Publications

Multiscale 3D displacement field measurement using stereo digital image correlation on a fractal speckle pattern
Joël Serra, Renaud Lalanne, John Eric Dufour, Jean-Noel Périé and Jean-Charles Passieux
Strain, 2024
https://doi.org/10.1111/str.12479

Numerical simulations and testing of notched composite plates under envelope loadings : Validation with the safe life domain method
Florent Grotto, Christophe Bouvet, Bruno Castanié, and Joël Serra
Composite Structures, 2024
https://doi.org/10.1016/j.compstruct.2024.118191

Multiaxial loading of aeronautic composite structures at intermediate scale : A review of VERTEX developments
Bruno Castanié, Jean-Charles Passieux, Jean-Noel Périé, Christophe Bouvet,John-Eric Dufour and Joël Serra
Composite Part C : Open Access, 2024
https://doi.org/10.1016/j.jcomc.2024.100439

Testing Structural Elements under Multiaxial Loading : A Numerical Model of the Bench to Understand and Predict Complex Boundary Conditions
Florent Grotto, Oscar Peta, Christophe Bouvet, Bruno Castanié and Joël Serra
Aerospace, 2024
https://doi.org/10.3390/aerospace11010068

Experimental characterization of tensile and compressive translaminar fracture toughness coupling multiphysics measurements
Romain Rutar, Joël Serra, Quentin Bausiere and Christophe Bouvet
Engineering Fracture Mechanics, 2023
https://doi.org/10.1016/j.engfracmech.2023.109568

Monitoring structural scale composite specimens in a post‐buckling regime : The integrated finite element stereo digital image correlation approach with geometrically non‐linear regularization
John-Eric Dufour, Guillaume Colantonio, Christophe Bouvet, Jean-Noel Périé, Jean-Charles Passieux, Joël Serra
Strain, 2023
https://doi.org/10.1111/str.12450

Design and Testing of Impacted Stiffened CFRP Panels under Compression with the VERTEX Test Rig
Florent Grotto, Christophe Bouvet, Bruno Castanié, Joël Serra
Aerospace, 2023
https://doi.org/10.3390/aerospace10040327

Local buckling on large sandwich panels used in light aviation : Experimental and computation dialogue
Malo Ginot, Christophe Bouvet, Bruno Castanié, Michele d’Ottavio, Joël Serra, Nicolas Mahuet
International Journal of Solids and Structures, 2023
https://doi.org/10.1016/j.ijsolstr.2023.112170

Local buckling on large sandwich panels used in light aviation : Experimental setup and failure scenarios
Malo Ginot, Christophe Bouvet, Bruno Castanié, Joël Serra, Nicolas Mahuet
Composite Structures, 2023
https://doi.org/10.1016/j.compstruct.2022.116439

Experimental behaviour of aeronautical carbon fibre reinforced thermoplastic panels under combined tension-shear-pressure loadings
Florent Grotto, Christophe Bouvet, Bruno Castanié, Joël Serra
Engineering Failure Analysis, 2023
https://doi.org/10.1016/j.engfailanal.2023.107075

Combined loadings after medium velocity impact on large CFRP laminated plates : Discrete ply model simulations
J. Serra, A. Trellu, C. Bouvet, S. Rivallant, B. Castanié, L. Ratsifandrihana
Composites Part C : Open Access, 2021
https://doi.org/10.1016/j.jcomc.2021.100203

=== Related Publications ===

Combined loadings after medium velocity impact on large CFRP laminate plates : Tests and enhanced computation/testing dialogue
A. Trellu, G. Pichon, C. Bouvet, S. Rivallant, B. Castanié, J. Serra, L. Ratsifandrihana
Composites Science and Technology, 2020
https://doi.org/10.1016/j.compscitech.2020.108194

Validation and modeling of aeronautical composite structures subjected to combined loadings : The VERTEX project. Part 1 : Experimental setup, FE-DIC instrumentation and procedures
Joël Serra, J.E. Pierré, J.C. Passieux, J.N. Périé, Christophe Bouvet, Bruno Castanié
Composite Structures, 2017
https://doi.org/10.1016/j.compstruct.2017.07.080

Validation and modeling of aeronautical composite structures subjected to combined loadings : The VERTEX project. Part 2 : Load envelopes for the assessment of panels with large notches
Joël Serra, J.E. Pierré, J.C. Passieux, J.N Périé, Christophe Bouvet, Bruno Castanié, C. Petiot
Composite Structures, 2017
https://doi.org/10.1016/j.compstruct.2017.08.055