Combined loadings after medium velocity impact on large CFRP laminated plates: Discrete ply model simulations

To decrease development costs of aeronautical composite structures, industrials and academic researchers are turning to “virtual testing” methods. To help achieve this objective, a new methodology has been developed at the Institut Clément Ader. It is based on a complex loading test rig for technolo...

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Autores principales: J. Serra, A. Trellu, C. Bouvet, S. Rivallant, B. Castanié, L. Ratsifandrihana
Formato: article
Lenguaje:EN
Publicado: Elsevier 2021
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Acceso en línea:https://doaj.org/article/e5255202a6b4463c8c1eaa8724b61e56
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