Abstract
The current study investigates the effect of foreign object damage (FOD) on the preexisting compressive residual stress field associated with laser shock peening (LSP) and its evolution upon combined LCF/HCF cycling. FOD was introduced onto an aerofoil-shaped specimen that had been previously LSP treated through ballistic impacts at angles of 0° and 45° to the leading edge. It is shown that the FOD notch created by 45° impact was asymmetric in shape and smaller in depth compared to that created at 0° impact. Significant through thickness compression was introduced parallel to the leading edge as a result of the LSP process. The residual strain distribution was mapped around the FOD notch by synchrotron X-ray radiation. The results show predominantly compressive stresses ahead of the notch, being greater for the 0° compared to 45° impact. No significant stress relaxation was observed after a combined (1000 HCF cycles superimposed on 1 LCF cycle) cycle.
Original language | English |
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Title of host publication | Mechanical Stress Evaluation by Neutrons and Synchrotron Radiation |
Publisher | Trans Tech Publications |
Pages | 19-24 |
Number of pages | 6 |
ISBN (Print) | 0878492585, 9780878492589 |
DOIs | |
Publication status | Published - 2010 |
Externally published | Yes |
Event | International Conference on Mechanical Stress Evaluation by Neutrons and Synchrotron Radiation (MECA SENS V) - Mito, Japan Duration: 10 Nov 2009 → 12 Nov 2009 Conference number: 5th |
Publication series
Name | Materials Science Forum |
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Volume | 652 |
ISSN (Print) | 0255-5476 |
ISSN (Electronic) | 1662-9752 |
Conference
Conference | International Conference on Mechanical Stress Evaluation by Neutrons and Synchrotron Radiation (MECA SENS V) |
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Abbreviated title | MECA SENS V |
Country/Territory | Japan |
City | Mito |
Period | 10/11/09 → 12/11/09 |
Keywords
- Foreign object damage (FOD)
- Laser Shock Peening (LSP)
- LCF/HCF
- Residual stress
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