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Ponencia
Análisis de postpandeo de un panel rigidizado de material compuesto mediante técnicas de modelado multi-global-local incluyendo daño interlaminar
(Asociación Española de Materiales Compuestos (AEMAC), 2015-07)
El uso de paneles rigidizados de material compuesto ha sido incorporado en numerosas aplicaciones. En las situaciones en las que las cargas originan estados tensionales de compresión, éstas pueden producir fenómenos de ...
Ponencia
Stress analysis of finite anisotropic plates with cutouts under displacement boundary conditions
(Asociación Española de Materiales Compuestos (AEMAC), 2015-07)
The aim of this article is to provide an analytical tool to estímate the stress concentration in anisotropic plates weakened by a circular or elliptical hole; it is achieved by developing Lekhnitskii formalism in order ...
Ponencia
Estudio experimental de placas preconformadas en postpandeo
(Asociación Española de Materiales Compuestos (AEMAC), 2015-07)
El pandeo de placas y láminas no necesariamente está asociado al colapso, que en ocasiones se produce para una carga que es varias veces superior. No obstante, aprovechar esta capacidad postpandeo no es fácil, siendo el ...
Artículo
Accurate determination of the stiffness properties for an elastic interface under peeling conditions between homogeneous materials
(Elsevier, 2022-04)
In this paper, several models for analysing peeling tests are considered, including numerical models based on FEM, semi-analytical approaches, and beam models including an elastic interface. Results show that none of the ...
Artículo
On the 3D extension of failure models for adhesive joints under mixed-mode fracture conditions: LEBIM and CZM
(Elsevier, 2019-04)
Interface models for triggering damage events have been extensively used in many engineering applications due to their inherent versatility and relatively simple numerical implementations. Usually, the non-linear behavior ...
Artículo
A new in situ peeling test for the characterisation of composite bonded joints
(Elsevier, 2018-10)
At the moment, bonded joints quality on composites used in aeronautical industry is verified based on the determination of the interlaminar fracture toughness (Gc) obtained by means of the Double Cantilever Beam (DCB) or ...