Damage modelling of carbon fibre composite crush tubes: numerical simulation and experimental validation of drop weight impact
File(s)Sommer et al - 2022.pdf (5.09 MB)
Published version
Author(s)
Type
Journal Article
Abstract
Angle-ply carbon fibre reinforced polymer (CFRP) crush tubes were tested in drop weight impact experiments.
High-fidelity computational modelling of the dynamic impact response was performed using explicit finite
element analysis in LS-DYNA. Ply-by-ply and fibre-aligned meshing was used for the composite lamina wherein
the intralaminar damage was treated with a 3D rate- and pressure-dependent continuum damage mechanics
(CDM) model, implemented as a user material. Delamination was modelled using cohesive tiebreak contacts to
deal with the mis-matched nodes caused by the use of a structured, fibre-aligned mesh. The material aligned
meshing scheme was shown to be required to capture the intralaminar splits observed in the ±45◦ plies.
The numerical predictions showed excellent correlation with experimental measurements in terms of both the
damage mechanisms and macroscopic material behaviour of the drop weight. In the simulation, interlaminar
friction between delaminated plies seemed to be a main contributor of energy dissipation. Parameter sensitivity
analysis showed that the interaction between the delamination fracture energy and friction can substantially
influence the results and stable crushing load, in particular. For the scenario studied here, a regular structured
mesh (unaligned) was shown to be insufficient for simulating realistic crack paths despite producing reasonable
predictions of the force–displacement and absorbed energy.
High-fidelity computational modelling of the dynamic impact response was performed using explicit finite
element analysis in LS-DYNA. Ply-by-ply and fibre-aligned meshing was used for the composite lamina wherein
the intralaminar damage was treated with a 3D rate- and pressure-dependent continuum damage mechanics
(CDM) model, implemented as a user material. Delamination was modelled using cohesive tiebreak contacts to
deal with the mis-matched nodes caused by the use of a structured, fibre-aligned mesh. The material aligned
meshing scheme was shown to be required to capture the intralaminar splits observed in the ±45◦ plies.
The numerical predictions showed excellent correlation with experimental measurements in terms of both the
damage mechanisms and macroscopic material behaviour of the drop weight. In the simulation, interlaminar
friction between delaminated plies seemed to be a main contributor of energy dissipation. Parameter sensitivity
analysis showed that the interaction between the delamination fracture energy and friction can substantially
influence the results and stable crushing load, in particular. For the scenario studied here, a regular structured
mesh (unaligned) was shown to be insufficient for simulating realistic crack paths despite producing reasonable
predictions of the force–displacement and absorbed energy.
Date Issued
2022-09-01
Date Acceptance
2022-06-03
Citation
Composites Part A: Applied Science and Manufacturing, 2022, 160
ISSN
1359-835X
Publisher
Elsevier
Journal / Book Title
Composites Part A: Applied Science and Manufacturing
Volume
160
Copyright Statement
© 2022 The Author(s). Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/
Identifier
https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000827237500003&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=a2bf6146997ec60c407a63945d4e92bb
Subjects
BEHAVIOR
CALIBRATION
Carbon fibre
CFRP TUBES
Composite laminate
Damage mechanics
Dynamic fracture
Engineering
Engineering, Manufacturing
FAILURE MODELS
High strain rate
IMPLEMENTATION
LOW-VELOCITY IMPACT
Materials Science
Materials Science, Composites
Numerical modelling
OPEN HOLE
PROGRESSIVE DAMAGE
REINFORCED COMPOSITES
Science & Technology
STRAIN-RATE
Technology
Publication Status
Published
Article Number
107033
Date Publish Online
2022-06-10