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A comparative study on the failure criteria for predicting the damage initiation in fibre-reinforced composites
File | Description | Size | Format | |
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J. Zheng et al_MCM_08-06-2021_Accepted.pdf | Accepted version | 474.38 kB | Adobe PDF | View/Open |
Title: | A comparative study on the failure criteria for predicting the damage initiation in fibre-reinforced composites |
Authors: | Zheng, J Maharaj, C Liu, J Chai, H Liu, H Dear, J |
Item Type: | Journal Article |
Abstract: | In this research, a review is performed to explore the advantages and disadvantages of different failure criteria for fibre reinforced composites. Widely-used failure criteria, such as the Maximum stress criterion, Hashin criterion, Puck’s criterion, LaRC03 and Northwestern University (NU) criteria are reviewed based on the relevant literature. A comparison is performed of these failure criteria, using the analytical results obtained from a MATLAB programme and numerical results obtained from an Abaqus finite element model. The applicability and reliability of these failure criteria for predicting damage in thermoplastic laminates, i.e. AS4 carbon fibre reinforced Polyether-ether-ketone (PEEK), are evaluated based on the analytical and numerical results. Thenumerical results reveal that the Maximum Stress criterion provides the most conservative prediction, whilst the Hashin and Northwestern University (NU) criteria give reasonable and sensible results with an acceptable running time. Puck and LaRC03 criteria deliver more accurate predictions, but with longer running times. |
Issue Date: | 23-Mar-2022 |
Date of Acceptance: | 8-Jun-2021 |
URI: | http://hdl.handle.net/10044/1/90368 |
DOI: | 10.1007/s11029-022-10016-3 |
ISSN: | 1573-8922 |
Publisher: | Springer Verlag |
Start Page: | 125 |
End Page: | 140 |
Journal / Book Title: | Mechanics of Composite Materials |
Volume: | 58 |
Copyright Statement: | © 2022, Springer Science Business Media, LLC, part of Springer Nature. The final publication is available at Springer via https://link.springer.com/article/10.1007/s11029-022-10016-3 |
Sponsor/Funder: | AVIC Manufacturing Technology Institute Aircraft Strength Research Institute, AVIC |
Funder's Grant Number: | N/A MESM_P73327 |
Keywords: | Science & Technology Technology Physical Sciences Mechanics Materials Science, Composites Polymer Science Materials Science failure criteria composite laminates stress analysis analytical analysis finite-element analysis (FEA) THERMOPLASTIC COMPOSITE PROGRESSIVE FAILURE NONLINEAR BEHAVIOR STRENGTH CRITERIA CAPABILITY YIELD Materials |
Publication Status: | Published |
Appears in Collections: | Mechanical Engineering Faculty of Engineering |