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Materials for engineering, 3rd Edition - (Malestrom)

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212<br />

<strong>Materials</strong> <strong>for</strong> <strong>engineering</strong><br />

10 –3<br />

da/dN (mm cycle –1 )<br />

10 –4<br />

10 –5<br />

PES<br />

L<br />

T<br />

Matrix<br />

20% wt% GF<br />

30% wt% GF<br />

direction<br />

0.5 0.6 0.7 0.8 0.9 1.0 1.5 2.0 2.5 3.0 3.5<br />

∆K 1 (MPa m 1/2 )<br />

6.22 Log(da/dN) versus log(∆K) curves of PES composites tested at a<br />

frequency of 5 Hz.<br />

with their volume fraction. It is also apparent that the effect of the fibres is<br />

greater <strong>for</strong> cracks growing normal to the mould fill direction than <strong>for</strong> those<br />

growing along the mould fill direction.<br />

The fatigue behaviour of a metal matrix composite is also usually superior<br />

to that of the unrein<strong>for</strong>ced matrix, particularly in the case of unidirectional<br />

fibre composite systems. Three types of S–N curves have been reported, as<br />

illustrated in Fig. 6.23, whose shape depends upon the mode of crack<br />

propagation. If the matrix crack grows in a direction perpendicular to the<br />

fibre axis, the sigmoidally-shaped S–N curve marked A is observed. If interfacial<br />

debonding takes place by the crack progressing in a direction parallel to the<br />

fibres and if the fibres are perfect, then the endurance limit will correspond<br />

to the static strength and the S–N curve will be horizontal (marked B). The<br />

majority of fibres will not be perfect, however, but will possess local weak<br />

points, so that a mixed type of fracture occurs and the S–N curve will be a<br />

mixture of types A and B.<br />

6.4.5 Environmental effects in fibre-rein<strong>for</strong>ced<br />

composites<br />

We have already discussed environmental effects upon metals and upon<br />

polymers. Most practical rein<strong>for</strong>cing fibres (with the possible exception of<br />

the aromatic polyamides such as Kevlar) are unlikely to be affected by

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