693.932 PEOPLE
| 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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Bouvet, Christophe
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (113/113 displayed)
- 2024Testing Structural Elements under Multiaxial Loading: A Numerical Model of the Bench to Understand and Predict Complex Boundary Conditionscitations
- 2023High temperature in situ impact testing of hybrid thermoplastic polyether ether ketone laminatescitations
- 2022Study of the fracture behaviour in hybrid fibers reinforced thermoplastic laminatescitations
- 2022Study of the fracture behaviour in hybrid fibers reinforced thermoplastic laminates: Influence of temperature and initial notch orientationcitations
- 2022Study of the fracture behaviour in hybrid fibers reinforced thermoplastic laminates: Influence of temperature and initial notch orientation ; Study of the fracture behaviour in hybrid fibers reinforced thermoplastic laminates: Influence of temperature and initial notch orientation: Influence of temperature and initial notch orientationcitations
- 2022Experimental characterization of the mode i translaminar fracture toughness of CFRP using infrared and dic measurements: compact tension and compact compression tests
- 2022Experimental characterization and numerical modelling of the translaminar fracture of woven-ply hybrid fibers reinforced thermoplastic laminatescitations
- 2021Experimental and Finite Element Analysis of the Tensile Behavior of Architectured Cu-Al Composite Wirescitations
- 2021Structural testing of large notched composite specimens under combined shear and pressure
- 2021Benchmark of wrinkling formulae and methods for pre-sizing of aircraft lightweight sandwich structurescitations
- 2021On the efficiency of some analytic wrinkling models
- 2021High temperature translaminar fracture of woven-ply thermoplastic laminates in tension and in compressioncitations
- 2021High temperature translaminar fracture of woven-ply thermoplastic laminates in tension and in compressioncitations
- 2020Combined loadings after medium velocity impact on large CFRP laminate plates: Tests and enhanced computation/testing dialoguecitations
- 2020Experimental and Numerical Study of Damages Induced by Low-Velocity Impact on 4th Generation Composite Laminatescitations
- 2020Study of translaminar fracture toughness of unidirectional flax/epoxy compositecitations
- 2020Influence of machining damage generated during trimming of CFRP composite on the compressive strengthcitations
- 2020Review of composite sandwich structure in aeronautic applicationscitations
- 2020Numerical analysis of shear stiffness of an entangled cross-linked fibrous materialcitations
- 2020Influence of impact velocity on impact behaviour of hybrid woven-fibers reinforced PEEK thermoplastic laminatescitations
- 2020Influence of impact velocity on impact behaviour of hybrid woven-fibers reinforced PEEK thermoplastic laminatescitations
- 2020New tool for reduction of harmful particulate dispersion and to improve machining quality when trimming carbon/epoxy compositescitations
- 2020Strain rate effect of mode II interlaminar fracture toughness on the impact response of a thermoplastic PEEK compositecitations
- 2020A new interface element connecting 3D finite elements with non-coincident nodes to simulate delamination in composite laminatescitations
- 2020Effects of dynamics and trigger on energy absorption of composite tubes during axial crushingcitations
- 2019Experimental investigation of compression and compression after impact of wood-based sandwich structurescitations
- 2019Experimental investigation of compression and compression after impact of wood-based sandwich structurescitations
- 2019Simulation of medium velocity impact and compression or shear after impact on large composite laminated plates
- 2019Development and characterization of wood based eco-structures composites
- 2019Effect of unstable crack growth on mode II interlaminar fracture toughness of a thermoplastic PEEK compositecitations
- 2019Effect of unstable crack growth on mode II interlaminar fracture toughness of a thermoplastic PEEK compositecitations
- 2019High temperature translaminar fracture in tension and in compression of woven-ply thermoplastic laminates
- 2019Prediction of the ultimate strength of quasi-isotropic TP-based laminates structures from tensile and compressive fracture toughness at high temperaturecitations
- 2019Insert sizing of sandwich panels by means of a failure mode map
- 2019Fracture mechanics of hybrid composites with ductile matrix and brittle fibers: Influence of temperature and constraint effectcitations
- 2019Surface integrity while trimming of composite structures: X-ray tomography analysiscitations
- 2019Numerical study of the crack growth in a woven composite
- 2018Damage tolerance of an impacted composite laminatecitations
- 2018Virtual testing of metallic inserts for sandwich structures
- 2018Noncircular CFRP bicycle’s chainring, part II: finite element analysis
- 2018Numerical modelling of shear hysteresis of entangled cross-linked carbon fibres intended for core materialcitations
- 2018Shear nonlinear behavior of the Nomex honeycomb core
- 2018Fracture mechanics of hybrid composites with ductile matrix and brittle fibers: Influence of temperature and constraint effectcitations
- 2018Fracture mechanics of hybrid composites with ductile matrix and brittle fibers: Influence of temperature and constraint effectcitations
- 2017Influence of temperature on the impact behavior and damage tolerance of hybrid woven-ply thermoplastic laminates for aeronautical applicationscitations
- 2017Mechanics of Aeronautical Composite Materials
- 2017Experimental and numerical analysis of Carbon Fiber Reinforced Polymer notched coupons under tensile loadingcitations
- 2017Evaluation of fracture toughness in composite structures using Infrared Thermography
- 2017Damage of woven composite under translaminar cracking tests using infrared thermographycitations
- 2017Shear testing of honeycomb cores for inserts
- 2017Analysis of nonlinear behavior on honeycomb cores
- 2016Experimental analysis of CFRP laminates subjected to compression after edge impactcitations
- 2016Enhanced nonlinear insert model
- 2016Experimental study of compression after impact of asymmetrically tapered composite laminatecitations
- 2016Numerical simulation of impact and compression after impact of asymmetrically tapered laminated CFRPcitations
- 2016Numerical simulation of impact and compression after impact ofasymmetrically tapered laminated CFRPcitations
- 2015Edge impact modeling on stiffened composite structurescitations
- 2015Entangled cross-linked fibres for an application as core material for sandwich structures - Part I: Experimental investigationcitations
- 2015Measure of fracture toughness of compressive fiber failure in composite structures using infrared thermographycitations
- 2015Analyse du comportement en traction de stratifiés composites entaillés en utilisant la corrélation d'images ainsi que le suivi infrarouge
- 2015Damage of woven composite under tensile and shear stress using infrared thermography and micrographic cutscitations
- 2014Edge impact damage scenario on stiffened composite structurecitations
- 2014Discrete ply modelling of impact and compression after impact on composite laminates
- 2014An experimental study of damage evolution in 2D thin woven composite under quasi-static loading using infrared thermography
- 2014INVESTIGATION OF IMPACT DAMAGE OF TAPERED COMPOSITE LAMINATES
- 2014Modelling permanent indentation in composite subjected to impact : identification through a specific three-point bending test
- 2014Experimental analysis of CFRP laminates subjected to Compression After Impact: the role of impact-induced cracks in failurecitations
- 2014Permanent indentation characterization for low-velocity impact modelling using three-point bending testcitations
- 2014Post-Impact Investigation of CFRP Laminated Plate
- 2013Damage analysis and fracture toughness evaluation in a thin woven composite laminate under static tension using infrared thermographycitations
- 2013Damage analysis and fracture toughness evaluation in a thin woven composite laminate under static tension using infrared thermographycitations
- 2013Experimental and numerical study of AA5086-H111 aluminum plates subjected to impactcitations
- 2013Modeling impact on aluminium sandwich including velocity effects in honeycomb corecitations
- 2013Reversible Rail Shear Apparatus Applied to the Study of Woven Laminate Shear Behaviorcitations
- 2013Étude expérimentale de l’endommagement d’un composite tissé mince sous traction quasi-statique via thermographie infrarouge
- 2013Étude expérimentale de l’endommagement d’un composite tissé mince sous traction quasi-statique via thermographie infrarouge
- 2012Low velocity impact modeling in composite laminates capturing permanent indentationcitations
- 2012The effect of stacking sequence on the low-velocity impact response of composite laminates
- 2012A bundle-scale model of propagation of a through-the-thickness notch in a woven composite under fatigue loading
- 2012Study of the crack growth in composite rotor blade skin
- 2012Experimental investigation of impact on composite laminates with protective layerscitations
- 2012Effect of fibre failure on low velocity impact of composite laminate with different stacking sequences
- 2012Comparative study on the impact behavior and damage tolerance of woven carbon fiber reinforced thermoplastic- and thermosetting composites
- 2012Experimental study on sandwich structures subjected to medium velocity impacts for aircraft armour applications
- 2012Discrete ply modelling of low velocity impact and compression after impact in unidirectional laminated composites
