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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Kazancı, Zafer
Queen's University Belfast
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (16/16 displayed)
- 2024Investigation of delamination characteristics in 3D-printed hybrid curved composite beamscitations
- 2024Development of a new progressive damage model for woven fabric compositescitations
- 2024Development of a new progressive damage model for woven fabric compositescitations
- 2024Finite fracture mechanics fracture criterion for free edge delamination
- 2023A three-dimensional Finite Fracture Mechanics model for predicting free edge delamination
- 2023Compressive characterisation of 3D printed composite materials using continuous fibre fabricationcitations
- 2023Three-dimensional semi-analytical investigation of interlaminar stresses in composite laminates
- 2023Tension and compression properties of 3D-printed composites: print orientation and strain rate effectscitations
- 2023A semi-analytical method for measuring the strain energy release rates of elliptical cracks
- 2023Predicting filling efficiency of composite resin injection repaircitations
- 2023Delamination strength comparison of additively manufactured composite curved beams using continuous fiberscitations
- 2023Investigation of several impact angles for predicting bird-strike damage in a riveted eVTOL composite wing
- 2022Comparison of different quasi-static loading conditions of additively manufactured composite hexagonal and auxetic cellular structurescitations
- 2020Crushing Investigation of Crash Boxes Filled with Honeycomb and Re-entrant (auxetic) Latticescitations
- 2012The Nonlinear Dynamic Behaviour of Tapered Laminated Plates Subjected to Blast Loadingcitations
- 2012Friction and wear behaviors of aircraft brake linings materialcitations
Places of action
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document
A semi-analytical method for measuring the strain energy release rates of elliptical cracks
Abstract
In this study, a fracture mechanics analysis is presented to address the concern of delamination propagation at the interface of a bi-material laminate. In general, the energy release rate at the crack front is the fracture parameter required to study the propagation of cracks. A new three-dimensional finite element technique, for the evaluation of the energy release rate along the interfacial semi-elliptical crack front in hybrid composite-metal substrates, is presented. Using a non-dimensional correction factor, the related equation expresses the normalized energy release rate. A non-dimensional function with non-dimensionalized functional groups is utilized to investigate the effects of several factors. These factors include the variation in material stiffness between layers, the relative thickness of the two substrates at whose interface the analysis is performed, and the effects of two semi-axes of a semielliptical crack on the analysis of the correction factor. These non-dimensional function values were derived by employing a careful interpolation technique on a set of finite element solutions, yielding predictions that exhibit accuracy within acceptable range of numerical results.<br/><br/>