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Investigation of mode III fracture behaviour in bonded pultruded GFRP composite joints
- Publication Year :
- 2017
-
Abstract
- In this work, a numerical-experimental characterization of pure mode III fracture toughness of bonded pultruded fibreglass composite joints is presented. Three types of specimen were considered, which differ for the fibres orientation of the bonded surfaces. The analysed angular orientations are: parallel (0 degrees-0 degrees), inclined (0 degrees-45 degrees), and perpendicular (0 degrees-90 degrees). The experimental investigation was realized by using the recently proposed torque shells test (TST). Numerical analyses, based on Finite Element Method (FEM), were performed in order to model a cohesive law of the adhesive interface. A minimization algorithm was also used for identification of cohesive zone model (CZM) parameters by comparing numerical and experimental outcomes. The results show how the TST provides with an almost pure mode III fracture loading condition when the adherends are non-isotropic materials. The comparison of experimental and numerical torque-angle curves, for every test case, shows a satisfactory agreement. As a result of the analyses, the influence of fibres direction on the mode III fracture behaviour of pultruded GFRP joints can be considered negligible for practical applications.
- Subjects :
- Materials science
Composite number
Ceramics and Composite
02 engineering and technology
Glass fibre
Industrial and Manufacturing Engineering
Fracture toughness
0203 mechanical engineering
Debonding
CZM
Finite element analysis (FEA)
Glass fibres
Mechanical testing
Ceramics and Composites
Mechanics of Materials
Mechanical Engineering
Mechanics of Material
Composite material
business.industry
Structural engineering
Fibre-reinforced plastic
021001 nanoscience & nanotechnology
Finite element method
Cohesive zone model
020303 mechanical engineering & transports
Pultrusion
Fracture (geology)
Adhesive
0210 nano-technology
business
Subjects
Details
- Language :
- English
- Database :
- OpenAIRE
- Accession number :
- edsair.doi.dedup.....d66ea275c3e8e14eb569bad183b089c6