Materials for engineering, 3rd Edition - (Malestrom)
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Determination of mechanical properties 51<br />
thick in order that most of the de<strong>for</strong>mation occurs under conditions of plane<br />
strain. Figure 2.11 illustrates the effect of specimen thickness on the measured<br />
value of the fracture toughness, K c : the fracture toughness can be halved as<br />
the stress conditions change from plane stress to plane strain with increasing<br />
specimen thickness. Once under plane strain, however, the value of the<br />
toughness becomes independent of the thickness and this value is referred to<br />
as K Ic , and is regarded as a material parameter. The corresponding value of<br />
G Ic may be calculated from equation [2.15].<br />
The two requirements of a relatively small plastic zone and plane strain<br />
conditions impose conditions upon the test-piece dimensions which have to<br />
be fulfilled in valid fracture toughness tests. These dimensions are always<br />
stated in the appropriate testing standards, e.g. BS 7448 (1991).<br />
In circumstances of extensive plasticity, an alternative toughness parameter<br />
has been proposed, namely the crack tip opening displacement (CTOD),<br />
usually given the symbol δ. The CTOD is obtained from the reading of a<br />
clip-gauge placed across the crack mouth and, under conditions of fracture,<br />
a critical value of δ c is determined. If the yield stress of the material is σ y , the<br />
toughness may then be obtained from the relation:<br />
G c = σ y δ c [2.18]<br />
2.6.1 The J integral<br />
There are types of material, e.g. elastomers, which behave in a non-linear<br />
elastic manner, i.e. their reversible stress–strain graph is curved. The energy<br />
Fracture toughness K c<br />
K lc<br />
Specimen thickness<br />
2.11 Change in fracture toughness with specimen thickness.