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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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Warnet, Laurent L.
University of Twente
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (54/54 displayed)
- 2022The relation between in-plane fiber waviness severity and first ply failure in thermoplastic composite laminatescitations
- 2022An experimental approach to reproduce in-plane fiber waviness in thermoplastic composites test coupons using a reverse forming methodcitations
- 2021Tool-ply interaction in the formation of waviness during C/PEEK consolidationcitations
- 2021Effect of in-plane fiber waviness defects on the compressive properties of quasi-isotropic thermoplastic compositescitations
- 2020Real-time observation of waviness formation during C/PEEK consolidationcitations
- 2019Automatic fiber tracing and waviness detection in carbon fiber composite micrographs
- 2019Towards the combination of automated lay-up and stamp forming for consolidation of tailored composite componentscitations
- 2019Rapid Manufacturing of a Tailored Spar by AFP and Stamp Forming
- 2018Effect of resin-rich bond line thickness and fibre migration on the toughness of unidirectional Carbon/PEEK jointscitations
- 2018Assessment of failure and cohesive zone length in co-consolidated hybrid C/PEKK butt jointcitations
- 2018Interlaminar fracture toughness of 5HS Carbon/PEEK laminates. A comparison between DCB, ELS and mandrel peel testscitations
- 2018Deconsolidation of C/PEEK blankscitations
- 2018Consolidation quality and mechanical performance of stamp formed tailored blanks produced by rapid AFPcitations
- 2018Rapid Manufacturing of a Tailored Spar by AFP and Stamp Forming
- 2017Influence of prepreg characteristics on stamp consolidationcitations
- 2017Quantification of tape deconsolidation during laser assisted fiber placement
- 2017Effects of release media on the fusion bonding of carbon/PEEK laminatescitations
- 2017Transverse crack initiation under combined thermal and mechanical loading of Fibre Metal Laminates and Glass Fibre Reinforced Polymers
- 2017Challenges in Stamp Forming Tailored Blanks
- 2016Intimate contact development in laser assisted fiber placementcitations
- 2016Carbon Nanofibers Grown on Large Woven Cloths: Morphology and Properties of Growthcitations
- 2016Woven fabric compositescitations
- 2015On the mechanical behaviour of a butt jointed thermoplastic composite under bending
- 2015Influence of surface preparation on fusion bonding of thermoplastic composites
- 2015Synthesis of Carbon Nanofibers on Large Woven Clothcitations
- 2015Matrix damage helaing in fiber reinforced composite materials containing embedded active and passive wires
- 2015Consolidation Quality of Press-Formed Tailored Blanks
- 2013Engineers in a flap over rotor blades
- 2013Influence of moisture content on impact properties of flax fibre reinforced polymers
- 2012Failure Modeling of Thermoplastic Butt-Joint Stiffened Panels by Quasi-Static Loading
- 2012On the weld strength of in situ tape placed reinforcements on weave reinforced structurescitations
- 2011Towards a process simulation tool for the laseer assisted tape placement process
- 2011Dynamic characterisation of a damaged composite structure with stiffeners employing fibre bragg gratings
- 2011Vibration based structural health monitoring and the modal strain energy damage index algorithm applied to a composite T-beamcitations
- 2010Modeling of Stress Development During Thermal Damage Healing in Fiber-reinforced Composite Materials Containing Embedded Shape Memory Alloy Wirescitations
- 2010Towards a process simulation tool for the laseer assisted tape placement process
- 2010Friction measurements on carbon fibre towscitations
- 2010Experimental characterization of fibre-reinforced composites improved with nanofibres or nanotubes
- 2010Weld strength assessment for tape placementcitations
- 2009Vibration based structural health monitoring in fibre reinforced composites employing the modal strain energy method
- 2009An attempt to use scratch tests to predict the residual lifetime of unplasticised poly(vinyl chloride) pipescitations
- 2008Damage healing in thermoplastic composite plates by employing shape memory alloy wires (on USB stick)
- 2008Dynamic analysis of degradation in E-glass reinforced epoxy composite
- 2008Delamination detection with fibre Bragg gratings based on dynamic behaviourcitations
- 2008Ductile or brittle? The impact behaviour of uPVC upon ageing
- 2007High velocity impact on textile reinformced composties (CD-rom)
- 2007High velocity impact on textile reinforced composites
- 2007Compression after impact on curved composite panels
- 2006Damage development around moulded-in holes in flat braided composites (CD-ROM)
- 2004Dielectric Properties in Composites
- 2003The effect of residual stress on transverse cracking in cross-ply carbon-polyetherimide laminates under bendingcitations
- 2002Modelling of a reinforced thermoplastic pipe
- 2002Springback analysis of doubly curved GLARE panels
- 2002Impact damage in woven fabric reinforced composites
Places of action
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article
An experimental approach to reproduce in-plane fiber waviness in thermoplastic composites test coupons using a reverse forming method
Abstract
In-plane fiber waviness is one of the defects that can occur from the stamp-forming process of thermoplastic composite (TPC) parts. The influence of this defect on the mechanical performance of multidirectional composites is not yet fully understood. The main challenge in determining the influence on mechanical properties lies in reproducing the waviness in test coupons that can subsequently be subjected to testing. This paper describes an experimental approach to reproduce representative in-plane waviness defects, specific for TPC, by reverse-forming of V-shape parts of various bend angles and inner radii. Characterization results show that this method enables the manufacturing of localized in-plane waviness in flat 24-ply quasi-isotropic C/PEEK composites with no voids. Furthermore, laminates having varying levels of maximum waviness angle ((Formula presented.)), between 14° to 64°, were successfully produced in this work. By comparing the (Formula presented.) value with the examples of industrial stamp-formed parts, it can be concluded that the developed coupon manufacturing method can reproduce waviness from TPC part production reasonably well. Finally, all of the produced laminates have defective region lengths smaller than 20 mm, localized within a predefined location which makes them well suited for standard compression test coupons.