In this work, carried out in AIRBUS office in Hamburg within the A350 XWB Development Program, the influence of geometric deviations of the bondline on the strength of a composite stepped bonded joint has been investigated. This finite element investigation takes into account adhesive plasticity and both adhesive and intraply damage. Failure has been implemented for the adhesive using a ductile damage law and for the intraply using a cohesive traction separation law
Influence of geometrical deviations of bondline on strength of adhesively bonded joints in composites-numerical analysis
Gagani, Abedin
2015/2016
Abstract
In this work, carried out in AIRBUS office in Hamburg within the A350 XWB Development Program, the influence of geometric deviations of the bondline on the strength of a composite stepped bonded joint has been investigated. This finite element investigation takes into account adhesive plasticity and both adhesive and intraply damage. Failure has been implemented for the adhesive using a ductile damage law and for the intraply using a cohesive traction separation lawFile in questo prodotto:
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/19664