Continuous debonding monitoring of a patch repaired helicopter stabilizer: damage assessment and analysis
- Submitting institution
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Sheffield Hallam University
- Unit of assessment
- 12 - Engineering
- Output identifier
- 2810
- Type
- D - Journal article
- DOI
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10.1016/j.compstruct.2015.03.014
- Title of journal
- Composite Structures
- Article number
- -
- First page
- 231
- Volume
- 127
- Issue
- -
- ISSN
- 0263-8223
- Open access status
- Out of scope for open access requirements
- Month of publication
- September
- Year of publication
- 2015
- URL
-
-
- Supplementary information
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-
- 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
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6
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- Funded by the EU 7th Framework Programme (“IAPETUS” project, total value: €3,342,226). This work was the result of the collaboration between 3 Universities and 7 aerospace companies. The project was coordinated by Tecnalia and was in collaboration with the University of Ioannina, the University of Sheffield, the University of Patras, Hellenic Aerospace Industry, pzl - Swidnik, Gmi Aero, Inasco Hellas, Huntsman and Daher Aerospace, resulting in novel repair technologies and hybrid materials that revolutionise aircraft repair processes.This paper looked at structural health monitoring of an aluminium vertical helicopter stabiliser with a pre-introduced crack repaired with an adhesively bonded composite patch,
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -