Abstract
This research predicted multi-material adhesively bonded joints' structural responses (eigenvalue responses and strain energy release rates, SERR). The study includes the adhesive bonding between aluminium alloy (AA2014-T6) and glass fibre-reinforced polymer (GFRP). The numerical analyses are performed in a commercial finite element tool (ABAQUS) platform using the virtual crack closer technique (VCCT) for various scenarios (intact structures, delamination, cracks, and a combination of delamination with crack). A circular delamination with a 10 mm radius 'R' and a 10 mm length crack 'l' with a 0.2 mm radius of curvature 'Rc' is induced in the GFRP adherend middle layer using node-to-surface constraints. The model accuracy has been validated by comparing the current prediction with those of published data and experimental values. The study also explores the influence of boundary conditions with different fibre layup orientations, adhesive thickness ratios, and variations in fibre layup and crack orientations. The study indicates that cross-ply fibre orientation in the polymer adherend consistently outperforms, increasing overlap length. Additionally, the SERR values are higher at 90° and 270°, with the [0°]2S orientation excelling for a combined damage case (delamination with an inclined crack), producing higher SERR values than longitudinal and transverse cracks, regardless of fibre orientation.
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Abbreviations
- ADC:
-
Analogue to digital converter
- ANN:
-
Artificial neural network
- c-DAQ:
-
Compact data acquisition
- CFCF:
-
Clamped-free-clamped-free condition
- CFFF:
-
Clamped-free-free-free condition
- FEA:
-
Finite element analysis
- FEM:
-
Finite element method
- FMLs:
-
Fibre metal laminates
- FFT:
-
Fast Fourier transform
- FRP:
-
Fibre-reinforced polymer
- GFRP:
-
Glass fibre-reinforced polymer
- MMB:
-
Multi-material bond
- MPC:
-
Multi-point constraint
- NDT:
-
Non-destructive testing
- SERR:
-
Strain energy release rate
- SLJ:
-
Single lap joint
- VCCT:
-
Virtual crack closure technique
- \(\left[ M \right]\) and \(\left[ K \right]\) :
-
Mass and Stiffness matrices
- \(x\left( t \right)\) :
-
Nodal displacement
- \(\ddot{x}\left( t \right)\) :
-
Nodal acceleration
- \(\left\{ {\overline{x}} \right\}\) :
-
Eigenvector
- \(\lambda\) :
-
Eigenvalue
- \(\omega\) :
-
Natural frequency
- \(\left\{ P \right\}\) :
-
Static load
- G I :
-
Strain energy release rate in Mode-I
- G II :
-
Strain energy release rate in Mode-II
- G III :
-
Strain energy release rate in Mode-III
- L :
-
Length of adherend
- W :
-
Breadth of adherend and adhesive
- t :
-
Thickness of adherend
- a :
-
Length of adhesive
- h :
-
Thickness of adhesive
- L o :
-
Overlapping length
- Lc :
-
Clamping length
- a/h :
-
Adhesive bond thickness ratio
- R :
-
Radius of delamination
- R c :
-
Crack radius of curvature
- L :
-
Length of the crack
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Akkasali, N.K., Biswas, S. & Panda, S.K. Damage (delamination and crack) effect on frequency and strain energy release rate (SERR) in adhesively bonded multi-material single lap joint—an experimental verification. Acta Mech 235, 1271–1290 (2024). https://doi.org/10.1007/s00707-023-03807-9
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DOI: https://doi.org/10.1007/s00707-023-03807-9