Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Ahmad Al-Azzawi"'
Publikováno v:
Journal of Reinforced Plastics and Composites. 41:167-186
This study includes experimental and numerical investigations on fibre-metal laminate structures containing adhesive joints under static bending loads. Experimental tests were carried out on Glare® 4B specimens manufactured in-house and containing d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::93c52f202b5bfde4e55864af42727b64
https://doi.org/10.1177/07316844211051706
https://doi.org/10.1177/07316844211051706
Publikováno v:
Al-Azzawi, A S M, Kawashita, L F & Featherston, C A 2019, ' A modified cohesive zone model for fatigue delamination in adhesive joints : Numerical and experimental investigations ', Composite Structures, vol. 225, 111114 . https://doi.org/10.1016/j.compstruct.2019.111114
A modified cohesive zone model (CZM) has been developed to simulate damage initiation and evolution in Fibre-Metal Laminates (FMLs) manufactured in-house but based on the Glare® material specifications. Specimens containing both splice and doubler f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::22ad51ac040a4673e7bd649c6fe10446
https://hdl.handle.net/1983/a12688cb-947b-49e7-9acc-5a9090cd56a7
https://hdl.handle.net/1983/a12688cb-947b-49e7-9acc-5a9090cd56a7
Autor:
Karen Margaret Holford, John McCrory, Luiz F. Kawashita, Ahmad Al-Azzawi, Carol Ann Featherston, Rhys Pullin
Publikováno v:
Al-Azzawi, A S M, McCrory, J, Kawashita, L F, Featherston, C A, Pullin, R & Holford, K M 2017, ' Buckling and postbuckling behaviour of Glare laminates containing splices and doublers. Part 1 : Instrumented Tests ', Composite Structures, vol. 176, pp. 1158-1169 . https://doi.org/10.1016/j.compstruct.2017.04.030
The progressive damage and fracture behaviour of Glare® fibre-metal laminates (FMLs) was investigated experimentally for the buckling and post- buckling regimes of laminates containing internal ‘splice’ and ‘doubler’ joints. Specimens were e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::982286676c1bb70fafefe51757ef33b9
http://www.scopus.com/inward/record.url?scp=85020690356&partnerID=8YFLogxK
http://www.scopus.com/inward/record.url?scp=85020690356&partnerID=8YFLogxK
Publikováno v:
Al-Azzawi, A S M, Kawashita, L F & Featherston, C A 2017, ' Buckling and postbuckling behaviour of Glare laminates containing splices and doublers. Part 2 : Numerical modelling ', Composite Structures, vol. 176, pp. 1170-1187 . https://doi.org/10.1016/j.compstruct.2017.04.063
A 3D finite element model using cohesive elements and continuum (bulk) material damage models was developed to examine the progressive damage and failure behaviour of Glare® Fibre Metal Laminate (FML) specimens subjected to in-plane compressive load
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9c707c8d12a2eca9c53a30d46e7c859f
https://hdl.handle.net/1983/270300c5-1c3e-4770-823c-bd88deb6e99e
https://hdl.handle.net/1983/270300c5-1c3e-4770-823c-bd88deb6e99e