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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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Achintha, Mithila
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (17/17 displayed)
- 2024Glass–GFRP Laminate: A Proof of Concept Experimental Investigationcitations
- 2023Exploration of Waste Glass Powder as Partial Replacement of Cement in Concretecitations
- 2022Glass–GFRP Sandwich: Structurally Superior Laminated Glass
- 2020Development of cohesive zone models for the prediction of damage and failure of glass/steel adhesive jointscitations
- 2019Failure prediction and optimal selection of adhesives for glass/steel adhesive jointscitations
- 2018Strength evaluation and failure prediction of bolted and adhesive glass/steel jointscitations
- 2016A review on design, manufacture and mechanics of composite riserscitations
- 2015An CFRP fabrics as internal reinforcement in concrete beams
- 2015An experimentally validated contour method/eigenstrains hybrid model to incorporate residual stresses in glass structural designscitations
- 2015Experimental and numerical investigation of residual stress relaxation in shot-peened notch geometries under low-cycle fatigue
- 2014Fatigue behaviour of geometric features subjected to laser shock peeningcitations
- 2014Hybrid contour method/eigenstrain model for predicting residual stress in glass
- 2012Fatigue behaviour of geometric features subjected to laser shock peening
- 2012Fatigue behaviour of geometric features subjected to laser shock peening:9th Fatigue Damage of Structural Materials Conference
- 2012Prediction of FRP debonding Using the global-energy-balance approach
- 2011Optimising LSP conditions and modelling the geometric effects on residual stress
- 2009Fracture mechanics of plate debonding
Places of action
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conferencepaper
Fatigue behaviour of geometric features subjected to laser shock peening
Abstract
The current paper reports selected findings from a major collaborative research programme conducted in the United Kingdom into the fundamental understanding of laser shock peening, when applied to key airframe and aero-engine alloys as a means of controlling fatigue performance.It is recognised that relatively deep compressive residual stresses are generated into the surface of a material subjected to LSP which can subsequently resist fatigue crack initiation from that surface. However, it is clear that balancing tensile stress will evolve at some location within the material in order to satisfy equilibrium and under certain circumstances this can lead to sub-surface fatigue initiation. The distribution of the RS field will be highly dependent on LSP process parameters, the structural form and the precise mode and raster pattern of pulse application.Finite element models will be described that predict the RS fields associated with LSP applied to the aerospace grade aluminium alloys Al 2024 and Al 7010 using an eigenstrain approach. Validation of these models is provided by laboratory fatigue experiments on test coupons containing different LSP patch geometries (full width or centre constrained), supplementary stress raising features (drilled holes) and different through thickness dimensions. Particular attention is paid to modelling the application of LSP at edge locations in terms of the angle of incidence and laser pulse sequencing. Interactions between the LSP process and geometric features was found to be key to understanding the location for fatigue crack initiation. Particularly relevant for engineering application, was the fact that not all instances of LSP application provided an improvement in cyclic fatigue life.