Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Fariborz Sheibanian"'
Publikováno v:
Metals, Vol 11, Iss 2, p 320 (2021)
This paper provides further understanding of the peak load effect on micro-crack formation and residual stress relaxation. Comprehensive numerical simulations using the finite element method are applied to simultaneously take into account the effect
Externí odkaz:
https://doaj.org/article/55538bd4f9af42cfb5c2893c8bac737d
This paper provides a further understanding of the peak load effect on the damage mechanics and residual stress relaxation. The comprehensive numerical simulations using the finite element method are applied to take into account simultaneously the ef
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15b49c108a77d072e7be83ab5aa5d755
https://doi.org/10.22541/au.160033881.11570079
https://doi.org/10.22541/au.160033881.11570079
Autor:
Hossein Hosseini-Toudeshky, Mehdi Ahmadi Najfabadi, Jalal Yousefi, Giangiacomo Minak, Naeim Akbari Shahkhosravi, Fariborz Sheibanian
In this paper, a very promising procedure to evaluate damage initiation and propagation of high speed drilled composite laminates base on Acoustic Emission (AE) and Finite Element (FE) techniques is proposed. First, the extent of delamination after h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cb4cf37f408d6a610be8274edce6ace1
http://hdl.handle.net/11585/684686
http://hdl.handle.net/11585/684686
Publikováno v:
Theoretical and Applied Fracture Mechanics. 106:102480
A new mixed mode strain based cohesive zone model (CZM) has been developed for progressive damage analyses of adhesively bonded joints under fatigue loading. Independency of this method from experimental characterization of mixed-mode conditions is t
Autor:
Meisam Jalalvand, Hon Wing Michael Lok Wu, Fariborz Sheibanian, Mohamad Fotouhi, Wisnom, Michael R.
Publikováno v:
ECCM18-18th European Conference on Composite Materials
University of Strathclyde
University of Strathclyde
In this paper, a new concept for health-monitoring of bonded patch repairs is presented. Aerospace structures using aluminium panels occasionally crack and bonded composite patches are one of the repair methods available to maintain the integrity of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::fb95680ff1f719d5cc70919be6d9ca2f
https://strathprints.strath.ac.uk/66565/1/Jalalvand_etal_ECCM18_Self_warning_hybrid_composite_patches_for_repairing.pdf
https://strathprints.strath.ac.uk/66565/1/Jalalvand_etal_ECCM18_Self_warning_hybrid_composite_patches_for_repairing.pdf