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Callister - An introduction - 8th edition

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8.6 Fracture Toughness Testing • 253<br />

Figure 8.13<br />

Temperature<br />

dependence of the<br />

Charpy V-notch<br />

impact energy (curve<br />

A) and percent shear<br />

fracture (curve B)<br />

for an A283 steel.<br />

(Reprinted from<br />

Welding Journal.<br />

Used by permission<br />

of the American<br />

Welding Society.)<br />

Impact energy (J)<br />

100<br />

80<br />

60<br />

40<br />

Temperature (°F)<br />

–40 0 40 80 120 160 200 240 280<br />

Impact<br />

energy<br />

B<br />

A<br />

Shear<br />

fracture<br />

100<br />

80<br />

60<br />

Shear fracture (%)<br />

40<br />

20<br />

20<br />

0<br />

–40 –20 0 20 40 60 80 100 120 140<br />

0<br />

Temperature (°C)<br />

fracture appearance (e.g., 50% fibrous fracture). Matters are further complicated<br />

inasmuch as a different transition temperature may be realized for each of these criteria.<br />

Perhaps the most conservative transition temperature is that at which the fracture<br />

surface becomes 100% fibrous; on this basis, the transition temperature is<br />

approximately 110C (230F) for the steel alloy that is the subject of Figure 8.13.<br />

Structures constructed from alloys that exhibit this ductile-to-brittle behavior<br />

should be used only at temperatures above the transition temperature, to avoid brittle<br />

and catastrophic failure. Classic examples of this type of failure occurred, with<br />

disastrous consequences, during World War II when a number of welded transport<br />

ships, away from combat, suddenly and precipitously split in half. The vessels were<br />

constructed of a steel alloy that possessed adequate toughness according to roomtemperature<br />

tensile tests. The brittle fractures occurred at relatively low ambient<br />

temperatures, at about 4C (40F), in the vicinity of the transition temperature<br />

of the alloy. Each fracture crack originated at some point of stress concentration,<br />

probably a sharp corner or fabrication defect, and then propagated around the entire<br />

girth of the ship.<br />

59 12 4 16 24 79<br />

Figure 8.14 Photograph of fracture surfaces of A36 steel Charpy V-notch specimens<br />

tested at indicated temperatures (in C). (From R. W. Hertzberg, Deformation and Fracture<br />

Mechanics of Engineering Materials, 3rd <strong>edition</strong>, Fig. 9.6, p. 329. Copyright © 1989 by John<br />

Wiley & Sons, Inc., New York. Reprinted by permission of John Wiley & Sons, Inc.)

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