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pro vyhledávání: '"C. Mabru"'
Akademický článek
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Publikováno v:
MATEC Web Conf. Volume 83, 2016 CSNDD 2016-International Conference on Structural Nonlinear Dynamics and Diagnosis
MATEC Web Conf. Volume 83, 2016 CSNDD 2016-International Conference on Structural Nonlinear Dynamics and Diagnosis, 2016, Marrakech, Morocco. pp.03003
MATEC Web Conf. Volume 83, 2016 CSNDD 2016-International Conference on Structural Nonlinear Dynamics and Diagnosis, 2016, Marrakech, Morocco. pp.03003, ⟨10.1051/MATECCONF/20168303003⟩
MATEC Web of Conferences, Vol 83, p 03003 (2016)
MATEC Web Conf. Volume 83, 2016 CSNDD 2016-International Conference on Structural Nonlinear Dynamics and Diagnosis, 2016, Marrakech, Morocco. pp.03003
MATEC Web Conf. Volume 83, 2016 CSNDD 2016-International Conference on Structural Nonlinear Dynamics and Diagnosis, 2016, Marrakech, Morocco. pp.03003, ⟨10.1051/MATECCONF/20168303003⟩
MATEC Web of Conferences, Vol 83, p 03003 (2016)
International audience; Aircraft structures are commonly subjected to repeated loading cycles leading to fatigue damage. Fatigue data can be extrapolated by fatigue models which are adopted to describe the fatigue damage behaviour. Such models depend
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e49057368c50745daf5eda1f846df840
https://hal.archives-ouvertes.fr/hal-02047807
https://hal.archives-ouvertes.fr/hal-02047807
Publikováno v:
Engineering Fracture Mechanics. 64:23-47
The fatigue crack propagation behaviour of a quaternary γ -TiAl alloy has been investigated under various test conditions in order to discern the specific role of temperature and environment. The results obtained in ambient air at room temperature a
Publikováno v:
Scopus-Elsevier
Alloys based on ordered intermetallics, and among them FeAl and TiAl, are now very close to meet design requirements for a wide use in structural applications where there is a need for stiff and light materials. However the damage tolerance of these
Akademický článek
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Publikováno v:
Applied Composite Materials. 4:95-119
This paper presents an experimental study of the initiation and development of damage in composite/composite joints. The materials studied are glass fibre reinforced polyester laminates and these are bonded together using an epoxy adhesive. Two types
Publikováno v:
Scopus-Elsevier
The fatigue crack growth behaviour of a quaternary Ti-48Al-2Mn-2Nb is investigated with a special emphasis on the role of environment. The fatigue crack-growth resistance is shown to be significantly lessened in ambient air. This is due to a lack of
Publikováno v:
Materials Science and Engineering: A. 219:212-220
In the present study the fatigue crack growth behaviour of a quaternary Ti 48Al 2Mn 2Nb based alloy in the as-received condition was investigated in air and vacuum at room temperature. The respective influence of crack closure and environment was mor
Publikováno v:
Scripta Materialia. 34:1449-1454
The fatigue crack growth rates measured in the case of the TiAl-based alloy investigated in the present study are highly sensitive to the {Delta}K value. The fatigue crack propagation is deeply affected by the crack closure phenomenon. As a consequen