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A comparative study on the failure criteria for predicting the damage initiation in fibre-reinforced composites

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J. Zheng et al_MCM_08-06-2021_Accepted.pdfAccepted version474.38 kBAdobe PDFView/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