| People | Locations | Statistics |
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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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Alderliesten, René
Delft University of Technology
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (44/44 displayed)
- 2024A new interpretation of mode I interlaminar fracture in layered materialscitations
- 2024Planar delamination behaviour of CFRP panels under quasi-static out-of-plane loadingcitations
- 2024Effect of pre-existing damage on delamination growth in repeatedly indented compositescitations
- 2024Planar Delamination Growth Of Composite Laminates Under Mode II Fatigue Loading
- 2024FLAx-REinforced Aluminum (FLARE)citations
- 2024Pre-straining as an effective strategy to mitigate ratcheting during fatigue in flax FRP composites for structural applications
- 2024Enhancing Fatigue Performance Of Structural Biocomposites By Pre-Straining And Pre-Creeping Methods
- 2023Towards understanding residual strength and damage evolution in damaged composite laminates
- 2023In-service delaminations in FRP structures under operational loading conditions: Are current fracture testing and analysis on coupons sufficient for capturing the essential effects for reliable predictions?citations
- 2023Investigation of compression after impact failure in carbon fiber reinforced polymers using acoustic emissioncitations
- 2023Assessment of two quasi-static approaches to mimic repeated impact response and damage behaviour of CFRP laminatescitations
- 2023Delamination link-ups in composite laminates due to multiple hail impactscitations
- 2023Experimental investigation of planar delamination behaviour of composite laminates under Out-Of-Plane loading
- 2023Flax fibre metal laminates (FLARE): A bio-based FML alternative combining impact resistance and vibration damping?
- 2023Effects of different joint wall lengths on in-plane compression properties of 3D braided jute/epoxy composite honeycombscitations
- 2023Compression after impact fatigue damage growth in CFRP – what does no-growth really mean?
- 2023Influence of neighbouring damage on delamination growth in multiple indented compositescitations
- 2022Applying the new experimental midpoint concept on strain energy density for fracture assessment of composite materialscitations
- 2022Delamination initiation in fully clamped rectangular CFRP laminates subjected to out-of-plane quasi-static indentation loadingcitations
- 2022Measurement of damage growth in ultrasonic spot welded joint
- 2022Do standard delamination tests relate to planar delamination growth?
- 2022Recycled carbon fibre mats for interlayer toughening of carbon fibre/epoxy compositescitations
- 2022A criterion for predicting delamination growth in composite laminatescitations
- 2022How literature reviews influence the selection of fatigue analysis framework
- 2022Co-cured carbon fibre/epoxy composite joints by advanced thermoplastic films with excellent structural integrity and thermal resistancecitations
- 2021Loading rate dependency of strain energy release rate in mode I delamination of composite laminatescitations
- 2021Fatigue delamination behaviour of carbon fibre/epoxy composites interleaved with thermoplastic veilscitations
- 2020Enhancing the fracture toughness of carbon fibre/epoxy composites by interleaving hybrid meltable/non-meltable thermoplastic veilscitations
- 2020Loading rate effects on mode-I delamination in glass/epoxy and glass/CNF/epoxy laminated compositescitations
- 2020The effect of bond-line thickness on fatigue crack growth rate in adhesively bonded jointscitations
- 2020Significantly enhanced structural integrity of adhesively bonded PPS and PEEK composite joints by rapidly UV-irradiating the substratescitations
- 2020The influence of interlayer/epoxy adhesion on the mode-I and mode-II fracture response of carbon fibre/epoxy composites interleaved with thermoplastic veilscitations
- 2020The effect of temperature on fatigue strength of poly(ether-imide)/multiwalled carbon nanotube/carbon fibers composites for aeronautical applicationcitations
- 2019Development of a physics-based theory for mixed mode I/II delamination onset in orthotropic laminatescitations
- 2019Physics of delamination onset in unidirectional composite laminates under mixed-mode I/II loadingcitations
- 2019Fatigue in fibre metal laminatescitations
- 2018Cyclic fatigue fracture of compositescitations
- 2018Delamination fatigue growth in polymer-matrix fibre compositescitations
- 2018The Challenge of Reversing Theories to Hybridize Structures with Fiber Metal Laminate Design Conceptscitations
- 2018The stress ratio effect on plastic dissipation during fatigue crack growthcitations
- 2018A new mixed mode I/II failure criterion for laminated composites considering fracture process zonecitations
- 2017Understanding mixed-mode cyclic fatigue delamination growth in unidirectional compositescitations
- 2016Experimental investigation of the microscopic damage development at mode i fatigue delamination tips in carbon/epoxy laminatescitations
- 2002Fatigue of Fiber Metal Laminates
Places of action
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article
Co-cured carbon fibre/epoxy composite joints by advanced thermoplastic films with excellent structural integrity and thermal resistance
Abstract
Carbon fibre/epoxy composite joints were assembled with Poly-etherether-ketone (PEEK) and Poly-ethylenimine (PEI) films using a co-curing process to prepare single-lap joint specimens. The joints were tested under quasi-static loading conditions at 22 °C and 130 °C and a fatigue loading condition. The experimental results demonstrated better or comparable structure integrity of the composite joints co-cured by PEEK and PEI films than the reference joints bonded by aerospace FM300 adhesives. In particular, the PEEK co-cured joints exhibited extraordinary mechanical performance at 130 °C and excellent fatigue resistance. For instance, the lap-shear strength at 130 °C and the fatigue life of the composite joints co-cured by 200μm PEEK films was 2.1 times and 2.7 times higher than that of the aerospace adhesive joints, respectively. Overall, the results of this work proved that advanced thermoplastic films are promising alternatives to epoxy adhesives for the co-cure joining of thermoset composites with significantly enhanced structural integrity and thermal stability. ; Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public. ; Aerospace Manufacturing Technologies ; Structural Integrity & Composites