1. 3D application of the coupled criterion to crack initiation prediction in epoxy/aluminum specimens under four point bending
- Author
-
Aurélien Doitrand, Dominique Leguillon, Safran Aircraft Engines, Institut Jean Le Rond d'Alembert (DALEMBERT), Sorbonne Université (SU)-Centre National de la Recherche Scientifique (CNRS), Matériaux, ingénierie et science [Villeurbanne] (MATEIS), Université Claude Bernard Lyon 1 (UCBL), Université de Lyon-Université de Lyon-Institut National des Sciences Appliquées de Lyon (INSA Lyon), Université de Lyon-Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA)-Centre National de la Recherche Scientifique (CNRS), and Université Pierre et Marie Curie - Paris 6 (UPMC)-Centre National de la Recherche Scientifique (CNRS)
- Subjects
Materials science ,Bending ,chemistry.chemical_element ,02 engineering and technology ,Stress (mechanics) ,[SPI]Engineering Sciences [physics] ,0203 mechanical engineering ,Aluminium ,[SPI.MECA.MEMA]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph] ,Bimaterial ,General Materials Science ,Composite material ,ComputingMilieux_MISCELLANEOUS ,Strain energy release rate ,Crack ,Applied Mathematics ,Mechanical Engineering ,Fracture mechanics ,[PHYS.MECA]Physics [physics]/Mechanics [physics] ,Epoxy ,[SPI.MECA]Engineering Sciences [physics]/Mechanics [physics.med-ph] ,021001 nanoscience & nanotechnology ,Condensed Matter Physics ,Finite element method ,Fracture ,020303 mechanical engineering & transports ,chemistry ,Mechanics of Materials ,Modeling and Simulation ,visual_art ,Fracture (geology) ,visual_art.visual_art_medium ,Energy release rate ,0210 nano-technology - Abstract
International audience; Until now, the coupled stress and energy criterion has mainly been used in 2D applications, but it is possible to extend it to a 3D case. Herein the crack initiation in epoxy/aluminum bimaterial specimens under four point bending is predicted through a 3D numerical application of the coupled criterion. The stress and the energy conditions are computed by means of 3D finite element modeling of both undamaged and cracked specimens. The crack initiates at the epoxy/aluminum interface, meshes of the cracked specimens take into account the crack topology which is determined using the interface normal stress isocontours. By indirect confrontation to experimental tests on aluminum/epoxy bimaterial specimens of different width, the proposed approach allows determining the interface strength and fracture energy. The blind application of the proposed method to a crack initiation in aluminum/epoxy/aluminum specimens of different epoxy layer thickness under four point bending leads to a reasonable agreement with experimental data.
- Published
- 2018
- Full Text
- View/download PDF