People | Locations | Statistics |
---|---|---|
Naji, M. |
| |
Motta, Antonella |
| |
Aletan, Dirar |
| |
Mohamed, Tarek |
| |
Ertürk, Emre |
| |
Taccardi, Nicola |
| |
Kononenko, Denys |
| |
Petrov, R. H. | Madrid |
|
Alshaaer, Mazen | Brussels |
|
Bih, L. |
| |
Casati, R. |
| |
Muller, Hermance |
| |
Kočí, Jan | Prague |
|
Šuljagić, Marija |
| |
Kalteremidou, Kalliopi-Artemi | Brussels |
|
Azam, Siraj |
| |
Ospanova, Alyiya |
| |
Blanpain, Bart |
| |
Ali, M. A. |
| |
Popa, V. |
| |
Rančić, M. |
| |
Ollier, Nadège |
| |
Azevedo, Nuno Monteiro |
| |
Landes, Michael |
| |
Rignanese, Gian-Marco |
|
Partridge, Ivana K.
University of Bristol
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (25/25 displayed)
- 2024Effects of accelerated curing in thermoplastic particle interleaf epoxy laminatescitations
- 2019Coupon scale Z-pinned IM7/8552 delamination tests under dynamic loadingcitations
- 2019Effective use of metallic Z-pins for composites' through-thickness reinforcementcitations
- 2018COUPON SCALE MODELLING OF THE BRIDGING MECHANICS OF HIGH-RATE LOADED Z-PINS
- 2018Dynamic bridging mechanisms of through-thickness reinforced composite laminates in mixed mode delaminationcitations
- 2018Evaluating Z-pin performance under high-velocity impact conditions
- 2017Dynamic bridging mechanisms of through-thickness reinforced composite laminates in mixed mode delaminationcitations
- 2016Understanding and prediction of fibre waviness defect generation
- 2016Use of microfasteners to produce damage tolerant composite structurescitations
- 2016On the delamination self-sensing function of Z-pinned composite laminatescitations
- 2016Developing cure kinetics models for interleaf particle toughened epoxies
- 2015Delamination resistance of composites using inclined Z-pins
- 2012Finite element modelling of z-pinned composite T-jointscitations
- 2012Cure kinetics, glass transition temperature development, and dielectric spectroscopy of a low temperature cure epoxy/amine systemcitations
- 2012RTM processing and electrical performance of carbon nanotube modified epoxy/fibre compositescitations
- 2012RTM processing and electrical performance of carbon nanotube modified epoxy/fibre compositescitations
- 2010Percolation threshold of carbon nanotubes filled unsaturated polyesterscitations
- 2010Toward a constitutive model for cure-dependent modulus of a high temperature epoxy during the curecitations
- 2009Monitoring Cure in Epoxies Containing Carbon Nanotubes with an Optical-Fiber Fresnel Refractometercitations
- 2009Dielectric monitoring of carbon nanotube network formation in curing thermosetting nanocompositescitations
- 2009Monitoring dispersion of carbon nanotubes in a thermosetting polyester resincitations
- 2008Thermomechanical analysis of a toughened thermosetting system
- 2008Thermomechanical analysis of a toughened thermosetting system.citations
- 2007Exploring mechanical property balance in tufted carbon fabric/epoxy composites.citations
- 2004Inverse heat transfer for optimization and on-line thermal properties estimation in composites curing.citations
Places of action
Organizations | Location | People |
---|
article
Finite element modelling of z-pinned composite T-joints
Abstract
This paper presents a finite element model (FEM) to analyse the structural deformation, strength properties and delamination fracture behaviour of composite T-joints reinforced with z-pins. The FE modelling involves multi-level analysis of a pinned joint using unit cell and macro-scale structural models. Unit cell model is used to calculate the crack bridging traction loads generated by the elastic and interfacial friction (pull-out) stresses of a single pin within a representative unit cell of the joint. Macro-scale analysis involves modelling delamination crack growth in the pinned joint using a cohesive zone model, which is based on the traction load analysis of a single pin. The FE model was validated using experimental results for a pinned carbon fibre/epoxy T-joint subjected to tensile (stiffener pull-off) loading. The model accurately calculated the crack initiation load, ultimate load, and fracture mode of the pinned joint.