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 |
|
Mayugo, Ja
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (9/9 displayed)
- 2019An analytical model to predict stress fields around broken fibres and their effect on the longitudinal failure of hybrid compositescitations
- 2018A methodology to simulate low velocity impact and compression after impact in large composite stiffened panelscitations
- 2012Simulation of drop-weight impact and compression after impact tests on composite laminatescitations
- 2011Matrix cracking and delamination in laminated composites. Part I: Ply constitutive law, first ply failure and onset of delaminationcitations
- 2011Matrix cracking and delamination in laminated composites. Part II: Evolution of crack density and delaminationcitations
- 2010Analytical Modelling of Transverse Matrix Cracking of [+/-theta/90(n)](s) Composite Laminates under Multiaxial Loadingcitations
- 2008A three-dimensional damage model for transversely isotropic composite laminatescitations
- 2007A continuum damage model for composite laminates: Part I - Constitutive modelcitations
- 2007A continuum damage model for composite laminates: Part II - Computational implementation and validationcitations
Places of action
Organizations | Location | People |
---|
article
A continuum damage model for composite laminates: Part II - Computational implementation and validation
Abstract
This papers describes the computational implementation of a new damage model for laminated composites proposed in a previous paper. The objectivity of the numerical solution is assured by regularizing the energy dissipated at a material point by each failure mechanism. A viscous model is proposed to mitigate the convergence difficulties associated with strain softening constitutive models. To verify the accuracy of the approach, analyses of coupon specimens were performed, and the numerical predictions were compared with experimental data.