A Simplified Layered Beam Approach for Predicting Ply Drop Delamination in Thick Composite Laminates
- Submitting institution
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University of Bristol
- Unit of assessment
- 12 - Engineering
- Output identifier
- 198653578
- Type
- D - Journal article
- DOI
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10.1016/j.matdes.2016.06.105
- Title of journal
- Materials and Design
- Article number
- -
- First page
- 570
- Volume
- 108
- Issue
- -
- ISSN
- 0261-3069
- Open access status
- Compliant
- Month of publication
- July
- Year of publication
- 2016
- 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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2
- Research group(s)
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A - Advanced Composites Collaboration for Innovation & Science ACCIS
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- This paper presents for the first time a two-scale finite-element-based approach for designing tapered laminates that are resistant to delamination onset from ply drop-offs. The latter can cause interlaminar cracking in regions with thickness transitions. The work was funded via the UoB EPSRC "Impact Acceleration Account" (£130k), together with Rolls-Royce plc, as a follow-up activity of Dr Allegri's EPSRC first grant (EP/H040188/1 - £125k). The approach has been implemented as a custom plug-in to the commercial FE software Abaqus and transferred to Rolls-Royce, where it is employed for the design of composite aero engine components.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -