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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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González, E. V.
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (10/10 displayed)
- 2024A novel methodology to measure the transverse Poisson’s ratio in the elastic and plastic regions for composite materialscitations
- 2022A three-dimensional plastic-damage model for polymer composite materialscitations
- 2014Comment to the paper 'Analysis of progressive matrix cracking in composite laminates ii. first ply failure' by george j dvorak and norman lawscitations
- 2014Effects of interply hybridization on the damage resistance and tolerance of composite laminatescitations
- 2012Simulation of drop-weight impact and compression after impact tests on composite laminatescitations
- 2011Effects of ply clustering in laminated composite plates under low-velocity impact loadingcitations
- 2011Effects of ply clustering in laminated composite plates under low-velocity impact loading
- 2009Simulation of delamination by means of cohesive elements using an explicit finite element code
- 2009Low-velocity impact damage on dispersed stacking sequence laminates. Part II: Numerical simulationscitations
- 2007Composite skin-stiffener virtual testing
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article
Effects of interply hybridization on the damage resistance and tolerance of composite laminates
Abstract
This paper presents an experimental study of the drop-weight impact response of interply hybrid laminates manufactured using polymer-matrix composite materials. Three different reinforcements, woven carbon fabric, woven glass fabric and unidirectional carbon tape, are combined with an epoxy resin using the Resin Transfer Molding (RTM) process. In-plane quasi-isotropic laminates are analyzed by combining pairs of materials and by changing their location in the through-the-thickness direction of the laminate. In addition, different impact configurations defined in terms of impact energy are performed to increase the number of case studies. The analysis is completed by non-destructive inspections based on ultrasonic technique and Compression After Impact (CAI) tests for the assessment of the residual strength. The results obtained highlight the effects of interply carbon and glass hybridization under low-velocity impact and CAI loading.