Institut de Mécanique et d’Ingénierie de Bordeaux (I2M): Soumissions récentes
Voici les éléments 540-546 de 845
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Article dans une revue avec comité de lecture;
PALIN-LUC, Thierry; (ASTM, 2004)
This paper deals with the effect on life of the desynchronism between two variable amplitude load sequences in combined bending and torsion. Experiments were carried out on smooth specimens made of the EN-GJS800-2 cast ... -
Article dans une revue avec comité de lecturePALIN-LUC, Thierry; ; (Elsevier, 2006)
This paper deals with a technique to transform a multiaxial stress and strain-time sequence (in service recorded) in a simplified sequence. This simplified sequence is shorter than the original one and equivalent in terms ...
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Article dans une revue avec comité de lecture; ; ; ;PERRY, Nicolas (Elsevier, 2016)
The production of plywood represents a major proportion of engineered wood products. The traditional manufacturing process requires very thorough drying of the wood before gluing. Gluing green wood is a new technology ...
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Article dans une revue avec comité de lecturePANETTIERI, Enrico; ; MONTEMURRO, Marco; (Elsevier, 2016)
Low-velocity impacts (LVI) on composite laminates pose significant safety issues since they are able to generate extended damage within the structure, mostly delaminations and matrix cracking, while being hardly detectable ...
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Communication sans acte;PALIN-LUC, Thierry; (Elsevier, 2016)
This paper is focused on the analysis of fatigue crack initiation and growth mechanisms in defect free VT3-1 titanium alloy (similar to Ti6Al4V) in VHCF regime under tensile and torsion loadings. Fully reversed fatigue ...
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Communication avec acte;MILCENT, Thomas (2014)
We introduce an Eulerian model for the coupling of a fluid governed by the Navier- Stokes equations, with an immersed interface endowed with full membrane elasticity (i.e. including shear e ects). We show numerical evidences ...
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Article dans une revue avec comité de lecture;PALIN-LUC, Thierry; (Elsevier, 2016)
This paper is focused on the VHCF behavior of aeronautical titanium alloy under tensile and torsion fatigue loadings. Tensile tests were carried out with two different stress ratios: R = À1 and R = 0.1. Both surface and ...
