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Callister - An introduction - 8th edition

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242 • Chapter 8 / Failure<br />

nature of the grains may be seen. This type of fracture normally results subsequent<br />

to the occurrence of processes that weaken or embrittle grain boundary<br />

regions.<br />

8.5 PRINCIPLES OF FRACTURE MECHANICS<br />

Brittle fracture of normally ductile materials, such as that shown in the chapteropening<br />

photograph (of the oil barge) for this chapter, has demonstrated the need<br />

fracture mechanics<br />

for a better understanding of the mechanisms of fracture. Extensive research<br />

endeavors over the past century have led to the evolution of the field of fracture<br />

mechanics. This subject allows quantification of the relationships between material<br />

properties, stress level, the presence of crack-producing flaws, and crack propagation<br />

mechanisms. Design engineers are now better equipped to anticipate, and thus<br />

prevent, structural failures. The present discussion centers on some of the fundamental<br />

principles of the mechanics of fracture.<br />

Stress Concentration<br />

The measured fracture strengths for most materials are significantly lower than<br />

those predicted by theoretical calculations based on atomic bonding energies.<br />

This discrepancy is explained by the presence of microscopic flaws or cracks that<br />

always exist under normal conditions at the surface and within the interior of a<br />

body of material. These flaws are a detriment to the fracture strength because<br />

an applied stress may be amplified or concentrated at the tip, the magnitude of<br />

this amplification depending on crack orientation and geometry. This phenomenon<br />

is demonstrated in Figure 8.8, a stress profile across a cross section containing<br />

an internal crack. As indicated by this profile, the magnitude of this<br />

localized stress diminishes with distance away from the crack tip. At positions<br />

far removed, the stress is just the nominal stress 0 , or the applied load divided<br />

s 0<br />

s m<br />

r t<br />

s 0<br />

a<br />

Stress<br />

X<br />

X'<br />

x 2a<br />

x'<br />

s 0<br />

x<br />

x'<br />

(a)<br />

Position along X–X'<br />

(b)<br />

Figure 8.8 (a) The geometry of surface and internal cracks. (b) Schematic stress profile<br />

along the line X–X in (a), demonstrating stress amplification at crack tip positions.

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