Effect on fatigue performance of residual stress induced via laser shock peening in mechanically damaged 2024-351 aluminium sheet
During manufacture and maintenance the fuselage skin of aircraft are susceptible to damage in the form of scratches. Normally not considered to be of major concern to aircraft structural integrity some airlines discovered fatigue cracks had initiated at the root of scratches. Crack propagation was i...
| Main Author: | |
|---|---|
| Other Authors: | |
| Published: |
Cranfield University
2014
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.659302 |