Zobrazeno 1 - 10
of 35
pro vyhledávání: '"Daniele Fanteria"'
Publikováno v:
Journal of Composite Materials. 56:2585-2598
An experimental program has been carried out for the evaluation of the delamination onset condition of various composite material systems, under the application of constant amplitude cyclic loading. Standard Double Cantilever Beam End Notch Flexure a
Publikováno v:
Dynamic Response and Failure of Composite Materials ISBN: 9783031285462
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89336e08cb62156bbc638834c63a3a8e
https://doi.org/10.1007/978-3-031-28547-9_9
https://doi.org/10.1007/978-3-031-28547-9_9
Publikováno v:
Journal of Composite Materials. 55:4601-4616
This work presents the results of an experimental study performed in carbon/epoxy composite materials manufactured using a ply-level hybridization technique. The aim of the study is to investigate the potential of such hybridization technique to prom
Publikováno v:
Composite Structures
Composite Structures, Elsevier, 2022, 282, pp.115042. ⟨10.1016/j.compstruct.2021.115042⟩
Composite Structures, Elsevier, 2022, 282, pp.115042. ⟨10.1016/j.compstruct.2021.115042⟩
A consistent energy-based cohesive zone model to simulate the mode I delamination behaviour of Fully-Uncoupled Multi-Directional (FUMD) laminates is presented in this study. The proposed energy-based approach allows determining a more general constit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::494db696b55376b818b05c73e20a63b5
http://hdl.handle.net/20.500.12278/124317
http://hdl.handle.net/20.500.12278/124317
Publikováno v:
Composite Structures. 210:755-766
A numerical framework for the determination of the damage, the stress and the inelastic strain field induced by the curing process for unidirectional carbon/epoxy composite material is proposed. The approach integrates a network model for the estimat
Publikováno v:
Composites Part B: Engineering. 153:97-107
An experimental program has been carried out at the Department of Civil and Industrial Engineering of the University of Pisa, in collaboration with Leonardo Helicopter Division (formerly AgustaWestland), for the evaluation of the interlaminar fractur
Experimental assessment of Fully-Uncoupled Multi-Directional specimens for mode I delamination tests
Publikováno v:
Composites Science and Technology
Composites Science and Technology, Elsevier, 2020, 200, pp.108421-. ⟨10.1016/j.compscitech.2020.108421⟩
Composites Science and Technology, 2020, 200, pp.108421. ⟨10.1016/j.compscitech.2020.108421⟩
Composites Science and Technology, Elsevier, 2020, 200, pp.108421-. ⟨10.1016/j.compscitech.2020.108421⟩
Composites Science and Technology, 2020, 200, pp.108421. ⟨10.1016/j.compscitech.2020.108421⟩
This paper proposes an experimental study whose goal is to validate the concept of Fully-Uncoupled Multi-Directional (FUMD) specimens for delamination tests. In order to reduce the likelihood of delamination jump, a glass/epoxy UD-fabric composite wa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6c33c3cb502b6c0c821e5647368577ca
https://hal.archives-ouvertes.fr/hal-03492167
https://hal.archives-ouvertes.fr/hal-03492167
Publikováno v:
Health Monitoring of Structural and Biological Systems IX.
Adhesive junctions or co-infusion of skin and stiffeners represent efficient manufacturing processes for aircrafts composites stiffened panels leading to weight saving, although they have not been widely adopted yet due to certification issues and th
Publikováno v:
Journal of Composite Materials
Journal of Composite Materials, SAGE Publications, 2019, 54 (6), pp.773-790. ⟨10.1177/0021998319868293⟩
Journal of Composite Materials, 2019, 54 (6), pp.773-790. ⟨10.1177/0021998319868293⟩
Journal of Composite Materials, SAGE Publications, 2019, 54 (6), pp.773-790. ⟨10.1177/0021998319868293⟩
Journal of Composite Materials, 2019, 54 (6), pp.773-790. ⟨10.1177/0021998319868293⟩
International audience; In this paper, a procedure to obtain fully uncoupled multi-directional stacking sequences for delamination specimens is outlined. For such sequences, in-plane, membrane-bending and torsion–bending coupling terms are null (in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ba0d39788888542cd6b8775095a0f35e
http://hdl.handle.net/20.500.12278/112060
http://hdl.handle.net/20.500.12278/112060
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, ⟨10.1177/0954410020939338⟩
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, ⟨10.1177/0954410020939338⟩
International audience; In this work, a design strategy for optimising thin-walled structures based on a global-local finite element (FE) modelling approach is presented. The preliminary design of thin-walled structures can be stated in the form of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::baddf5a9adc0fe9ae74e5cdb67c2b885
https://hdl.handle.net/10985/19269
https://hdl.handle.net/10985/19269