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In this paper, we have studied the induced residual stress due to the cold expanding of two adjacent holes.
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Corner crack initiated at the entrance face for cold expanded holes, while face crack initiated at the mid-plane of non-expanded holes.
Fatigue crack growth tests have been carried out at 20°C and 150°C for both cold expanded and non-cold expanded conditions.
Tests were carried out using plates containing plain holes and cold expanded holes in aluminium.
This result was attributed to the surface upset which was present in cold expanded holes.
A series of uniaxial fatigue tests were carried out using specimens containing non-cold expanded and cold expanded holes to assess the effect of split sleeve cold expansion on fatigue behavior of titanium alloy TC4.
In this paper a series of residual stress measurements and fatigue crack growth tests have been carried out using aluminium alloy 2650 specimens containing cold expanded and non cold expanded holes.
This paper has sought to investigate the fatigue behavior of cold expanded specimens after being subjected to bolt tightening.
Fatigue crack growth rates in specimens containing cold expanded fastener holes were affected significantly by elevated temperature exposure.
3D finite element models were also used to analyze the residual stress fields around cold expanded holes.
Nevertheless, cold expanded specimens are practically used in bolted and riveted connections possessing different fatigue behavior than open hole specimens.
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