Zobrazeno 1 - 10
of 28
pro vyhledávání: '"A. F. Laurin"'
Publikováno v:
Composites Part A: Applied Science and Manufacturing. 81:243-253
Laminated composite materials are increasingly used for the design of aircraft primary structures subjected to complex 3D loadings. The delamination observed in curved parts ensuring the junction between the different perpendicular panels is one of t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1b9d584b6187a1ee45cc96ca2b5132c
https://doi.org/10.1016/j.compositesa.2015.11.018
https://doi.org/10.1016/j.compositesa.2015.11.018
Publikováno v:
Composites Part A: Applied Science and Manufacturing
Composites Part A: Applied Science and Manufacturing, Elsevier, 2018, 113, pp.209-219. ⟨10.1016/j.compositesa.2018.07.026⟩
Composites Part A: Applied Science and Manufacturing, Elsevier, 2018, 113, pp.209-219. ⟨10.1016/j.compositesa.2018.07.026⟩
In this study, an innovative test is proposed to identify the longitudinal compressive strength of a unidirectional ply. The key idea consists in designing a laminate that, when subjected to a tensile loading, fails by compressive failure in its cent
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cb926eb4c8a116a46f5f7b9f214eff63
https://hal.archives-ouvertes.fr/hal-01870106
https://hal.archives-ouvertes.fr/hal-01870106
Enhanced strength analysis method for composite open-hole plates ensuring design office requirements
Publikováno v:
Composites Part B: Engineering
Composites Part B: Engineering, Elsevier, 2014, 62, pp.5-11. ⟨10.1016/j.compositesb.2014.02.002⟩
Composites Part B: Engineering, Elsevier, 2014, 62, pp.5-11. ⟨10.1016/j.compositesb.2014.02.002⟩
International audience; The use of unidirectional carbon fibre-reinforced composites in the design of primary structures, such as the centre wing box, has spread increasingly over the past few years. However, composite structures can be weakened by t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::39e1464169ff51a1b6406cc08471d9ae
https://doi.org/10.1016/j.compositesb.2014.02.002
https://doi.org/10.1016/j.compositesb.2014.02.002
Publikováno v:
Journal of Composite Materials. 47:2713-2747
This paper presents a multiscale hybrid approach for predicting damage and failure of laminated composite structures based on the thermo-mechanical properties (stress/strain behaviour and strength) of the unidirectional plies. This kind of approach i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c81912c308ce6051fb4ce4e9a3a6307
https://doi.org/10.1177/0021998312470151
https://doi.org/10.1177/0021998312470151
Publikováno v:
Journal of Composite Materials. 47:743-762
This paper presents a comparison between the experimental results provided in the PART B of the second World Wide Failure Exercise and the predictions obtained from a Micromechanical-based hybrid mesoscopic 3D approach described in the PART A of this
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c65aba0bcc04752c7a9f207b51b86009
https://doi.org/10.1177/0021998312460558
https://doi.org/10.1177/0021998312460558
Publikováno v:
Journal of Composite Materials. 46:2389-2415
A new micromechanical-based hybrid mesoscopic 3D approach has presented for the prediction of failure under triaxial loadings. The failure criterion is based on physical principles and introduces micromechanical aspects (such as the effect of the loc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::31c0100acbf2d58b8e5aace29ed775a4
https://doi.org/10.1177/0021998312450179
https://doi.org/10.1177/0021998312450179
Publikováno v:
Composite Structures. 94:2278-2284
In part II of this study, a methodology is presented to compute the failure of large-scale bolted joints in composite structures. This methodology is based both on a multilevel calculation strategy and on virtual testing. At the global level, coarse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7aa800fa8efdbf57d6e63d71a2f6a340
https://doi.org/10.1016/j.compstruct.2011.07.005
https://doi.org/10.1016/j.compstruct.2011.07.005