الرئيسية › دليل الباحثين › X. Feaugas
X. Feaugas
الانتماء : Centre National de la Recherche Scientifique · Laboratoire des Sciences de l'Ingénieur pour l'Environnement · La Rochelle Université
- 25منشورات (انتماء فرنسي)
- 329مجموع المنشورات
- 8405الاستشهادات
- 48مؤشر h
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إنشاء ملفي المجاني إضافة منشوراتيمجالات البحث
- Hydrogen embrittlement and corrosion behaviors in metals
- Hydrogen Storage and Materials
- Fusion materials and technologies
- Fatigue and fracture mechanics
- Microstructure and mechanical properties
المنشورات (25)
- Experimental and numerical damage analysis of composite patched AA2024-T3 plates with notch and adhesive void defects
- Enhanced numerical modelling of damage and repair in notched 2024-T3 aluminum plates using XFEM, CZM, and VCCT
- Numerical and experimental analysis of the performance of the metal patch compared to the composite patch under aging conditions in water immersion
- Analysis of load-displacement curves of an adhesive-reinforced composite patch repaired plate using the combination of XFEM and CZM techniques
- Prediction of mass adhesive damage based on the Rousselier model: Experimental and numerical analysis
- Substrate geometry effect on the strength of repaired plates: Combined XFEM and CZM approach
- Analysis of the effect of modifying the thickness of a damaged and repaired plate by composite patch on the J-Integral; effect of bonding defects
- Multiscale analysis of hydrogen-induced softening in f.c.c. nickel single crystals oriented for multiple-slips: elastic screening effect
- Analysis of the presence of bonding defects on the fracture behavior of a damaged plate repaired by composite patch
- Hygrothermal ageing effect of ADEKIT A140 adhesive on the J-integral of a plate repaired by composite patch
- Influence of water ingress onto the crack propagation rate in a AA2024-T3 plate repaired by a carbon/epoxy patch
- Numerical analysis of the effect of the presence, number and shape of bonding defect on the shear stresses distribution in an adhesive layer for the single-lap bonded joint; Part 1
- Finite element assessment of an affine self–consistent model for hexagonal polycrystals
- Effects of composite adherend properties on stresses in double lap bonded joints
- Effect of humidity absorption by the adhesive on the performances of bonded composite repairs in aircraft structures
- Stress intensity factor for repaired crack with bonded composite patch under thermo-mechanical loading
- Experimental and numerical study of repair techniques for panels with geometrical discontinuities
- Numerical estimation of the mass gain between double symmetric and single bonded composite repairs in aircraft structures
- Linear and non-linear analyses for semi-elliptical surface cracks in pipes under bending
- Effect of composite hygrothermal aging on the SIF variation in bonded composite repair of aircraft structures
- Analysis of the plastic zone size ahead of repaired cracks with bonded composite patch of metallic aircraft structures
- Analysis of the distribution of thermal residual stresses in bonded composite repair of metallic aircraft structures
- Analyze of the notch effect on the distribution of the stresses in the adhesive layer between two bonded aluminum 2024-T3 plates
- Stress distribution in a 2024-T3 aluminum plate with a circular notch, repaired by a graphite/epoxy composite patch
- Numerical analysis for the determination of the stress intensity factors and crack opening displacements in plates repaired with single and double composite patches
المؤلفون المشاركون
- Sébastien Touzain
- S. Cohendoz
- S. Mallarino
- Bruno Preaudeau
- N. Benssediq
- Abdelwaheb Amrouche
- Ilias-Mohammed-Amine Ghermaoui
- L. Aminallah
- Abdelali OUDRISS
- Rénald Brenner
- F. Onimus
- Ph. Pilvin
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