| 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 |
|
Furtado, Carolina
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (24/24 displayed)
- 2023A design methodology of composite scarf repairs using artificial intelligencecitations
- 2022MODE I CRACK PATH TRANSITIONS IN UNIDIRECTIONAL CARBON FIBRE COMPOSITES ANALYSED USING IN SITU 3D COMPUTED TOMOGRAPHY AND THE EXTENDED FINITE ELEMENT METHOD
- 2022In Situ Synchrotron X-ray Microtomography of Progressive Damage in Canted Notched Cross-Ply Composites with Interlaminar Nanoreinforcementcitations
- 2022Evaluation of digital volume correlation (DVC) applicability in silicon dioxide (SiO2) particle-doped carbon fibre reinforced polymers using in situ synchrotron radiation computed tomography (SRCT)
- 2021Modelling damage in multidirectional laminates subjected to multi-axial loadingcitations
- 2021A methodology to generate design allowables of composite laminates using machine learningcitations
- 2021A methodology to generate design allowables of composite laminates using machine learningcitations
- 2021Modelling damage in multidirectional laminates subjected to multi-axial loading:ply thickness effects and model assessmentcitations
- 2021In situ synchrotron computed tomography study of nanoscale interlaminar reinforcement and thin-ply effects on damage progression in composite laminatescitations
- 2020Is there a ply thickness effect on the mode I intralaminar fracture toughness of composite laminates?citations
- 2020Thin-ply polymer composite materials: a reviewcitations
- 2020Interlaminar to intralaminar mode I and II crack bifurcation due to aligned carbon nanotube reinforcement of aerospace-grade advanced compositescitations
- 2019Static and fatigue interlaminar shear reinforcement in aligned carbon nanotube-reinforced hierarchical advanced compositescitations
- 2019Simulation of failure in laminated polymer composites: building-block validationcitations
- 2019Damage micro-mechanisms in notched hierarchical nanoengineered thin-ply composite laminates studied by in situ synchrotron x-ray microtomographycitations
- 2019Virtual calculation of the B-value allowables of notched composite laminatescitations
- 2019A micro-mechanics perspective to the invariant-based approach to stiffnesscitations
- 2018Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminatescitations
- 2017Prediction of size effects in open-hole laminates using only the Young's modulus, the strength, and the R-curve of the 0 degrees plycitations
- 2017Interlaminar reinforcement of carbon fiber composites using aligned carbon nanotubes
- 2017Damage modelling of thin-ply nano-reinforced composite laminates
- 2017Synergetic effects of thin ply and nanostitching studied by synchrotron radiation computed tomography
- 2016Selective ply-level hybridisation for improved notched response of composite laminatescitations
- 2016Selective ply-level hybridisation for improved notched response
Places of action
| Organizations | Location | People |
|---|
article
Simulation of failure in laminated polymer composites: building-block validation
Abstract
The development of numerical tools to complement the experimental determination of structural design parameters is of key importance to hasten the certification process of new materials and structures. In this work, a methodology to simulate elastic and inelastic deformation of composite laminates at the subcomponent level based on finite element analysis is proposed. A modified version of a continuum damage model proposed in the literature combined with a frictional cohesive zone model is used to capture the intralaminar and interlaminar damage and failure of composite laminates in general loading conditions. The methodology is validated for three aerospace-grade carbon fibre reinforced (epoxy) polymer composite material systems and coupon configurations with increasing level of complexity, including unnotched tension/compression, open-hole tension/compression and filled hole compression. The predictions obtained are in good agreement with the experimental results for all the test cases, oftentimes within the standard error of the tests, with a maximum relative error of 13%.