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Fatigue Crack Growth in 7050T7451 Aluminium Alloy Thick Section ...

Fatigue Crack Growth in 7050T7451 Aluminium Alloy Thick Section ...

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DSTO-TR-1477The largest cracks were found grow<strong>in</strong>g from all positions (sides, edges and corners up to about10mm either side of the centre of the specimen) from the specimen surface, although thepredom<strong>in</strong>ant position was at or near the external radii <strong>in</strong> the specimen edge (5”radius) as shown<strong>in</strong> Figure 13. Here an example of a ma<strong>in</strong> crack with two ma<strong>in</strong> regions of <strong>in</strong>itiation, both of whichare just with<strong>in</strong> the radius of the corner which was a favoured site for <strong>in</strong>itiation for many of thema<strong>in</strong> cracks. Although the corners were favoured as sites for <strong>in</strong>itiation, these corners had beenrounded with a 1 to 2mm radius to prevent them from be<strong>in</strong>g overly significant as <strong>in</strong>itiation sitesand to mimic the type of peen<strong>in</strong>g rework carried out on F/A-18 structure.Figure 13 Typical region of crack <strong>in</strong>itiation near a corner. This was the most common position for crack<strong>in</strong>itiation <strong>in</strong> these peened specimens. Note that the <strong>in</strong>itiation sites are not <strong>in</strong> the middle of thecurved section but closer to the transition region.The number of cracks that could be observed <strong>in</strong>tersect<strong>in</strong>g the fracture appeared to <strong>in</strong>creased withthe stress level and specimen life (at a particular stress level).The crack growth around the orig<strong>in</strong>s of the cracks, particularly the cracks which occurred <strong>in</strong> thespecimens loaded at the lower stress levels revealed considerable distortion of the normal crackfront shape. Some examples are shown <strong>in</strong> Figure 14. Typically the cracks <strong>in</strong>itially grew with alonger surface length than depth compared to cracks <strong>in</strong> the etched specimens (Barter, 2003), thenrapidly deepened result<strong>in</strong>g <strong>in</strong> a bulg<strong>in</strong>g out of the centre of the crack front. This is evident <strong>in</strong>Figure 14B. (The band<strong>in</strong>g <strong>in</strong> this Figure shows the repeat <strong>in</strong> the block load<strong>in</strong>g). The shape was tosome extent distorted <strong>in</strong> this manner due to the deepest po<strong>in</strong>t of the crack mov<strong>in</strong>g <strong>in</strong>to thematerial that is less affected by the residual stresses produced by the peen<strong>in</strong>g, while the rema<strong>in</strong>derof the crack fount is still affected by the residual stress. Odd shaped crack fronts can also occurdur<strong>in</strong>g crack<strong>in</strong>g from cold worked fastener holes, Clark, 1991.13

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