Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Margarita Akterskaia"'
Publikováno v:
Composite Structures
A two-way coupling global-local finite element approach which has demonstrated its potential on the basis of representative test cases in earlier work, is used for the progressive failure analysis of large stiffened composite panels. In order to real
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f7f428d8675d09cbe719fa190931bf15
https://doi.org/10.1016/j.compstruct.2017.02.011
https://doi.org/10.1016/j.compstruct.2017.02.011
Publikováno v:
Hallett, S, Akterskaia, M, Jansen, E, Weaver, P & Rolfes, R 2019, ' Progressive Failure Analysis Using Global-Local Coupling Including Intralaminar Failure and Debonding ', AIAA Journal, vol. 57, no. 7, pp. 3078-3089 . https://doi.org/10.2514/1.J057677
AIAA Journal
AIAA Journal
Composite laminate stiffened panels are often used in aircraft fuselage design because of their favorable properties. To assess the failure load of these thin-walled structures and to exploit their reserves, a reliable simulation capability for their
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7d701a74c32e64b2bfa5b137805f4b32
https://zenodo.org/record/2667336
https://zenodo.org/record/2667336
Publikováno v:
Composite Structures
Together with fiber breakage and matrix cracking, delamination is one of the common damage mechanisms occurring in laminated fiber-reinforced composite structures. Delamination initiates due to the relatively low interlaminar strength of adjacent pli
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::21024720042475bd8b3733cd64055425
Publikováno v:
Advances in Predictive Models and Methodologies for Numerically Efficient Linear and Nonlinear Analysis of Composites ISBN: 9783030119683
PoliTO Springer Series
PoliTO Springer Series-Advances in Predictive Models and Methodologies for Numerically Efficient Linear and Nonlinear Analysis of Composites
Advances in Predictive Models and Methodologies for Numerically Efficient Linear and Nonlinear Analysis of Composites
PoliTO Springer Series
PoliTO Springer Series-Advances in Predictive Models and Methodologies for Numerically Efficient Linear and Nonlinear Analysis of Composites
Advances in Predictive Models and Methodologies for Numerically Efficient Linear and Nonlinear Analysis of Composites
A novel two-way global-local coupling approach to model progressive separation of skin and stringer in combination with intralaminar damage in stiffened CFRP panels under compression is presented. The methodology makes it possible to examine the dama
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5b2f0dc08393791d64ab9dd22e2cddff
https://doi.org/10.1007/978-3-030-11969-0_6
https://doi.org/10.1007/978-3-030-11969-0_6
Publikováno v:
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f62598d4a5a45f7b93e3068db3b4271
https://doi.org/10.2514/6.2018-0735.c1
https://doi.org/10.2514/6.2018-0735.c1
Publikováno v:
Composite Structures
Akterskaia, M, Jansen, E, Hallett, S R, Weaver, P & Rolfes, R 2018, ' Analysis of skin-stringer debonding in composite panels through a two-way global-local method ', Composite Structures, vol. 202, pp. 1280-1294 . https://doi.org/10.1016/j.compstruct.2018.06.064
Akterskaia, M, Jansen, E, Hallett, S R, Weaver, P & Rolfes, R 2018, ' Analysis of skin-stringer debonding in composite panels through a two-way global-local method ', Composite Structures, vol. 202, pp. 1280-1294 . https://doi.org/10.1016/j.compstruct.2018.06.064
According to various experimental results, stiffened panels under compressive loading are prone to debonding between the skin and the flange of the stringer. In this paper, a novel two-way global-local coupling approach is presented that is able to m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::448506cb7c4270b60e21e92947524d84