Numerical study of interface cracking in composite structures using a
novel geometrically nonlinear Linear Elastic Brittle Interface Model:
mixed-mode fracture conditions and application to structured interfaces
novel geometrically nonlinear Linear Elastic Brittle Interface Model:
mixed-mode fracture conditions and application to structured interfaces
File(s)2005.13315v1.pdf (1.92 MB)
Accepted version
Author(s)
García-Guzmán, L
Reinoso, J
Valverde, A
Martínez-Pañeda, E
Távara, L
Type
Journal Article
Abstract
Interface cracking is one of the most prominent failure modes in fibre
reinforced polymer (FRP) composites. Recent trends in high-tech applications of FRP composites exploit the limits of the load bearing capacity, generally encompassing the development of notable nonlinear effects from geometrical and material signatures. In this investigation, we present a comprehensive assessment of the new Linear Elastic Brittle Interface Model (LEBIM) in geometrically nonlinear applications undergoing mixed-mode fracture conditions. This interface model for triggering fracture events is formulated through the advocation of continuum-like assumptions (for initial non-zero interface thickness) and allows the incorporation of the potential role of the in-plane deformation effects. The performance of the present interface model is demonstrated through the simulation of specimens with mixed-mode delamination, with special attention for its application in samples equipped with structured interfaces. Current predictions exhibit an excellent agreement with respect to experimental data, validating the proposed methodology.
reinforced polymer (FRP) composites. Recent trends in high-tech applications of FRP composites exploit the limits of the load bearing capacity, generally encompassing the development of notable nonlinear effects from geometrical and material signatures. In this investigation, we present a comprehensive assessment of the new Linear Elastic Brittle Interface Model (LEBIM) in geometrically nonlinear applications undergoing mixed-mode fracture conditions. This interface model for triggering fracture events is formulated through the advocation of continuum-like assumptions (for initial non-zero interface thickness) and allows the incorporation of the potential role of the in-plane deformation effects. The performance of the present interface model is demonstrated through the simulation of specimens with mixed-mode delamination, with special attention for its application in samples equipped with structured interfaces. Current predictions exhibit an excellent agreement with respect to experimental data, validating the proposed methodology.
Date Issued
2020-09-15
Date Acceptance
2020-05-15
Citation
Composite Structures, 2020, 248
ISSN
0263-8223
Publisher
Elsevier
Journal / Book Title
Composite Structures
Volume
248
Copyright Statement
© 2020 Elsevier Ltd. All rights reserved. This manuscript is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International Licence http://creativecommons.org/licenses/by-nc-nd/4.0/
Identifier
http://arxiv.org/abs/2005.13315v1
Subjects
cond-mat.mtrl-sci
cond-mat.mtrl-sci
cs.NA
math.NA
Notes
Composite Structures (2020)
Publication Status
Published
Article Number
ARTN 112495
Date Publish Online
2020-05-22