A novel process-linked assembly failure model for adhesively bonded composite structures
- Submitting institution
-
City, University of London
- Unit of assessment
- 12 - Engineering
- Output identifier
- 1309
- Type
- D - Journal article
- DOI
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10.1016/j.cirp.2017.04.103
- Title of journal
- CIRP Annals - Manufacturing Technology
- Article number
- -
- First page
- 29
- Volume
- 66
- Issue
- 1
- ISSN
- 0007-8506
- Open access status
- Compliant
- Month of publication
- April
- Year of publication
- 2017
- 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
- The article addresses internationally pioneering research in development of a probabilistic model that correlates process parameters’ variations to the mechanical performance of composite bonded assemblies. It has gained significant interested already from both the Commercial Aircraft Composites Repair Committee (CACRC) and the CMH-17 communities, two major committees for composite repair and general composite handbook, respectively. A numerical tool based on the proposed model has been developed and its data is available open-access. This package has been widely downloaded and will help to improve standardization of failure models in aircraft design software
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -