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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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Dalverny, Olivier
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (22/22 displayed)
- 2023Anand model calibration for SAC305 solder joints based on the evolution of the shear stress and strain hysteresis loops for different thermal cycling conditionscitations
- 2022In Situ Ageing with the Platform Preheating of AlSi10Mg Alloy Manufactured by Laser Powder-Bed Fusion Processcitations
- 2019Experimental SAC305 shear stress-strain hysteresis loop construction using Hall's one-dimensional model based on strain gages measurementscitations
- 2019Analysis of the multilayer woven fabric behaviour during the forming process: focus on the loss of cohesion within the woven fibre network
- 2018Microstructural evolutions of Sn-3.0Ag-0.5Cu solder joints during thermal cyclingcitations
- 2018Microstructural evolutions of Sn-3.0Ag-0.5Cu solder joints during thermal cyclingcitations
- 2018Sensitivity analysis of composite forming process parameters using numerical hybrid discrete approach
- 2018Experimental strain energy density dissipated in SAC305 solder joints during different thermal cycling conditions using strain gages measurementscitations
- 2018Experimental strain energy density dissipated in SAC305 solder joints during different thermal cycling conditions using strain gages measurementscitations
- 2017An algorithm for damage detection and localization Usibg output-only response for civil engineering structures subjected to seismic excitations
- 2017An algorithm for damage detection and localization using output-only response for civil-engineering structures subjected to seismic excitation
- 2017Analysis of the multilayer woven fabric behaviour during the forming process. Focus on the loss of cohesion within the woven fibre network.
- 2017Analysis of the multilayer woven fabric behaviour during the forming process. Focus on the loss of cohesion within the woven fibre network
- 2016Experimental study of 48600 Carbons fabrics behavior using marks tracking technique method
- 2015Experimental characterization of the mechanical behavior of two solder alloys for high temperature power electronics applicationscitations
- 2015Experimental and Numerical Study of Interfacial Fracture Parameters of a Brazed Joints
- 2012Identification of orthotropic material properties using displacement field measurements
- 2012Non destructive investigation of defects in composite structures by three infrared thermographic techniques
- 2012Micromechanical modeling of brittle damage in composite materials: primary anisotropy, induced anisotropy and opening-closure effects
- 2008Modélisation des assemblages de ballons pressurisés stratosphériques
- 20042D and 3D numerical models of metal cutting with damage effectscitations
- 2002Transient Numerical Models of Metal Cutting using the Johnson-Cook's Rupture Criterion.citations
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document
Experimental study of 48600 Carbons fabrics behavior using marks tracking technique method
Abstract
Lightweight and energy saving are the main challenges in the aircraft industry production, that explain the increase of composite demand and the diversity of its applications. The investigation of the shear behavior and stiffness of technical woven fabric are essential to guarantee the performance of the final product. In case of forming process (for example RTM process), the in-plane deformability of the woven fabric is necessary for forming without creating defects. The change of the fiber orientation (warp and weft) have a significant impact on final mechanical properties. In this study, the use of marks tracking technique allow the determination of the rigidity of 48600 C 1300 carbon fabrics, and allow calculation of their shear angle, lock angle during tensile and bias-extension tests.