Analysis of the bauschinger effect on a multilayer helicopter blade by XFEM simulation

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dc.contributor.authorNour, Abdelkader
dc.contributor.authorGherbi, Mohamed Tahar
dc.contributor.authorTawfiq, Imad
dc.date.accessioned2018-01-22T06:45:10Z
dc.date.available2018-01-22T06:45:10Z
dc.date.issued2017
dc.identifier.issn1270-9638
dc.identifier.urihttps://dspace.univ-boumerdes.dz/handle/123456789/4360
dc.identifier.urihttps://doi.org/10.1016/j.ast.2017.05.039
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.relation.ispartofseriesAerospace Science and Technology/ Vol.69 (2017);pp. 97-113
dc.subjectBladeen_US
dc.subjectFatigueen_US
dc.subjectHelicopteren_US
dc.subjectBauschingeren_US
dc.subjectCracken_US
dc.subjectCompositeen_US
dc.titleAnalysis of the bauschinger effect on a multilayer helicopter blade by XFEM simulationen_US
dc.typeArticleen_US

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