Post-Buckling Behaviour Simulation of Think Curved Composite Panels in Airbus Defence and Space: Review of Numerical Methods

This paper was authored by F. Sanchez, R. Tejerina, G. Banos, E. Osle in support of their presentation at the 2015 NAFEMS World Congress that was held in San Diego, USA on 21-24th June 2015.

Document Details

ReferenceNWC15_232
AuthorsSanchez. F Tejerina. R Banos. G Osle. E
LanguageEnglish
TypePaper
Date 21st June 2015
OrganisationAirbus
RegionWorld

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