A plate model for compressive strength prediction of delaminated composites
- Submitting institution
-
The University of Bath
- Unit of assessment
- 12 - Engineering
- Output identifier
- 196622087
- Type
- D - Journal article
- DOI
-
10.1016/j.compstruct.2018.11.066
- Title of journal
- Composite Structures
- Article number
- -
- First page
- 509
- Volume
- 210
- Issue
- -
- ISSN
- 0263-8223
- Open access status
- Compliant
- Month of publication
- November
- Year of publication
- 2018
- URL
-
-
- Supplementary information
-
https://ars.els-cdn.com/content/image/1-s2.0-S0263822318318920-mmc1.xml
- 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
-
3
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- The paper led to the award of €9k travel grant by DFG (German research council) for Butler and Rhead to collaborate with University of Berlin. The results have been used by GKN to extrapolate design strains from thick to thin winglet skins on Bombardier C-Series wing, supported by limited testing (contact: former Stress Technical Authority, GKN Aerospace).
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -