the maximum allowable pressure.
                            For this spherical pressure vessel, the circumferential wall stress s is a function of the pressure
                         p in the vessel and the radius r and wall thickness t according to
                                                               pr
                                                           s =                                     (8.8)
                                                                2t
                         For both parts (a) and (b), assume a condition of plane strain.

                         Solution
                         (a) For the first design criterion, it is desired that the circumferential wall stress be less than
                         the yield strength of the material. Substitution of s y  for s in Equation 8.5 and incorporation of
                         a factor of safety N leads to

                                                               s y
                                                      K Ic = Y a  b 1pa c                          (8.9)
                                                               N
                        where a c  is the critical crack length. Solving for a c  yields the following expression:
                                                            N 2  K Ic  2
                                                       a c =    a   b                             (8.10)
                                                             2
                                                           Y p    s y
                         Therefore, the critical crack length is proportional to the square of K Ic /s y , which is the basis for
                         the ranking of the metal alloys in Table B.5. The ranking is provided in Table 8.3, where it may
                         be seen that the medium carbon (1040) steel with the largest ratio has the longest critical crack
                         length and, therefore, is the most desirable material on the basis of this criterion.
                         (b) As stated previously, the leak-before-break criterion is just met when one-half the internal
                         crack length is equal to the thickness of the pressure vessel—that is, when a   t. Substitution
                         of a   t into Equation 8.5 gives
                                                        K Ic = Ys1pt                              (8.11)
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