Zobrazeno 1 - 10
of 28
pro vyhledávání: '"Skin-stringer debonding"'
This paper investigates the damage behavior of a reinforced composite panel under symmetrical and asymmetrical bending load. The examined reinforced composite structure is a curved CFRP panel and a co–cured CFRP omega stringer. It may be considered
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::30d61496d74e07fb2626b422c7062f34
https://hdl.handle.net/11583/2979146
https://hdl.handle.net/11583/2979146
Autor:
Akterskaia, Margarita
An increasing application of fibre-reinforced composites in aircraft and aerospace engineering contributed to the rise of development of highly effective numerical tools. On the one hand, computational simulations help to overcome the problems relate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d365bee607e492e8ba0a3abdf49696db
https://www.repo.uni-hannover.de/handle/123456789/5260
https://www.repo.uni-hannover.de/handle/123456789/5260
The present work is focused on the study of the damage behaviour of a composite reinforced panel under quasi-static bending loading conditions. The investigated reinforced composite structure, consisting of a curved CFRP panel reinforced and a co-cur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::70bab62ce2056020283de5e1c800748a
http://hdl.handle.net/11591/399591
http://hdl.handle.net/11591/399591
Autor:
Umberto Mercurio, F. Scaramuzzino, Domenico Tescione, Aniello Riccio, Rosario Borrelli, A. Raimondo
Publikováno v:
Applied Composite Materials. 21:467-481
In this paper, a numerical study has been carried out on skin delamination and skin-stringer debonding growth in a composite wing-box under compressive loading conditions. The adopted numerical models use the Virtual Crack Closure Technique to simula
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1a6b0415350f20be7a25ab2abf16b35e
https://doi.org/10.1007/s10443-013-9347-2
https://doi.org/10.1007/s10443-013-9347-2
Publikováno v:
Key Engineering Materials. :605-608
In this paper, a numerical study, on the compressive behaviour of stiffened composite panels with skin-stringer debonding has been carried out. The analysis has been performed by adopting a novel robust (mesh and time step independent) finite element
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::03e8b9c14f92d4db9244b36c093c31bb
https://doi.org/10.4028/www.scientific.net/kem.577-578.605
https://doi.org/10.4028/www.scientific.net/kem.577-578.605
Akademický článek
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Numerical simulations on stiffened composite panels have been performed in order to investigate the influence of fibre bridging phenomenon on the onset and on the evolution of skin-stringer debonding. A novel numerical procedure for delamination grow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::41b2012308c6dcd710728b96e9b6ba20
http://hdl.handle.net/11591/374144
http://hdl.handle.net/11591/374144
Akademický článek
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Publikováno v:
Advanced composites letters
Advanced composites letters, Woodhead Publishing Limited, 2014, 23 (6), pp.142-148. ⟨10.1177/096369351402300602⟩
Advanced Composites Letters
Advanced Composites Letters, 2014, 23 (6), pp.142--148
Advanced composites letters, 2014, 23 (6), pp.142-148. ⟨10.1177/096369351402300602⟩
Scopus-Elsevier
Advanced composites letters, Woodhead Publishing Limited, 2014, 23 (6), pp.142-148. ⟨10.1177/096369351402300602⟩
Advanced Composites Letters
Advanced Composites Letters, 2014, 23 (6), pp.142--148
Advanced composites letters, 2014, 23 (6), pp.142-148. ⟨10.1177/096369351402300602⟩
Scopus-Elsevier
WOS:000349723000002; International audience; An experimental investigation aiming to characterize the fatigue failure mechanisms and effect of ageing of skin/stringer interfaces is presented. A simplified specimen known as a "stringer foot specimen"
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::58e0bafc223f8f4883d3bc2abbb87566
https://oatao.univ-toulouse.fr/24025/
https://oatao.univ-toulouse.fr/24025/