- 2012Damage assessment of thin woven composite subjected to quasi-static tensile loading using infrared thermography
- 2012Damage assessment of thin woven composite subjected to quasi-static tensile loading using infrared thermography
- 2012Modelling Shape Memory Alloy Behaviour under Proportional Loading and Anisothermal Conditionscitations
- 2011chapter 5: Static and dynamic behaviours of composite laminate
- 2011Evaluation of the impact resistance of various composite sandwich beams by vibration testscitations
- 2011Application of modal analysis for evaluation of the impact resistance of aerospace sandwich materials
- 2011Fatigue crack growth in thin notched woven glass composites under tensile loading. Part I: experimentalcitations
- 2010A New Sandwich Structured Composite With Entangled Carbon Fibres As Core Material: Processing And Mechanical Properties
- 2010Influence of woven ply degradation on fatigue crack growth in thin notched composites under tensile loadingcitations
- 2010Modelling of impact damage and permanent indentation on laminate composite plate
- 2010Mechanical protection for composite structures submitted to low energy impact
- 2009Fibers networks as a new type of core material. Processing and mechanical properties
- 2009Low velocity impact modelling in laminate composite panels with discrete interface elementscitations
- 2009Monitoring the effects of impact damages on modal parameters in carbon fiber entangled sandwich beamscitations
- 2009Static and dynamic testing of glass fiber entangled sandwich beams: a comparison with honeycomb and foam sandwich beams
- 2009Fabrication and mechanical testing of glass fiber entangled sandwich beams: A comparison with honeycomb and foam sandwich beamscitations
- 2009Mechanical behavior of entangled fibers and entangled cross-linked fibers during compressioncitations
- 2008Modelling of low-energy/low-velocity impact on Nomex honeycomb sandwich structures with metallic skinscitations
- 2008Core crush criterion to determine the strength of sandwich composite structures subjected to compression after impactcitations
- 2006About modelling the shape memory alloy behaviour based on the phase transformation surface identification under proportional loading and anisothermal conditionscitations
- 2004Determination and modeling of equivalent stress and equivalent transformation strain for polycrystalline textured shape memory alloys
- 2004Phase transformation yield surface determination of isotropic and textured shape memory alloys
- 2004Determination of phase transformation yield surface of anisotropic shape memory alloys
- 2004A phenomenological model for pseudoelasticity of shape memory alloys under multiaxial and non proportional loadings
- 2004Constitutive equations for pseudo-elastic behavior of shape memory alloys under multiaxial non proportional loadings
- 2002Mechanical behavior of a Cu-Al-Be shape memory alloys under multiaxial proportional and non proportional loadings
- 2002Experimental and numerical determinations of the initial surface of phase transformation under biaxial loading in some polycrystalline shape memory alloys
- 2002What about the yield transformation surface determination (austenite - martensite) with the measurement of austenite and martensite lattice parameters for some shape memory alloys ?
Places of action
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conferencepaper
Shear nonlinear behavior of the Nomex honeycomb core
Abstract
Sandwich structures are widely used for many different applications since they offer exceptional benefits, providing a high bending stiffness with a very low weight. In aeronautics, sandwich panels are commonly made of Nomex honeycomb, and therefore this core has been studied for decades. Concerning the literature, most of the investigations on honeycomb cores are focused on to investigate the compression properties of the structure, for energy absorption applications or impacts on sandwich panels. In the other hand, there are far fewer studies concerning the understanding of the shear nonlinear behavior of the honeycomb [1], this can be considered a major drawback, knowing that it’s the core who absorbs most of the shear components when a bending force is applied.To help fill this gap, this work focuses on to study the shear behavior of the honeycomb structure. Several experimental tests are conducted using different boundary conditions to observe the buckling of the cells. This helps to understand the causes of the phenomenological stages that appear when the honeycomb structure is submitted to shear loads. Finally, a numerical approach is used to simulate the honeycomb response to be able to see on the interior cell walls and to better understand this phenomenon. This work is a contribution to the understanding of the shear buckling of Nomex honeycomb cores.