Zobrazeno 1 - 10
of 35
pro vyhledávání: '"Reinforced panel"'
Publikováno v:
E3S Web of Conferences, Vol 383, p 05015 (2023)
When designing thin-walled aircraft structures, as a rule, the main limitations are associated with ensuring stability. The objects of research in this work are composite z-shaped reinforced panels of the wing box of an aircraft. For the early stages
Externí odkaz:
https://doaj.org/article/7319bd0f19dc4b4790720d62b7d921c6
Akademický článek
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Publikováno v:
Applied Sciences, Vol 9, Iss 6, p 1168 (2019)
The blow-off impulse effect of a composite reinforced panel subjected to lightning strike is studied combing electric-thermal coupling with explicit dynamic methods. A finite element model of a composite reinforced panel is established under the acti
Externí odkaz:
https://doaj.org/article/7aa1f8b303a24b4c8d1da319f807e83f
Autor:
Augello, Riccardo, Pagani, Alfonso, Carrera, Erasmo, Peeters, D.M.J., do Prado, Alex Pereira, dos Santos, Henrique E.A.A., Galeb, Pedro H.G., H. Cabral, Pedro, Vassilopoulos, Anastasios P., Michaud, Véronique
Publikováno v:
Proceedings of the 20th European Conference on Composite Materials: Composites Meet Sustainability: Vol 4 – Modeling and Prediction
Proceedings of the 20th European Conference on Composite Materials: Composites Meet Sustainability
Proceedings of the 20th European Conference on Composite Materials: Composites Meet Sustainability
The present paper deals with the buckling and post-buckling analysis of a multilayered composite reinforced panel. The panel, design for aeronautical applications, results in a complex stacking sequence, and the development of a refined model able to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=narcis______::9326e53d20a19d6a6d47e428ae69f265
http://resolver.tudelft.nl/uuid:cd21969f-60fa-485e-a889-be38199153a8
http://resolver.tudelft.nl/uuid:cd21969f-60fa-485e-a889-be38199153a8
The present paper deals with the buckling and post-buckling analysis of a multilayered composite reinforced panel. The panel, design for aeronautical applications, results in a complex stacking sequence, and the development of a refined model able to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dris___00893::47ffab2e19fce55b15b023f43e9dc6d2
http://resolver.tudelft.nl/uuid:cd21969f-60fa-485e-a889-be38199153a8
http://resolver.tudelft.nl/uuid:cd21969f-60fa-485e-a889-be38199153a8
Autor:
Silva, Felipe Langellotti
O crescimento do emprego de materiais compósitos e a flexibilização dos processos de manufatura permitem a adoção deste tipo de material em diversos casos que antes não eram explorados. Este trabalho investiga técnicas de otimização aplicáv
Publikováno v:
International Journal of Industrial Ergonomics
Introduction In April 2020, novel coronavirus SARS-CoV-2 (COVID-19) produced an ongoing mass fatality event in New York. This overwhelmed hospital morgues necessitating emergent expansion of capacity in the form of refrigerated trucks, trailers, and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b6a20d9c38cf4cdc168f9d9f8829772b
https://pubmed.ncbi.nlm.nih.gov/35039703
https://pubmed.ncbi.nlm.nih.gov/35039703
In this work, a numerical analysis of the buckling behavior of a panel in CFRP with longitudinal and transverse stiffeners is reported. The focus was to evaluate the influence of damage at the center of the panel, simulated with a cut that affects th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b808be36a5b0ed867f95d4632ddcff2b
https://hdl.handle.net/11587/437114
https://hdl.handle.net/11587/437114
Akademický článek
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Autor:
Aniello Riccio, Salvatore Saputo, Vincenza Antonucci, R. Ricchiuto, Valentina Lopresto, A. Raimondo, Francesco Caputo
Publikováno v:
Progress in Aerospace Sciences 81 (2016): 41–48. doi:10.1016/j.paerosci.2015.11.004
info:cnr-pdr/source/autori:Riccio A.; Ricchiuto R.; Saputo S.; Raimondo A.; Caputo F.; Antonucci V.; Lopresto V./titolo:Impact behaviour of omega stiffened composite panels/doi:10.1016%2Fj.paerosci.2015.11.004/rivista:Progress in Aerospace Sciences/anno:2016/pagina_da:41/pagina_a:48/intervallo_pagine:41–48/volume:81
info:cnr-pdr/source/autori:Riccio A.; Ricchiuto R.; Saputo S.; Raimondo A.; Caputo F.; Antonucci V.; Lopresto V./titolo:Impact behaviour of omega stiffened composite panels/doi:10.1016%2Fj.paerosci.2015.11.004/rivista:Progress in Aerospace Sciences/anno:2016/pagina_da:41/pagina_a:48/intervallo_pagine:41–48/volume:81
The mechanical response of reinforced composite structures under impact loads is particularly challenging owing to the rising of multiple and simultaneous failure phenomena. Indeed, low velocity impacts may produce intra-laminar damages, like fibre b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4072ded97a004f861429409694bd1a23
http://hdl.handle.net/11591/360637
http://hdl.handle.net/11591/360637