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                             PROPERTIES OF STRUCTURAL STEELS AND EFFECTS OF STEELMAKING AND FABRICATION


                                                              STRUCTURAL STEELS, STEELMAKING, AND FABRICATION  1.21
















                                    FIGURE 1.10  Transition curves from Charpy-V notch impact tests. (a) Variation of percent shear fracture with
                                    temperature, (b) Variation of absorbed energy with temperature.
                                  within any given product designation unless specifically produced to minimum requirements. The test
                                  temperature may be specified higher than the lowest operating temperature to compensate for a lower
                                  rate of loading in the anticipated application. (See Art. 1.1.5.)
                                    It should be noted that as the thickness of members increases, the inherent restraint increases and
                                  tends to inhibit ductile behavior. Thus special precautions or greater toughness, or both, is required
                                  for tension or flexural members comprised of thick material. (See Art. 1.16.)

                                  Fracture-Mechanics Analysis.  Fracture mechanics offers a more direct approach for prediction of
                                  crack propagation. For this analysis, it is assumed that a crack, which may be defined as a flat, inter-
                                  nal defect, is always present in a stressed body. By linear-elastic stress analysis and laboratory tests
                                  on a precracked specimen, the defect size is related to the applied stress that will cause crack prop-
                                  agation and brittle fracture, as outlined below.
                                    Near the tip of a crack, the stress component f perpendicular to the plane of the crack (Fig. 1.11a)
                                  can be expressed as

                                                                   f =  K l                            (1.2)
                                                                       2p r

                                  where r is distance from tip of crack and K l is a stress-intensity factor related to geometry of crack and
                                  to applied loading. The factor K l can be determined from elastic theory for given crack geometries and






















                                      FIGURE 1.11  Fracture mechanics analysis for brittle fracture. (a) Sharp crack in a stressed infinite plate.
                                      (b) Disk-shaped crack in an infinite body. (c) Relation of fracture toughness to thickness.


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