Residual stresses due to foreign object damage in laser-shock peened aerofoils: Simulation and measurement
- Submitting institution
-
University of Portsmouth
- Unit of assessment
- 12 - Engineering
- Output identifier
- 7138341
- Type
- D - Journal article
- DOI
-
10.1016/j.mechmat.2014.12.001
- Title of journal
- Mechanics of Materials
- Article number
- -
- First page
- 78
- Volume
- 82
- Issue
- -
- ISSN
- 0167-6636
- Open access status
- Out of scope for open access requirements
- Month of publication
- March
- Year of publication
- 2015
- URL
-
-
- Supplementary information
-
-
- Request cross-referral to
- -
- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
-
4
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- This paper reported the research outcome from an EPSRC funded collaborative project (EP_E05658X_1) with partners including the University of Manchester, QinetiQ and Rolls-Royce plc. Synchrotron X-ray was used to map the residual stress and its evolution during fatigue for the first time, whilst finite element analysis was used to simulate the experimental results. The research spurred further studies in this cutting-edge area for aerospace research, notably by Wu et al, Eng Fract Mech, 2017; Wang et al, Mech Mater, 2017; Faisal et al, Exp Mech 2018 and Farahani et al, Int J Damage Mech, 2018.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -