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dc.contributor.authorGuida, M.
dc.contributor.authorMarulo, F.
dc.contributor.authorMeo, M.
dc.contributor.authorGrimaldi, A.
dc.contributor.authorOlivares, Gerardo
dc.date.accessioned2012-01-25T18:23:51Z
dc.date.available2012-01-25T18:23:51Z
dc.date.issued2011-02
dc.identifierWOS:000285673300001
dc.identifier.citationM. Guida, F. Marulo, M. Meo, A. Grimaldi, G. Olivares, SPH -- Lagrangian study of bird impact on leading edge wing, Composite Structures, Volume 93, Issue 3, February 2011, Pages 1060-1071, ISSN 0263-8223, 10.1016/j.compstruct.2010.10.001en_US
dc.identifier.issn0263-8223
dc.identifier.urihttp://dx.doi.org/10.1016/j.compstruct.2010.10.001
dc.identifier.urihttp://hdl.handle.net/10057/4216
dc.descriptionFull text of this article is not available in SOAR.en_US
dc.description.abstractResults from the experimental tests are given so that they can be used to validate numerical models and promote the use of the numerical tools in aircraft design and certification process. The explicit finite element software LS - Dyna and MSC - Dytran were selected to perform the simulations using two different approaches: Lagrangian and smooth particle hydrodynamics techniques and a comparison was performed to define the differences between two approaches. This paper demonstrates the accuracy of the methods for bird impact on a rigid target and subsequently it produced the state of the art of the bird-strike simulation. Impact, failure after the impact, and high strength at impact properties of glass fibre laminate combination sandwich composite were investigated in this study.en_US
dc.language.isoen_USen_US
dc.publisherElsevieren_US
dc.relation.ispartofseriesComposite Structures;v.93, no.3
dc.subjectSPHen_US
dc.subjectLagrangianen_US
dc.subjectWing leading edgeen_US
dc.subjectFibre material laminateen_US
dc.subjectBird-strikeen_US
dc.subjectHigh speeden_US
dc.titleSPH -- Lagrangian study of bird impact on leading edge wingen_US
dc.typeArticleen_US
dc.description.versionPeer reviewed


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