Page 407 - Mechanical Behavior of Materials
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408                                             Chapter 8  Fracture of Cracked Members


            Section 8.5
            8.23 A large part in a turbine-generator unit operates near room temperature and is made of
                 ASTM A470-8 steel. A surface crack has been found that is roughly a semi-ellipse, with
                 surface length 2c = 60 mm and depth a = 20 mm. The stress normal to the plane of the
                 crack is 200 MPa, and the member width and thickness are large compared with the crack
                 size. What is the safety factor against brittle fracture? Should the power plant continue
                 to operate if failure of this part is likely to cause costly damage to the remainder of the
                 unit?
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            8.24 A solid circular shaft 40 mm in diameter is made of the steel 300-M (300 C temper). It is
                 subjected to a bending moment of 2 kN·m and may contain a half-circular surface crack,
                 as in Fig. 8.17(d).
                   (a) What crack size a c will cause brittle fracture?
                   (b) What crack size a must be found by inspection to achieve a safety factor in stress of
                      3.5 against brittle fracture?
                   (c) Calculate the ratio of the crack size from (a) to that from (b), and comment on the
                      significance of this value.
            8.25 A beam with a rectangular cross section, as in Fig. 8.17(c), is made of 2219-T851 aluminum
                 and must withstand a bending moment of M = 150 N·m. The thickness is b = 20 mm, and
                 a quarter-circular corner crack as large as a = 1 mm may be present.
                   (a) What beam depth t is required for a safety factor 3.0 against brittle fracture?
                   (b) For the beam depth t as calculated in (a), is the design adequate with respect to possible
                      fully plastic failure? (Suggestion: Make a conservative estimate of M o by assuming that
                      the crack extends across the full thickness b.)
            8.26 A round rod of silicon nitride ceramic is loaded as a simply supported beam under a uniformly
                 distributed force, as in Fig. A.4(b). The rod diameter is 10 mm, the length between supports is
                 120 mm, and the distributed force is w = 3.0 N/mm.
                   (a) If a half-circular surface crack as deep as 0.5 mm may be present, what is the safety
                      factor against brittle fracture?
                   (b) If a safety factor of 4.0 is required, what is the largest permissible depth for a half-
                      circular surface crack?
            8.27 Solid circular shafts made of titanium 6Al-4V (annealed) are subjected in service to bending,
                 with a moment M = 6.0kN·m. Half-circular surface cracks, as in Fig. 8.17(d), may exist in
                 the part. From nondestructive inspection, it is expected that no cracks larger than a = 5.0mm
                 are present.
                   (a) What shaft diameter is required to resist yielding with a safety factor of 2.0 if no crack
                      is present?
                   (b) For an inspection-size crack, what shaft diameter is required to resist brittle fracture
                      with a safety factor of 3.0?
                   (c) What shaft diameter should actually be used?
            8.28 A shaft of diameter 60 mm has a circumferential surface crack, as in Fig. 8.14, of depth
                 a = 10 mm. The shaft is made of the 18-Ni maraging steel (air melted) of Table 8.1.
                   (a) If the shaft is loaded with a bending moment of 2 kN·m, what is the safety factor against
                      brittle fracture?
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