Residual stress and fatigue crack growth life prediction in fastener holes cold-worked by uniform indentation in 2024-T351 aluminium alloy
This thesis concerns primarily the residual stress characterisation in fastener holes cold worked by a novel StressWave process, and the prediction of the fatigue crack growth under the influence of such residual stress. Aerospace 2024-T351 aluminium alloy plate of 6.35mm thickness containing a nomi...
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Open University
2007
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.500610 |