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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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Ataş, Akın
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (21/21 displayed)
- 2022Strain rate effect on the tensile properties of plain weave aramid, carbon, and glass fabric reinforced monolithic and hybrid compositescitations
- 2021Effect of quasi-static and intermediate strain rates on the tensile properties of hybrid polymer compositescitations
- 2018Bolted joints in quasi-unidirectional glass-fibre NCF composite laminatescitations
- 2018Compression after low velocity impact tests of marine sandwich composites: Effect of intermediate wooden layerscitations
- 2018Experimental investigation of pinned joints in NCF Glass-Fibre reinforced composite platescitations
- 2016Bolted joints in three axially braided carbon fibre/epoxy textile composites with moulded-in and drilled fastener holescitations
- 2016Damage and failure analysis of bolted joints in composite laminatescitations
- 2015Open hole compressive strength and damage mechanismscitations
- 2014Application of cohesive zone elements in damage analysis of compositescitations
- 2014Strength prediction of bolted joints in CFRP composite laminates using cohesive zone elementscitations
- 2013Subcritical damage mechanisms of bolted joints in CFRP composite laminatescitations
- 2013Failure analysis of bolted joints in cross-ply composite laminates using cohesive zone elements
- 2012Modelling delamination onset and growth in pin loaded composite laminatescitations
- 2012Effect of clamping force on the delamination onset and growth in bolted composite laminatescitations
- 2012Effect of geometric parameters on the stress distribution in Al 2024-T3 single-lap bolted jointscitations
- 2012Progressive failure analysis of bolted joints in composite laminatescitations
- 2012Strength prediction of bolted joints in cross-ply laminates based on subcritical damage modelling
- 2011A qualitative comparison of stresses at aircraft bolted joint holes under initial clamping forcecitations
- 2009Failure analysis of laminated composite plates with two parallel pin-loaded holescitations
- 2009The effect of curing conditions and fiber end shapes on the mechanical properties of compositescitations
- 2008İki eksenli gerilme altındaki kompozit plakalarda dairesel delik çevresindeki gerilme dağılımları
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article
Compression after low velocity impact tests of marine sandwich composites: Effect of intermediate wooden layers
Abstract
In the present work, compression after impact (CAI) behavior of sandwich composite materials with intermediate wooden layers was investigated. Sandwich panels were manufactured by using vacuum assisted resin transfer molding (VARTM) method with pinewood and ashwood intermediate layers. 15 and 25 mm thick PVC foams with a same density of 80 kg/m3 were chosen in conjunction with the face sheets composed of non-crimp biaxial E-glass fabrics and bisphenol-A epoxy vinyl ester resin material system. Impact tests were performed under 30 J (low) and 60 J (high) energy levels with conical and hemispherical impactors. CAI tests were conducted in accordance with the ASTMC364/C364M-07 standard. Using pinewood and ashwood intermediate layers increased the residual CAI strength and decreased the depth of the impact damage. The intermediate wooden layers have also a potential to reduce the thickness of the composite face sheets and foam core which may increase the proportion of the recyclable wooden materials within the sandwich structure.