Finite element simulation of carbon fibre-reinforced composite laminates subjected to low velocity impact using damage induced static load-deflection methodology
- Submitting institution
-
The University of Bolton
- Unit of assessment
- 12 - Engineering
- Output identifier
- 0049_12_REF2_PM_02
- Type
- D - Journal article
- DOI
-
10.1016/j.tws.2015.09.008
- Title of journal
- Thin-Walled Structures
- Article number
- -
- First page
- 63
- Volume
- 97
- Issue
- -
- ISSN
- 0263-8231
- Open access status
- Out of scope for open access requirements
- Month of publication
- December
- Year of publication
- 2015
- URL
-
https://doi.org/10.1016/j.tws.2015.09.008
- 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
-
-
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- This paper proposes a new methodology for estimating the behaviour of aerospace composites under low velocity impact by using pre assumed damage zones corresponding to the impactor shape and deflection profile. This new approach offers a much reduced computational time.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -
