Abstract Compression After Impact (CAI) strength is critical to the safety and weight of carbon fibre aircraft. In this paper, the standard aerospace industry practice of using separate …
This work aims to evaluate the critical buckling load of panels made of cross-laminated timber, considering finite element simulations and different analytical methods of calculating …
A multiscale extension for a parallel noninvasive mixed domain decomposition method is presented. After briefly exposing our noninvasive implementation of the Latin method, we …
G Guguin, O Allix, P Gosselet, S Guinard - Advanced Modeling and …, 2016 - Springer
Most large engineering structures are described as assemblies of plates and shells and they are computed as such using adhoc Finite Element packages. In fact their computation in 3D …
A non-invasive implementation of the Latin domain decomposition method for frictional contact problems is described. The formulation implies to deal with mixed (Robin) conditions …
M Wangermez, O Allix, PA Guidault, O Ciobanu… - Computer Methods in …, 2020 - Elsevier
This paper proposes a coupling strategy between a homogeneous macroscopic description of a structure and a description at a lower scale of some local details. In order to facilitate its …
The paper is focussed on the robustness of parallel computation in the case of buckling and post-buckling analyses. In the nonlinear context, domain decomposition methods are mainly …
A Nuñez-Labielle, J Cante, AE Huespe… - Computer Methods in …, 2022 - Elsevier
The work explores the computational modeling of propagating shocks in hyperelastic materials to be considered in the context of numerical analysis and design of mechanical …
This paper is devoted to the study of a micro–macro LaTIn-based Domain Decomposition Method for which the partitioning, the geometry and the boundary conditions play a major …