Materials for engineering, 3rd Edition - (Malestrom)
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128<br />
<strong>Materials</strong> <strong>for</strong> <strong>engineering</strong><br />
initial painting operation and subsequent maintenance work. They have<br />
not been used extensively in the UK because frequent rain inhibits the<br />
<strong>for</strong>mation of the stable oxide layer and rusting continues (athough it is at<br />
a reduced rate). Long dry summer periods are desirable in order to develop<br />
the adherent oxide layer.<br />
3.4.3 Stress, strain and corrosion<br />
Both dry and wet corrosion may be exacerbated in the presence of applied<br />
stress or strain.<br />
Stress-corrosion cracking<br />
Stress-corrosion cracking (SCC) may appear as mechanical failure by cracking<br />
under circumstances where, in the absence of corrosion, no failure would<br />
have been expected. The stress may arise by external application or be present<br />
as a residual internal stress, and the corrosive medium is highly specific to<br />
each alloy. Under fluctuating stress, the phenomenon is known as corrosion<br />
fatigue. Some <strong>for</strong>m of surface pit must initially be <strong>for</strong>med, but there appears<br />
to be no common mechanism of crack propagation <strong>for</strong> all the different systems<br />
of alloys and corrodents that produce cracking. The rate of propagation of a<br />
stress-corrosion crack (da/dt) as a function of stress intensity (K) varies in<br />
the manner shown in the idealised curve of Fig. 2.21.<br />
At low K values, the crack velocity is highly K-dependent, becoming<br />
vanishingly small at K I SCC . Considerable experimental patience is required<br />
to establish the latter value, which may correspond to crack growth rates as<br />
low as 10 –11 m s –1 . There is a K-independent velocity plateau at intermediate<br />
values of K, and stage III in Fig. 2.21 shows a rapid acceleration as the value<br />
of K Ic is approached. It is striking that an aggressive environment can commonly<br />
reduce the value of K Ic by 95% down to that of K I SCC . The problem is<br />
normally tackled by metallurgical means, i.e. by modifying the composition<br />
of the alloy to increase its corrosion resistance, rather than by changing the<br />
state of stress or the environment.<br />
Hydrogen embrittlement<br />
Hydrogen embrittlement is a special case of SCC caused by absorbed hydrogen<br />
and it is particularly important <strong>for</strong> high-strength steels and aluminium alloys.<br />
There are numerous potential sources of hydrogen, including welding,<br />
electroplating and corrosive attack.<br />
In the case of ferritic steels, it has been suggested that dissolved hydrogen<br />
atoms can diffuse into internal cavities and recombine to <strong>for</strong>m hydrogen gas.<br />
The gas can exert an internal pressure to assist the fracture process. An